Description:FIELD OF THE INVENTION
[0001] The present invention discloses a support structure. More particularly, the present disclosure relates to a support structure for mounting components to a surface.

BACKGROUND
[0002] In various industries, including automotive, aerospace, marine, and others, securing components within systems is of paramount importance to ensure safety, reliability, and optimal performance. However, in the realm of automotive industry in case of two-wheeled vehicles, such as motorcycles or scooters, this endeavor presents a particularly formidable challenge due to the constrained spatial configurations within which engineers must operate.
[0003] Support structures are required to be configured in such a way that they will be able to carry the weight of the components and able to withstand the working environment conditions of the components. Further, in the case of vehicles, configuring a support structure for each individual component is challenging because doing so would increase the number of components in the vehicle which would lead to an overall increase in the weight of the vehicle.
[0004] The configuration of support structures necessitates meticulous consideration, ensuring they possess the requisite strength to bear the weight of components and withstand the rigors of their operational environments. This requirement is particularly crucial within the realm of vehicles, where the challenge intensifies due to the intricate balance between structural integrity and weight optimization. Indeed, within the context of vehicles, developing individual support structures for every component poses a challenging task, as each addition not only contributes to the complexity of the vehicle's layout but also augments its overall weight.
[0005] The existing support structures frequently struggle with multifaceted challenges, ranging from difficulties in configuration to complexities in assembly, and from a lack of adaptability to concerns over structural integrity. Moreover, conventional support frameworks often fall short in their ability to accommodate the diverse range of component sizes and shapes encountered across various applications. This inflexibility poses a significant obstacle, hindering the seamless integration of components and compromising overall system performance.
[0006] In addition to their inherent configuration limitations, existing support structures also present significant challenges during installation and servicing, particularly within the context of vehicle applications. The complexities associated with mounting these structures onto vehicles contribute to substantial hurdles, impeding both initial installation and subsequent maintenance efforts. When vehicles require servicing, the cumbersome nature of these support structures worsens the situation, making it difficult to replace or modify them as needed. Further, an evident deficiency lies in the lack of reusability inherent in current support structure, rendering them unsuitable for repeated use across multiple servicing cycles. Consequently, components mounted on such structures face considerable obstacles during routine maintenance procedures, significantly prolonging service times and amplifying associated costs.
[0007] The above information as disclosed in this background section is only for enhancement of understanding of the background of the disclosure and therefore it may contain information that does not form the prior art that is already known in this country to a person of ordinary skill in the art. Further limitations and disadvantages of conventional and traditional approaches will become apparent to one of skill in the art, through comparison of described systems with some aspects of the present disclosure, as set forth in the remainder of the present disclosure and with reference to the drawings.

SUMMARY
[0008] It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention, as claimed.
[0009] In one of the embodiments of the present disclosure, a support structure for securing components comprising a fitment portion, a holding portion and a stay portion. The fitment portion comprising at least one fitment protrusion, the holding portion comprising plurality of fitment provisions and the stay portion comprising at least two arms. Further, the fitment portion is configured to pass within an insertion region and to connect the at least one fitment protrusion with at least one of the pluralities of fitment provisions. Furthermore, the insertion region is defined between the at least two arms of the stay portion.
[00010] In one of the embodiments of the present disclosure, the holding portion is disposed between the fitment portion and the stay portion. Further, the fitment portion, the holding portion and the stay portion are integrally connected. Furthermore, the width of the fitment portion is always less than the width of the insertion region.
[00011] In one of the embodiments of the present disclosure, the at least two arms are originated from an intersection point of the holding portion and the stay portion of the support structure. Further, an opposite end of the at least two arms comprising one or more engaging ends. Furthermore, the one or more engaging ends of the at least two arms are configured to detachably abut with openings present in a surface.
[00012] In one of the embodiments of the present disclosure, an engagement between the one or more engaging ends of the at least two arms and the opening in the surface is enabled by snap-fit connections.
[00013] In one of the embodiments of the present disclosure, the fitment portion and the holding portion are configured to encircle the securing components, and wherein adjustment of the holding portion is enabled based on a diameter of the securing components. Further, the at least one fitment protrusion are distributed along circumference of the fitment portion and the plurality of fitment provisions are distributed along circumference of the holding portion.
[00014] In one of the embodiments of the present disclosure, a method for securing components within a surface using a support structure is disclosed. The method comprising steps of passing, a fitment portion of the support structure through an insertion region. The insertion region is defined between at least two arms of a stay portion. Further, connecting, at least one fitment protrusion of the fitment portion with at least one of a plurality of fitment provisions of a holding portion. Furthermore, positioning the support structure within the surface using one or more engaging ends of the at least two arms and abutting the support structure with openings present in the surface.
[00015] In one of the embodiments of the present disclosure, the method comprising step of encircling the securing components with the fitment portion and the holding portion of the support structure. Further, the method also comprising step of flexibly adjusting the plurality of fitment provisions of the holding portion based on a diameter of the securing components.

BRIEF DESCRIPTION OF FIGURES:
[00016] The accompanying drawings, which are incorporated herein and constitute part of this specification, illustrate preferred embodiments of the invention, and together with the general description given above and the detailed description given below, serve to explain features of the invention.
[00017] Figure 1 illustrates a perspective view of an assembly showing support structure used for securing components, in accordance with an embodiment of the present subject matter.
[00018] Figure 2 illustrates a perspective view of a support structure in accordance with an embodiment of the present subject matter.
[00019] Figure 3 illustrates a top view of a support structure and sectional view of the same along a plane AA in accordance with an embodiment of the present subject matter.
[00020] Figure 4 illustrates a plan view of a support structure inside a fuel tank of a vehicle in accordance with an embodiment of the present subject matter.

DETAILED DESCRIPTION
[00021] Exemplary embodiments detailing features of the present disclosure in accordance with the present subject matter will be described hereunder with reference to the accompanying drawings. Various aspects of different embodiments of the present invention will become discernible from the following description set out hereunder. Rather, the following description provides a convenient illustration for implementing exemplary embodiments of the present subject matter. Further, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. Additionally, all numerical terms, such as, but not limited to, “first”, “second”, “third”, “primary”, “secondary”, “main” or any other ordinary and/or numerical terms, should also be taken only as identifiers, to assist the reader's understanding of the various elements, embodiments, variations and/or modifications of the present disclosure, and may not create any limitations, particularly as to the order, or preference, of any element, embodiment, variation and/or modification relative to, or over, another element, embodiment, variation and/or modification.
[00022] The following detailed description refers to the accompanying drawings. Wherever possible, the same reference numbers are used in the drawings and the following description to refer to the same or similar elements. While embodiments may be described, modifications, adaptations, and other implementations are possible. For example, substitutions, additions, or modifications may be made to the elements illustrated in the drawings, and the methods described herein may be modified by substituting, reordering, or adding stages to the disclosed methods. Accordingly, the following detailed description does not limit the claimed subject matter. Instead, the proper scope of the claimed subject matter is defined by the appended claims. It should be noted that the description and figures merely illustrate principles of the present subject matter. Various arrangements may be devised that, although not explicitly described or shown herein, encompass the principles of the present subject matter. Moreover, all statements herein reciting principles, aspects, and examples of the present subject matter, as well as specific examples thereof, are intended to encompass equivalents thereof.
[00023] Further, various embodiments disclosed herein are to be taken in the illustrative and explanatory sense and should in no way be construed as limiting of the present disclosure. All joinder references (e.g., attached, affixed, coupled, disposed, etc.) are only used to aid the reader's understanding of the present disclosure, and may not create limitations, particularly as to the position, orientation, or use of the systems and/or methods disclosed herein. Therefore, joinder references, if any, are to be construed broadly. Moreover, such joinder references do not necessarily infer those two elements are directly connected to each other.
[00024] It will also be appreciated that one or more of the elements depicted in the drawings/figures can also be implemented in a more separated or integrated manner, or even removed or rendered as inoperable in certain cases, as is useful in accordance with a particular disclosure. Additionally, any signal hatches in the drawings/figures should be considered only as exemplary, and not limiting, unless otherwise specifically specified.
[00025] The at least one object of the present disclosure is to provide support structures that offer improved functionality, ensuring they can effectively carry the weight of components and withstand the working conditions within diverse environments. Further, to simplify the configuration of the support structures and assembly process of the same, reducing complexity and streamlining installation procedures.
[00026] The at least one object of the present disclosure is to provide support structures that exhibit greater adjustability and flexibility, enabling them to accommodate variations in component size and shape without compromising structural integrity. Further, to facilitate ease of installation and servicing, ensuring that support structures can be readily mounted onto vehicles and easily serviced or replaced as needed.
[00027] The at least one object of the present disclosure is to provide support structures that are reusable, minimizing the need for frequent replacement and thereby reducing maintenance costs over the operational lifespan of the vehicle. Further, to optimize weight efficiency within support structure, minimizing the overall weight added to vehicles while maintaining necessary strength and stability. Furthermore, to enhance compatibility and adaptability, ensuring that support structures can seamlessly integrate with various vehicle components and adapt to evolving engineering requirements.
[00028] Figure 1 illustrates a perspective view of an assembly showing support structure used for securing components. Figure 2 illustrates a perspective view of the support structure. Figure 3 illustrates a top view of the support structure and sectional view of the same along a plane AA. The figures 1 to 3 are taken together for describing the present subject matter.
[00029] The support structure (200) as disclosed in the present disclosure is configured to secure components within various systems, offering a comprehensive framework that addresses the challenges of installation and stability. More specifically, the support structure (200) comprising three integral components - a fitment portion (200A), a holding portion (200B), and a stay portion (200C). The fitment portion (200A), comprising at least one fitment protrusion (202), serves as the point of attachment for securing components such as but not limited to cables of vehicle, Roll Over Valve (ROV), Evaporative Emission Control System (EVAP). The at least one fitment protrusion (202) is configured to seamlessly pass within an insertion region (218) which is situated between the two arms (206, 212) of the stay portion (200C).
[00030] Within the insertion region (218) lies the functionality of the support structure (200), as it facilitates the connection between the at least one fitment protrusion (202) and the plurality of fitment provisions (204) housed within the holding portion (200B). The holding portion (200B) is configured with multiple fitment provisions (204) strategically distributed to ensure robust attachment and stability. Further, the stay portion (200C) reinforces the structure's stability, comprising at least two arms (206, 212) that define the insertion region (218) and provide essential support. This configuration not only enhances the structural integrity of the support structure (200) but also offers versatility in component mounting, accommodating a diverse range of sizes and shapes with ease.
[00031] In one of the embodiments of the present disclosure, positioned between the fitment portion (200A) and the stay portion (200C), the holding portion (200B) serves as a pivotal element within the structure's framework. More specifically, these three components - the fitment portion, holding portion, and stay portion - are seamlessly integrated, forming a cohesive unit that ensures structural integrity and operational efficiency. This integration is crucial for strengthening the support structure (200) stability and reliability during use.
[00032] In one of the embodiments of the present disclosure, the width of the fitment portion (200A) is deliberately maintained to be less than that of the insertion region (218) situated between the arms of the stay portion (200C). This deliberate discrepancy in width facilitates the smooth passage of the fitment portion (200A) through the insertion region (218), ensuring a snug fit and secure attachment within the support structure (200). By aligning the dimensions in this manner, the support structure (200) is optimized for seamless installation and robust component mounting, ultimately enhancing its overall effectiveness within various systems and applications.
[00033] In one of the embodiments of the present disclosure, the intersection point where the at least two arms (206, 212) originate, serving as a pivotal juncture where the holding portion (200B) and the stay portion (200C) also connect. This intersection point serves as a crucial anchor point, providing structural stability and support to the entire framework of the support structure (200). From this intersection point, the at least two arms (206, 212) extend outward, forming an integral part of the support structure (200). Further, positioned at the opposite ends (210, 216) of the support structure (200) are engaging ends (208A, 208B, 214A, 214B), which play a vital role in facilitating secure attachment to external surfaces or components.
[00034] The positioning of the engaging ends (208A, 208B) and (214A, 214B) on the arms (206) and (212) respectively and are configured to optimize the functionality and versatility of the support structure (200). More specifically, the engaging ends (208A, 208B, 214A, 214B) are strategically located in close proximity to the opposite ends (210, 216) of the support structure (200), ensuring efficient utilization of space and enhancing the structure's overall stability and effectiveness. By situating the engaging ends (208A, 208B, 214A, 214B) on the at least two arms (206, 212) and aligning them with the same end of the support structure (200), a symmetrical and balanced configuration is achieved, promoting uniform distribution of forces and facilitating secure attachment to external surfaces or components. This symmetrical placement also enhances the support structure's adaptability to various mounting configurations, allowing it to accommodate different spatial constraints and operational requirements with ease. Additionally, by positioning the engaging ends (208A, 208B, 214A, 214B) in this manner, the support structure (200) can effectively leverage its inherent structural integrity and maximize its utility within diverse applications.
[00035] The engaging ends (208A, 208B, 214A, 214B) are configured to ensure optimal grip and stability, enabling the support structure (200) to effectively fulfil its intended function within various systems. By strategically positioning the engaging ends (208A, 208B, 214A, 214B) at the extremities of the at least two arms (206, 212), the support structure (200) achieves enhanced versatility and adaptability, allowing it to accommodate a diverse range of mounting configurations and operational requirements.
[00036] Figure 4 illustrates a plan view of the support structure (200) inside a fuel tank (400) of a two wheeled vehicle. Further, in one of the embodiments of the present disclosure the surface (302) is within the fuel tank (400) of the vehicle. More specifically, the functionality of the support structure (200) is further enhanced by the configuration of its engaging ends (208A, 208B, 214A, 214B) and their interaction with openings (304, 306) on a surface (302). Furthermore, as shown in figure 3, section A-A is passing through the at least two arms (206, 212) and the enlarged view of the section A-A is also shown in the figure 3. The figures 3 and 4 are taken together for describing the present subject matter. The engaging ends (208A, 208B, 214A, 214B) are positioned on the ends of the at least two arms (206, 212) of the support structure (200), serve as key attachment points, allowing for secure and detachable abutment with the openings (302, 306) in the surface (302). This configuration enables the support structure (200) to be easily mounted onto or removed from the surface (302) as needed, facilitating straightforward installation and maintenance procedures. The detachable nature of the engagement ensures versatility and adaptability, allowing the support structure (200) to be repositioned or replaced as required without necessitating extensive disassembly or modification of the surrounding components. Moreover, the interaction between the engaging ends (208A, 208B, 214A, 214B) and the openings (304, 306) provides a reliable anchoring mechanism, ensuring stability and preventing unwanted movement or displacement of the support structure (200) during operation. Accordingly, the support structure (200) offers a practical and efficient solution for securely fastening components within various systems, contributing to improved functionality and ease of use in real-world applications.
[00037] In one of the embodiments of the present disclosure, an engagement mechanism between the engaging ends (208A, 208B, 214A, 214B) of the at least two arms (206, 212) and the openings (304, 306) present in the surface (302) is facilitated by snap-fit connections, offering a robust and efficient attachment solution. Snap-fit connections involve the interlocking of engaging ends (208A, 208B, 214A, 214B) of the at least two arms (206, 212) acting as a mating component through resilient deformation, creating a secure and reliable bond without the need for additional fasteners or adhesive materials with the openings (304, 306) present in the surface (302). More specifically, in the support structure (200), this snap-fit mechanism enables the engaging ends (208A, 208B, 214A, 214B) to engage with the openings (304, 306) seamlessly and firmly in the surface (302), ensuring a tight and stable connection. The said mechanism offers several advantages, including simplicity, ease of assembly, and rapid installation. The snap-fit connections also provide a degree of flexibility, allowing for straightforward disassembly and reassembly if needed, without compromising the integrity of the attachment. Furthermore, the inherent resilience of snap-fit connections enhances the durability and longevity of the engagement, withstanding the rigors of repeated use and environmental conditions.
[00038] In one of the embodiments of the present disclosure, the support structure (200) incorporates a fitment portion (200A) and a holding portion (200B) with the specific purpose of encircling and securing components within a system. This configuration allows for a comprehensive and stable attachment of the components, ensuring they remain firmly in place during operation. The fitment portion (200A) and the holding portion (200B) are engineered to encircle the securing components (102), enveloping them in a secure embrace that minimizes the risk of displacement or movement. The securing components (102) such as but not limited to cables of vehicle, Roll Over Valve (ROV), Canister, Evaporative Emission Control System (EVAP), electronic modules, fluid containers, mechanical components, lighting fixtures, communication devices, powertrain components, fluid lines, hoses.
[00039] In one of the embodiments of the present disclosure, the holding portion (200B) is configured with adjustable material, allowing for adaptation based on the diameter of the securing components (102). This adjustability feature enables the support structure to accommodate components of varying sizes and shapes, ensuring a snug and customized fit that enhances overall stability and functionality. By enabling adjustment of the holding portion based on the diameter of the securing components, the support structure (200) offers versatility and versatility in its application, catering to the diverse needs and requirements of different systems and environments. This capability enhances the reliability of component mounting and also simplifies installation procedures, allowing for seamless integration within various applications.
[00040] In one of the embodiments of the present disclosure, the distribution of the at least one fitment protrusions (202) along the circumference of the fitment portion (200A) and the plurality of fitment provisions (204) along the circumference of the holding portion (200B) is configured to optimize the secure attachment of components (102) within the support structure (200). By dispersing the fitment protrusions and fitment provisions along the circumference of their respective portions, the support structure achieves a uniform and comprehensive coverage that enhances stability and reliability. This distribution ensures that the securing components are evenly supported and held in place, minimizing the risk of uneven weight distribution or potential points of weakness. Further, the placement of the at least one fitment protrusions (202) allow for efficient utilization of space within the support structure, maximizing its capacity to accommodate a diverse range of component sizes and shapes. Furthermore, by evenly distributing he at least one fitment protrusions (202) and the plurality of fitment provisions (204), the support structure (200) facilitates a balanced and secure attachment mechanism that promotes optimal performance and longevity.
[00041] In one of the embodiments of the present disclosure, the method for securely fastening components within a surface (302) using a support structure (200) is disclosed. More specifically, the fitment portion (200A) of the support structure (200) is passed through an insertion region (218) which is positioned between at least two arms (206, 212) of a stay portion (200C). This initial step allows for the precise placement of the support structure (200) within the designated area on the surface (302). Subsequently, the method involves connecting at least one fitment protrusion (202) of the fitment portion (200A) with one of the pluralities of fitment provisions (204) of a holding portion (200B). This connection establishes a secure attachment point between the support structure (200) and the component (102) being secured, ensuring stability and preventing displacement. Further, the support structure (200) is carefully positioned within the surface (302) using one or more engaging ends (208A, 208B, 214A, 214B) of the arms (206, 212). The one or more engaging ends (208A, 208B, 214A, 214B) serve as anchor points, facilitating precise alignment and placement of the support structure (200) within the designated area. Furthermore, the support structure (200) abutting with openings (304, 306) present in the surface (302), further enhancing its stability and ensuring a firm and reliable attachment. Accordingly, the support structure (200) effectively fulfils its intended function of securely fastening components within the surface, offering a practical and efficient solution for various applications.
[00042] In one of the embodiments of the present disclosure, the method includes further steps aimed at ensuring the secure attachment and adaptability of components within the support structure (200). More specifically, securing the components with both the fitment portion (200A) and the holding portion (200B) of the support structure (200). This additional action emphasizes the comprehensive nature of the attachment process, utilizing both components of the support structure (200) to firmly hold the secured components in place. By leveraging the fitment portion to encircle the components and the holding portion to provide additional support, the method enhances the stability and reliability of the attachment, minimizing the risk of movement or displacement during operation.
[00043] In one of the embodiments of the present disclosure, the support structure (200) is composed of at least two distinct materials. More specifically, this configuration is tailored to optimize the performance characteristics of different sections of the support structure. Particularly, the elastic modulus or strength of the stay portion (200C) is intentionally engineered to surpass that of the holding portion (200B). This contrast in material properties ensures that the stay portion (200C), which bears the primary load and provides structural support, possesses superior rigidity and resilience compared to the holding portion (200B). Accordingly, by selecting materials with varying mechanical properties, the support structure (200) can effectively balance strength, flexibility, and durability, thereby enhancing its overall performance and longevity.
[00044] In one of the embodiments of the present disclosure, the method incorporates steps to flexibly adjust the plurality of fitment provisions (204) within the holding portion (200B) based on the diameter of the securing components. This adjustment feature underscores the versatility of the support structure (200), allowing it to accommodate components of varying sizes and shapes with ease. By flexibly adjusting the fitment provisions, the support structure (200) can tailor its grip and support to suit the specific dimensions of the securing components, ensuring a snug and customized fit. This adaptability enhances the functionality and usability of the support structure (200), enabling it to effectively secure a wide range of components within different systems and applications.
[00045] In one of the exemplary embodiments as shown in figure 1 of the present disclosure, the support structure (200) is used to mount the Roll Over Valve (ROV) (102). The ROV, is a safety feature used in the fuel tank (400) of the vehicle and the same is shown in figure number 4 of the present disclosure. The ROV is configured to prevent fuel from spilling out in the event of a rollover or when the vehicle is tilted at extreme angles. It achieves this by closing off the fuel tank's vent during such situations. The body of the ROV includes a float mechanism or a rollover ball that reacts to changes in the vehicle's orientation. When the vehicle is upright, the valve allows the fuel tank to vent properly, maintaining the fuel system's equilibrium. However, when the vehicle starts to tilt beyond a certain angle, typically around 45 degrees, the ROV promptly closes to prevent fuel from escaping. Further, the stems (104, 106) of the ROV (102) are used to connect the ROV on either side with the connecting tubes. The stems may be or may not be offset of each other. Further, in between the stems (104, 106) and the body there are intermediate parts, which enable connection of the stem of the ROV with the body of the stem.
[00046] The support structure (200) plays a crucial role in mounting the stems (104, 106) of the Roll Over Valve (ROV) (102) within the vehicle's fuel tank system. Specifically, the configuration enables the stems (104, 106) of the ROV to be securely held within the holding portion (200B) of the support structure. The process involves passing the fitment portion (200A) of the support structure through an insertion region (218), which is situated between at least two arms (206, 212) of a stay portion (200C). Further, connecting at least one fitment protrusion (202) of the fitment portion (200A) with one of a plurality of fitment provisions (204) of the holding portion (200B), depending on the diameter of the stems (104, 106) of the ROV. This customizable aspect allows for precise fitting of the support structure (200) to accommodate variations in stem diameter, ensuring a secure and tailored attachment. In this configuration, the arms (206, 212) of the stay portion (200C) may remain open or be modified as needed to suit the specific requirements of the mounting process. Accordingly, the support structure (200) is configured to adapt to different vehicle configurations and operational needs, enhancing its functionality and effectiveness in securely mounting the ROV stems within the fuel tank system.
[00047] In one of the exemplary embodiments as shown in figure 4 of the present disclosure, the support structure (200) is used to mount the Roll Over Valve (ROV) (102) inside the fuel tank (400) of a two wheeled vehicle. The fuel tank (400) comprises two main layers: a fuel tank inner and a fuel tank outer. The space between these layers is designated for storing fuel, ensuring the safe containment of the fuel within the vehicle. Further, within the fuel tank inner, there exists a structural arrangement involving a primary fuel tank wall and a secondary fuel tank wall. While the space between the fuel tank outer and the primary fuel tank wall serves as the primary reservoir for holding the fuel, an additional space (302) is allocated between the primary fuel tank wall and the secondary fuel tank wall. The space (302) is configured with with openings (304, 306) which are utilized to detachably hold the one or more engaging ends (208A, 208B, 214A, 214B) of the at least two arms (206, 212) as described earlier. Accordingly, the support structures (200) can be securely affixed within the fuel tank (400), utilizing the space between the primary and secondary fuel tank walls to maintain their position. This arrangement ensures the stability and integrity of the support structures (200) within the fuel tank (400), facilitating their efficient operation in securing components such as the Roll Over Valve (ROV) mentioned earlier.
[00048] In one of the embodiments of the present disclosure, the support structure (200) is placed in close proximity to a canister in the fuel tank (400). This positioning aims to optimize the efficiency of the Roll Over Valve (ROV) while simultaneously reducing the size of the connecting tube. By situating the mounting structure near the canister, the system minimizes potential inefficiencies and streamlines the operation of the ROV, contributing to overall system performance and fuel system efficiency.
[00049] In one of the exemplary embodiments of the present disclosure, the support structure (200) is used in the mounting of cables within a vehicle, contributing to the organization and security of the vehicle's wiring system. More specifically, this configuration facilitates the secure containment of one or more cables within the holding portion (200B) of the support structure (200). The process entails threading the fitment portion (200A) of the support structure through an insertion region (218), strategically positioned between at least two arms (206, 212) of a stay portion (200C). Subsequently, the connection of at least one fitment protrusion (202) from the fitment portion (200A) to a chosen fitment provision (204) within the holding portion (200B) occurs, with the selection based on the diameter of the cables being mounted. This adaptable configuration allows for precise fitting of the support structure (200) to accommodate variations in cable diameter, ensuring a secure and tailored attachment. Accordingly, the support structure (200) find utility in managing cables associated with vehicle components like batteries, contributing to the efficient organization and functionality of the vehicle's electrical systems.
[00050] The one or more engaging ends (208A, 208B, 214A, 214B) of the at least two arms (206, 212) of the support structure (200) are configured for maintaining its stability within the fuel tank (400). By inserting the one or more engaging ends (208A, 208B, 214A, 214B) into the openings (304, 306) of the secondary fuel tank wall, the support structure (200) is firmly positioned. The abutment of the engaging portion against the secondary fuel tank wall ensures a rigid stance for each support structure, contributing to the structural integrity of the fuel tank. Further, this configuration facilitates ease of maintenance and replacement. In the event of repair or replacement needs, the support structure (200) can be conveniently tilted, allowing for straightforward removal from the secondary fuel tank wall. This accessibility simplifies maintenance procedures, reducing downtime and enhancing the overall operational efficiency of the fuel tank system.
[00051] In one of the embodiments of the present disclosure, the support structure (200) consists of three main components: a fitment portion (200A), a holding portion (200B) and a stay portion (200C). Traditionally, support structures may incorporate a single larger diameter stay portion to provide the necessary rigidity and strength. However, in the present disclosure, there may be more than one smaller diameter stay portions instead. This departure from the conventional knowledge allows for a reduction in the material required for constructing the support structures. Despite the reduction in material, the support structure (200) of the present disclosure ensures that the support structures maintain the required rigidity and strength for their intended purpose. By employing multiple smaller diameters stay portions, the support structures achieve a balanced distribution of structural support, effectively optimizing the use of materials while upholding the necessary durability and stability. Accordingly, enhancing the efficiency of material usage but also contributes to the overall effectiveness and reliability of the support structures within various applications.
[00052] In one of the embodiments of the present disclosure, the connecting tube employed in the system is preformed and constructed from multiple layers of resin. This configuration enhances the durability and reliability of the connecting tube, ensuring it can effectively withstand the operational demands within the vehicle's fuel system. The use of multiple resin layers provides added strength and resilience, making the connecting tube suitable for long-term use in various environmental conditions.
[00053] In one of the embodiments of the present disclosure, the support structure (200) can be utilized to secure additional auxiliary components of an Evaporative Emission Control System (EVAP) of the fuel tank. This configuration allows mounting of various EVAP components using the same support structure configuration, enhancing the flexibility and adaptability of the system to accommodate different system configurations and requirements. In one of the embodiments of the present disclosure, the support structures (200) are directly responsible for holding the stem of the ROV or auxiliary components of an EVAP system. This direct attachment method ensures a secure and stable connection, minimizing the risk of component movement or dislodgment during vehicle operation. In one of the embodiments of the present disclosure, the support structures (200) may hold the stems (104, 106) of the ROV (102) or auxiliary components along with the connecting tube positioned over the stem of the ROV within the EVAP system. This arrangement optimizes space utilization and enhances the overall stability and functionality of the system by securely holding multiple components in place.
[00054] In one of the embodiments of the present disclosure, the at least two arms (206, 212) of the support structure (200) may be constructed from metal, resin material, or elastic material in various embodiments. This diverse material selection enables customization based on specific application needs, ensuring compatibility with different environmental conditions, operational demands, and component requirements.
[00055] In one of the embodiments of the present disclosure, length of the support structure (200) may vary within a range of 1 cm to 10 cm, providing flexibility to accommodate different installation requirements and component configurations. Similarly, the width of each stay of the support structure (200) may range between 0.2 cm to 2 cm, allowing for customization to suit specific space constraints and structural considerations.
[00056] The present disclosure offers several advantages that contribute to enhanced functionality, efficiency, and reliability within various systems such as but not limited to the vehicle's fuel system. More specifically, the support structures provide a secure and stable mounting solution for components such as the Roll Over Valve (ROV) and auxiliary components of the Evaporative Emission Control System (EVAP). By securely holding these components in place, the support structures ensure proper functioning and prevent potential issues such as component movement or dislodgment during vehicle operation. This stability is crucial for maintaining the integrity of the fuel system, minimizing the risk of fuel leaks or malfunctions that could compromise vehicle safety and performance.
[00057] The versatility of the support structures allows for customization and adaptation to various system configurations and component requirements. Whether mounting the ROV stem directly or accommodating additional EVAP components, or cable routing within the vehicle, the support structures offer flexibility in installation and configuration. This adaptability ensures compatibility with different vehicle models, system layouts, and component sizes, enhancing the applicability and scalability of the invention across a range of vehicle platforms. Further, the features of the support structures, such as the adjustable holding portion and multiple stay portions, optimize material usage while maintaining structural integrity. By utilizing smaller diameter stay portions instead of a single larger diameter, the support structures reduce material requirements without compromising strength or rigidity. This not only contributes to cost savings but also promotes environmental sustainability by minimizing material waste. Furthermore, the inclusion of features like snap-fit connections and adjustable fitment provisions enhances ease of installation, maintenance, and replacement, reducing downtime and enhancing overall operational efficiency.
[00058] The advantage of the support structure lies in its ability to achieve a delicate balance between rigidity and flexibility within a single component, thereby eliminating the necessity for multiple parts. This characteristic is made possible by the intentional selection of materials with different strength moduli for constructing the support structure. By utilizing materials with varying mechanical properties, such as elastic modulus, the support structure can exhibit both the stiffness required for stability and the flexibility needed for adaptability. Consequently, the support structure can effectively withstand external forces and environmental conditions while accommodating minor variations in component dimensions or system requirements. This integrated approach not only simplifies the configuration and manufacturing process but also enhances the overall efficiency and reliability of the support structure within diverse applications.
[00059] The support structure incorporates a detachable engagement mechanism for its engaging portion with the fuel tank directly. This feature eliminates the need for additional processes such as welding or fasteners typically used for securing support structures in place. Instead, the engaging portion of the support structure seamlessly integrates with the fuel tank, facilitating easy installation and removal without the requirement for specialized equipment or labour-intensive techniques. This streamlined approach not only reduces assembly time and complexity but also minimizes the risk of damage to the fuel tank or surrounding components during installation or maintenance procedures.
[00060] The above-described embodiments, and particularly any “preferred” embodiments, are possible examples of implementations and merely set forth for a clear understanding of the principles of the invention. It will be apparent to those skilled in the art that changes in form, connection, and detail may be made therein without departing from the spirit and scope of the invention.
[00061] Non-limiting and non-exhaustive embodiments of the invention are described with reference to the following figures, wherein like reference numerals refer to like parts throughout the various views unless otherwise specified. It should be appreciated that the following figures may not be drawn to scale.
[00062] The foregoing disclosure is not intended to limit the present disclosure to the precise forms or particular fields of use disclosed. As such, it is contemplated that various alternate embodiments and/or modifications to the present disclosure, whether explicitly described or implied herein, are possible in light of the disclosure. Having thus described embodiments of the present disclosure, a person of ordinary skill in the art will recognize that changes may be made in form and detail without departing from the scope of the present disclosure. Therefore, it is intended that the present invention is not limited to the particular embodiment disclosed, but that the present invention will include all embodiments falling within the scope of the appended claims.
[00063] In the foregoing specification, the disclosure has been described with reference to specific embodiments. However, as one skilled in the art will appreciate, various embodiments disclosed herein can be modified or otherwise implemented in various other ways without departing from scope of the disclosure. Accordingly, this description is to be considered as illustrative and is for the purpose of teaching those skilled in the art the manner of making and using various embodiments of the disclosure. It is to be understood that the forms of disclosure herein shown and described are to be taken as representative embodiments. Equivalent elements, materials, processes or steps may be substituted for those representatively illustrated and described herein. Moreover, certain features of the disclosure may be utilized independently of the use of other features, all as would be apparent to one skilled in the art after having the benefit of this description of the disclosure. Expressions such as “including”, “comprising”, “incorporating”, “consisting of”, “have”, “is” used to describe and claim the present disclosure are intended to be construed in a non-exclusive manner, namely allowing for items, components or elements not explicitly described also to be present. Reference to the singular is also to be construed to relate to the plural.
, Claims:We Claim:

1. A support structure (200) for securing components, the support structure (200) comprising:
a fitment portion (200A), the fitment portion (200A) comprising at least one fitment protrusion (202);
a holding portion (200B), the holding portion (200B) comprising plurality of fitment provisions (204); and
a stay portion (200C), the stay portion (200C) comprising at least two arms (206, 212);
wherein, the fitment portion (200A) is configured to pass within an insertion region (218) and to connect the at least one fitment protrusion (202) with at least one of the plurality of fitment provisions (204), and
wherein the insertion region (218) is defined between the at least two arms (206, 212) of the stay portion (200C).

2. The support structure (200) as claimed in claim 1, wherein the holding portion (200B) is disposed between the fitment portion (200A) and the stay portion (200C);
wherein the fitment portion (200A), the holding portion (200B) and the stay portion (200C) are integrally connected; and
wherein a width of the fitment portion (200A) is always less than width of the insertion region (218).

3. The support structure (200) as claimed in claim 1, wherein the at least two arms (206, 212) are originated from an intersection point of the holding portion (200B) and the stay portion (200C) of the support structure (200); and
wherein opposite ends (210, 216) of the at least two arms (206, 212) comprising one or more engaging ends (208A, 208B, 214A, 214B).

4. The support structure (200) as claimed in claim 3, wherein the one or more engaging ends (208A, 208B, 214A, 214B) of the at least two arms (206, 212) are configured to detachably abut with openings (304, 306) present in a surface (302).

5. The support structure (200) as claimed in claim 4, wherein an engagement between the one or more engaging ends (208A, 208B, 214A, 214B) of the at least two arms (206, 212) and the openings (304, 306) in the surface (302) is enabled by snap-fit connections.

6. The support structure (200) as claimed in claim 1, wherein the fitment portion (200A) and the holding portion (200B) are configured to encircle the securing components, and wherein adjustment of the holding portion (200B) is enabled based on a diameter of the securing components.

7. The support structure (200) as claimed in claim 1, wherein the at least one fitment protrusion (202) are distributed along circumference of the fitment portion (200A) and the plurality of fitment provisions (204) are distributed along circumference of the holding portion (200B).

8. The support structure (200) as claimed in claim 1, wherein the support structure (200) is composed of at least two distinct materials; and wherein the material of the stay portion (200C) exhibits a higher elastic modulus than the material of the holding portion (200B).

9. A method for securing components within a surface (302) using a support structure (200), the method comprising steps of:
passing, a fitment portion (200A) of the support structure (200) through an insertion region (218), the insertion region (218) is defined between at least two arms (206, 212) of a stay portion (200C);
connecting, at least one fitment protrusion (202) of the fitment portion (200A) with at least one of a plurality of fitment provisions (204) of a holding portion (200B);
positioning, the support structure (200) within the surface (302) using one or more engaging ends (208A, 208B, 214A, 214B) of the at least two arms (206, 212); and
abutting the support structure (200) with openings (304, 306) present in the surface (302).

10. The method as claimed in claim 9, wherein encircling the securing components with the fitment portion (200A) and the holding portion (200B) of the support structure (200).

11. The method as claimed in claim 9, wherein flexibly adjusting the plurality of fitment provisions (204) of the holding portion (200B) based on a diameter of the securing components.