Sign In to Follow Application
View All Documents & Correspondence

Unmanned Aerial Vehicle With Pivoting Joints For Spraying Agrochemicals

Abstract: Exemplary embodiments of the present disclosure are directed towards a method for spraying agrochemicals, comprising an unmanned aerial vehicle (UAV) spraying agrochemicals through pivoting joints and adjustable nozzle bars. The UAV features arms connected to these nozzle bars via pivoting joints, allowing flexible extraction and retraction. Locking pins secure the bars in various positions, facilitating swath width manipulation for precise spraying. These pivotal joints enable selective folding and locking, adapting to diverse operational needs and storage constraints. The pivoting joint design minimizes space while enhancing ease in the agrochemicals application. The locking pin functionality empowers users to control spraying angles, achieving multi-directional coverage. The UAV employs stoppers with adjustable locking elements to prevent damage during transportation while providing shock absorption features. Fig. 2

Get Free WhatsApp Updates!
Notices, Deadlines & Correspondence

Patent Information

Application #
Filing Date
22 January 2024
Publication Number
06/2024
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
Parent Application

Applicants

MARUT DRONETECH PRIVATE LIMITED
Door No 2-53/23/2/1, T- Hub Foundation, Himalaya Block- D, IIIT, Gachibowli, Rangareddy, Telangana. 500032, India.

Inventors

1. PREM KUMAR VISLAWATH
H.No. 6-89, Plot No. 5, SLNS Colony, Meerpet, Saroornagar, Rangareddy, Telangana-500079, India.
2. PEDDI SURAJ
H.No. 1-5-203/3/6, Ganesh Nagar, Jagtial, Telangana. 505327, India.

Specification

Description:TECHNICAL FIELD
[001] The present disclosure generally relates to the field of UAV (Unmanned Aerial Vehicle) technology. More particularly, the present disclosure relates to the unmanned aerial vehicle with pivoting joints for spraying agrochemicals.

BACKGROUND
[002] The utilization of Unmanned Aerial Vehicles (UAVs) equipped with spraying mechanisms has become integral in modern agriculture and various industrial applications. These UAVs play a crucial role in ensuring efficient and precise distribution of liquids, such as pesticides, fertilizers, or disinfectants. However, the current designs of spraying drones encounter several challenges that significantly impact their overall effectiveness, reliability, and maintenance costs.

[003] One of the critical issues faced by existing spraying drones is the vulnerability of their nozzle tips. During non-operational phases, the protruding nozzles are susceptible to damage, leading to increased maintenance costs and the need for frequent replacement of damaged nozzle components. This issue directly affects the efficiency of the spraying process.

[004] Additionally, the orientation of spraying nozzles in conventional UAVs is often undetermined, resulting in inefficiencies in the spraying pattern. The lack of a standardized orientation leads to suboptimal coverage of the target area, diminishing the overall effectiveness of the spraying operation.

[005] UAVs with downward-folding arms encounter challenges related to the free movement of these folding arms. During handling, transportation, or deployment, the folding arms may inadvertently hit surrounding structures, causing damage to the nozzle bars and adjacent components. This not only affects the functionality of the spraying drone but also contributes to increased service and maintenance costs. Current solutions available in the market inadequately address these critical issues. The absence of a protective mechanism for nozzle tips, coupled with undetermined nozzle orientations and potential structural damage, hampers the overall efficiency and reliability of spraying drones.

[006] In light of these challenges and limitations, there exists a pressing need for an innovative solution that ensures the protection of nozzle tips during non-operational phases, establishes a standardized and optimized orientation for spraying nozzles, and prevents structural damage caused by downward-folding arms.

SUMMARY
[007] The following presents a simplified summary of the disclosure in order to provide a basic understanding to the reader. This summary is not an extensive overview of the disclosure and it does not identify key/critical elements of the invention or delineate the scope of the invention. Its sole purpose is to present some concepts disclosed herein in a simplified form as a prelude to the more detailed description that is presented later.

[008] Exemplary embodiments of the present disclosure are directed towards folding nozzle bar mechanism for unmanned aerial vehicle spraying.

[009] Another objective of the present disclosure is directed towards a folding mechanism is designed for even and wide spraying swath in UAVs, optimizing spray coverage.

[0010] Another objective of the present disclosure is directed towards multi-directional nozzle bar folding, the mechanism includes two or more folding joints with a locking system, enabling manipulation of swath width and adjustable spraying angles.

[0011] Another objective of the present disclosure is directed towards the folding design reduces space requirements, enhancing operational ease during UAV deployment.

[0012] Another objective of the present disclosure is directed towards safeguards the nozzle tip, increasing its lifespan and preventing damage that could lead to malfunction.

[0013] Another objective of the present disclosure is directed towards lightweight, agile, and robust materials are used, reducing vibrations during spraying operations.

[0014] Another objective of the present disclosure is to prevent damage by resisting and locking UAV arms in two degrees of freedom, thereby maintaining structural integrity.

[0015] Another objective of the present disclosure is directed towards increasing efficiency in the spraying operation.

[0016] Another objective of the present disclosure is directed towards optimizing use of nozzles leading to an extended lifetime.

[0017] Another objective of the present disclosure is directed towards increasing strength and restricting degrees of freedom to the UAV arm.
[0018] Another objective of the present disclosure is directed towards shields nozzles from wear, tear, and shocks during rough handling.

[0019] Another objective of the present disclosure is directed towards implemented an adjustable locking material to restrict degrees of freedom.

[0020] Another objective of the present disclosure is directed towards maintained structural integrity during adverse handling and transportation.

[0021] Another objective of the present disclosure is directed towards all industrial applications involving unmanned aerial vehicle spraying.

[0022] Another objective of the present disclosure is directed towards reducing health risks associated with agrochemicals exposures for workers through the use of an unmanned aerial vehicle to spray agrochemicals.

[0023] According to other exemplary aspect, an unmanned aerial vehicle with pivoting joints for spraying agrochemicals, includes arms attached to one or more nozzle bars by one or more pivoting joints, wherein the one or more pivoting joints providing flexibility for extraction and retraction of the one or more nozzle bars.

[0024] According to another exemplary aspect, locking pins configured to secure the one or more nozzle bars at a extraction position and a retraction position.

[0025] According to another exemplary aspect, the nozzle bar comprises two or more pivoting joints with the locking mechanism facilities manipulation of the swath width of the spray.

[0026] According to another exemplary aspect, the pivoting joints are configured to allow the nozzle bar to be selectively folded and locked in an open or closed position, providing adaptability to varying operational requirements and storage conditions.

[0027] According to another exemplary aspect, pivoting joint is configured to reduce the space and helps in ease of spraying agrochemicals.

[0028] According to another exemplary aspect, the locking pin enables the user to control the spraying angle and achieve multi-directional spraying.

[0029] According to another exemplary aspect, the arms are attached to the unmanned aerial vehicle through one or more stoppers.

[0030] According to another exemplary aspect, the stoppers configured to resist and lock the one or more arms in two degrees of freedom, thereby preventing damage during handling and transportation.

[0031] According to another exemplary aspect, the stopper is coupled to adjustable locking element configured to restrict both degrees of freedom by maintaining structural integrity during adverse handling and transportation.

[0032] According to another exemplary aspect, the stopper comprises shock absorbing features.

[0033] According to another exemplary aspect, a method for spraying agrochemicals using unmanned aerial vehicle, includes enabling a user to spray Agrochemicalsby extracting the nozzle bar of the unmanned aerial vehicle.
[0034] According to another exemplary aspect, enabling the user to adjust a locking pin to extract the nozzle bar from the arm of the unmanned aerial vehicle.

[0035] According to another exemplary aspect, spraying agrochemicals using the extracted nozzle bar.

[0036] According to another exemplary aspect, enabling the user to manipulate the swath width of the spray by adjusting the locking pin.

[0037] According to another exemplary aspect, enabling the user to retract the nozzle bar by adjusting the locking pin after spraying the agrochemicals.

BRIEF DESCRIPTION OF THE DRAWINGS
[0038] In the following, numerous specific details are set forth to provide a thorough description of various embodiments. Certain embodiments may be practiced without these specific details or with some variations in detail. In some instances, certain features are described in less detail so as not to obscure other aspects. The level of detail associated with each of the elements or features should not be construed to qualify the novelty or importance of one feature over the others.

[0039] FIG. 1 is an example block diagram depicting a schematic representation of an unmanned aerial vehicle with pivoting joints for spraying agrochemicals, in accordance with one or more exemplary embodiments.

[0040] FIG. 2 is an example block diagram depicting a schematic representation of extraction of the nozzle bar of the unmanned aerial vehicle for spraying, in accordance with one or more exemplary embodiments.

[0041] FIG. 3 is an example block diagram depicting a schematic representation of retraction of the nozzle bar of the unmanned aerial vehicle for spraying, in accordance with one or more exemplary embodiments.

[0042] FIG. 4A is an example block diagram depicting a schematic representation of unmanned aerial vehicle with arm stopper, in accordance with one or more exemplary embodiments.

[0043] FIG. 4B is an example block diagram in detail view of the unmanned aerial vehicle arm stopper, in accordance with one or more exemplary embodiments.

[0044] FIG. 5 is an example block diagram depicting a schematic representation of locking element and stopper of the unmanned aerial vehicle, in accordance with one or more exemplary embodiments.

[0045] FIG. 6 is an example flow diagram depicting a method for spraying agrochemicals using unmanned aerial vehicle, in accordance with one or more exemplary embodiments.

DETAILED DESCRIPTION OF EXAMPLE EMBODIMENTS
[0046] It is to be understood that the present disclosure is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the drawings. The present disclosure is capable of other embodiments and of being practiced or of being carried out in various ways. Also, 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.

[0047] The use of “including”, “comprising” or “having” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. The terms “a” and “an” herein do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced item. Further, the use of terms “first”, “second”, and “third”, and the like, herein do not denote any order, quantity, or importance, but rather are used to distinguish one element from another.

[0048] Referring to FIG. 1 is an example block diagram 100 depicting a schematic representation of an unmanned aerial vehicle with pivoting joints for spraying agrochemicals, in accordance with one or more exemplary embodiments.

[0049] The unmanned aerial vehicle may be employed in agricultural environments to potentially deliver one or more agricultural products to land where crops are growing. Agricultural products may include water, pesticides, fertilizer, seeds, engineered soil, compost, or any other product that may be configured to potentially promote or aid in the production of one or more plant species.

[0050] The unmanned aerial vehicle includes arms 102, a propeller 104, a pipe 106, a nozzle bar 108, a tank 110, a pivoting joint (as shown in FIG.2), a locking pin(as ashown in FIG.2). The nozzle bar 108 may be coupled to the unmanned aerial vehicle through the pivoting joints. The pivoting joints where the nozzle bar is attached, The nozzle bar 108 pivoting joint provides the flexibility for movement, allowing the nozzle bar to be extended or retracted. The pivoting joint may be designed to facilitate the extraction or retraction of the nozzle bars when they are not actively spraying. This pivoting joint mechanism likely contributes to reducing the risk of damage during non-operational periods. Here extraction may be unfolding and rectration may be folding.

[0051] One or more propellers 104 may be attached to the arms of the unmanned aerial vehicle. The one or more propellers 104 may be configured to assist in flying the unmanned aerial vehicle. The tank (110) is configured to store the liquid form of agrochemicals. This agrochemicals can be supplied to the nozzle bar through pipes. The pipe 106 may includes but not limited to plastic tubes, this pipe 106 may be multiple pipes and arranged to evry nozzle bar to supply the agrochemicals. For example Fertilizers.

[0052] The nozzle bar 108 may be attached/joint to unmanned aerial vehicle arms 102 using locking pin (as shown in FIG.2). The locking pin may be configured to the retraction and the extraction of the nozzle bar from the unmanner aerial vehicle arms. The nozzle bar 108 pivoting joints (ex: foldings) may be designed in a way that it has two or more folding joints and locking mechanism for closing and opening. Nozzle bar 108 pivoting joints (ex: folding) may be configured to enable the user to adjust and manipulate the swath width of the spray. The unmanned aerial vehicle 100 may include drones and like.

[0053] In accordance with present disclosure, the unmanned aerial vehicle may be configured to spary the agrochemicals may include but not limited to ferilizers, natural or artificial substance containing the chemical elements that improve growth and productiveness of plants/crops. The agrochemicals enhance the natural fertility of the soil or replace chemical elements taken from the soil by previous crops.

[0054] In accordance with the present disclosure, the unmanned aerial vehicle may be configured to spray agrochemicals in areas (e.g., water bodies, flat surfaces) prone to vector-borne diseases. This includes the control of mosquitoes that carry diseases such as malaria, Zika, or dengue, contributing to public health efforts.

[0055] In accordance with the present disclosure, the unmanned aerial vehicle may be configured to spray agrochemicals. The unmanned aerial vehicle may be operated remotely by the user.

[0056] Referring to FIG. 2 is an example block diagram 200 depicting a schematic representation of extraction of the nozzle bar of the unmanned aerial vehicle for spraying, in accordance with one or more exemplary embodiments. The nozzle bar 108 pivoting joint 201 may be a pivotal connection point, where the nozzle bar 108 is attached to arms of the unmanned aerial vehicle.

[0057] The nozzle bar 108 may be attached/joint to unmanned aerial vehicle arms using locking pin 202. The locking pin 202 may be configured to the retraction and the extraction of the nozzle bar 108 from the unmanner aerial vehicle arms. The nozzle bar 108 may be configured to adjust the spraying angle and multi directional.

[0058] The nozzle bar 108 may be complemented by a locking pin that enables the nozzle bar 108 to be securely locked in a closed position, i.e., retraction the nozzle bar 108 through pivoting joints 201 and opened i.e extraction the nozzle bar from the arm of the unmmaned aerial vehicle when needed.

[0059] Referring to FIG. 3 is an example block diagram 300 depicting a schematic representation of retraction of the nozzle bar of the unmanned aerial vehicle for spraying, in accordance with one or more exemplary embodiments. The locking pin 202 may be configured to enables the nozzle bar 108 and opened i.e extraction the nozzle bar 108 pivoting joint 201 from the arm 102 of the unmmaned aerial vehicle when needed.

[0060] Referring to FIG. 4A is an example block diagram 400a depicting a schematic representation of unmanned aerial vehicle with arm stopper, in accordance with one or more exemplary embodiments. The unmanned aerial vehicle may includes arms 102 and arm stopper 402.

[0061] The stopper 402 may be coupled to the unmanned aerial vehicle arm 102. The stopper 402 may be restricted to unneccery degrees of freedom, enhancing structural integrity and preventing damage during handling and transportation. The arm 102 downward folding stopper helps the arm 102 to resist and lock in two degrees of freedom. The stopper 402 may be configured to arms downward securely,preventing unintended movements.

[0062] Referring to FIG. 4B is an example block diagram 400b in detail view of the unmanned aerial vehicle arm stopper, in accordance with one or more exemplary embodiments.

[0063] Referring to FIG. 5 is an example block diagram 500 depicting a schematic representation of locking element and stopper of the unmanned aerial vehicle, in accordance with one or more exemplary embodiments.

[0064] The diagram 500 includes arm 102, a arm stopper 402, an adjustable locking element 502. The adjustable locking element 502 may be round-shaped or without any specific shape limitation. The adjustable locking element 502 may be made of any suiatable material. The adjustable locking element 502 coupled to the arm stopper 402. The arm stopper 402 with the adjustable locking element 502 may be configured to restrict the both the degrees of freedom by maintaining the structural integrity even in cases of adverse handling and transportation. The both degrees of freedom means two independent directions or axes in which the unammaned aerial vehicles arm can move. The folding arm stopper may be designed to restrict or limit movement along these two degrees of freedom, ensuring that the unmanned aerial vehicle arm or arms 102 remains securely in place and maintains its structural integrity, especially during adverse handling and transportation.

[0065] Referring to FIG. 6 is an example flow diagram 600 depicting a method for spraying Agrochemicals using unmanned aerial vehicle, in accordance with one or more exemplary embodiments.

[0066] The exemplary method 600 commences at step 602, enabling the user to spray agrochemicals by extracting the nozzle bar of the unmanned aerial vehicle. Thereafter, at step 604, enabling the user to extract the nozzle bar by adjusting the locking pin. Therafter at step 606, the user sprays agrochemicals using the extracted nozzle bar of the unmanned aerial vehicle. Therafter at step 608, enabling the user to manipulate the swath width of the spray. Therafter at step 610, enabling the user to retract the nozzle bar by adjusting the locking pin after the user has sprayed the agrochemicals.

[0067] The use of “including”, “comprising” or “having” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. The terms “a” and “an” herein do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced item. Further, the use of terms “first”, “second”, and “third”, and the like, herein do not denote any order, quantity, or importance, but rather are used to distinguish one element from another.

[0068] Reference throughout this specification to “one embodiment”, “an embodiment”, or similar language means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the present disclosure. Thus, appearances of the phrases “in one embodiment”, “in an embodiment” and similar language throughout this specification may, but do not necessarily, all refer to the same embodiment.

[0069] Although the present disclosure has been described in terms of certain preferred embodiments and illustrations thereof, other embodiments and modifications to preferred embodiments may be possible that are within the principles of the invention. The above descriptions and figures are therefore to be regarded as illustrative and not restrictive.

[0070] Thus, the scope of the present disclosure is defined by the appended claims and includes both combinations and sub-combinations of the various features described hereinabove as well as variations and modifications thereof, which would occur to persons skilled in the art upon reading the foregoing description.

, Claims:We Claim

1. An unmanned aerial vehicle with pivoting joints for spraying agrochemicals, comprising:

one or more arms attached to one or more nozzle bars by one or more pivoting joints, wherein the one or more pivoting joints providing flexibility for extraction and retraction of the one or more nozzle bars;

one or more locking pins configured to secure the one or more nozzle bars at a extraction position and a retraction position;

the nozzle bar comprises two or more pivoting joints with the locking mechanism facilities manipulation of the swath width of the spray;

2. The unmanned aerial vehicle as claimed in claim 1, wherein the pivoting joints are configured to allow the nozzle bar to be selectively folded and locked in an open or closed position, providing adaptability to varying operational requirements and storage conditions.

3. The unmanned aerial vehicle as claimed in claim 1, pivoting joint is configured to reduce the space and helps in ease of spraying the agrochemicals.

4. The unmanned aerial vehicle as claimed in claim 1, wherein the locking pin enables the user to control the spraying angle and achieve multi-directional spraying.

5. The unmanned aerial vehicle as claimed in claim 1, wherein the one or more arms are attached to the unmanned aerial vehicle through one or more stoppers.

6. The unmanned aerial vehicle as claimed in claim 5,wherein the one or more stoppers configured to resist and lock the one or more arms in two degrees of freedom, thereby preventing damage during handling and transportation.

7. The unmanned aerial vehicle as claimed in claim 5, wherein the stopper is coupled to adjustable locking element configured to restrict both degrees of freedom by maintaining structural integrity during adverse handling and transportation.

8. The unmanned aerial vehicle as claimed in claim 5, wherein the stopper comprises shock absorbing features.

9. A method for spraying agrochemicals using unmanned aerial vehicle, comprising:

enabling a user to spray the agrochemicals by extracting the nozzle bar of the unmanned aerial vehicle;

enabling the user to adjust a locking pin to extract the nozzle bar from the arm of the unmanned aerial vehicle;

spraying agrochemicals using the extracted nozzle bar;

enabling the user to manipulate the swath width of the spray by adjusting the locking pin; and

enabling the user to retract the nozzle bar by adjusting the locking pin after spraying the agrochemicals.

10. The method as claimed in claim 9, wherein the pivoting joints are configured to allow the nozzle bar to be selectively folded and locked in an open or closed position, providing adaptability to varying operational requirements and storage conditions.

Documents

Application Documents

# Name Date
1 202441004319-STATEMENT OF UNDERTAKING (FORM 3) [22-01-2024(online)].pdf 2024-01-22
2 202441004319-STATEMENT OF UNDERTAKING (FORM 3) [22-01-2024(online)]-1.pdf 2024-01-22
3 202441004319-REQUEST FOR EARLY PUBLICATION(FORM-9) [22-01-2024(online)].pdf 2024-01-22
4 202441004319-POWER OF AUTHORITY [22-01-2024(online)].pdf 2024-01-22
5 202441004319-FORM-9 [22-01-2024(online)].pdf 2024-01-22
6 202441004319-FORM FOR STARTUP [22-01-2024(online)].pdf 2024-01-22
7 202441004319-FORM FOR SMALL ENTITY(FORM-28) [22-01-2024(online)].pdf 2024-01-22
8 202441004319-FORM 1 [22-01-2024(online)].pdf 2024-01-22
9 202441004319-EVIDENCE FOR REGISTRATION UNDER SSI(FORM-28) [22-01-2024(online)].pdf 2024-01-22
10 202441004319-EVIDENCE FOR REGISTRATION UNDER SSI [22-01-2024(online)].pdf 2024-01-22
11 202441004319-DRAWINGS [22-01-2024(online)].pdf 2024-01-22
12 202441004319-DECLARATION OF INVENTORSHIP (FORM 5) [22-01-2024(online)].pdf 2024-01-22
13 202441004319-COMPLETE SPECIFICATION [22-01-2024(online)].pdf 2024-01-22