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Disc Based Multi Net Launcher Mechanism

Abstract: ABSTRACT The high-speed disc-based net launcher presents a novel solution for capturing drones and other aerial targets with precision and efficiency. Comprising a motor-driven spindle, a disc embedded with an interwoven net (144), and servo mechanisms for controlled release, the launcher operates through a sequence of coordinated steps. Upon activation, the motor-driven spindle facilitates disc loading and release, propelling the net towards the targeted drone with centrifugal force. Equidistantly attached weights along the disc's outer rim provide stability and ensure timed net deployment. Programmable spindle speed allows for variable targeting distances, enhancing versatility. The launcher's nondestructive approach minimizes collateral damage and complies with regulatory frameworks. With applications in security, wildlife management, and law enforcement, the high-speed disc-based net launcher offers a precise and versatile solution for addressing concerns related to unauthorized drone activities. Figure associated with Abstract is Fig. 1

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Notices, Deadlines & Correspondence

Patent Information

Application #
Filing Date
18 March 2024
Publication Number
15/2024
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
Parent Application

Applicants

ZEBU INTELLIGENT SYSTEMS PRIVATE LIMITED
6th Floor, DGS Prime, Siddhi Vinayak Nagar, Madhapur, Hyderabad, Telangana 500081

Inventors

1. Santosh Balajee Banisetty
6th Floor, DGS Prime, Siddhi Vinayak Nagar, Madhapur, Hyderabad, Telangana 500081
2. Stalin Kanagaraj
6th Floor, DGS Prime, Siddhi Vinayak Nagar, Madhapur, Hyderabad, Telangana 500081

Specification

DESC:DESCRIPTION
Technical Field of the Invention

The present invention relates to a field of net gun technology, specifically focusing on high-speed disc-based net launchers for capturing drones and other aerial targets.

Background of the Invention

The rapid proliferation of unmanned aerial vehicles (UAVs) has prompted a critical reassessment of drone interception methodologies. Traditional interception approaches often involve destructive means, leading to concerns about collateral damage and safety hazards. As the utilization of drones continues to expand across various sectors, the need for nondestructive and highly effective countermeasures becomes paramount.

The response to this emerging threat has taken various forms. Radio frequency (RF) jamming disrupts the drone's control and navigation signals, while geofencing creates virtual barriers that drones are programmed to avoid. Both methods have limitations, with RF jamming risking interference with essential communications and geofencing being circumvented by more sophisticated drones. Kinetic solutions, such as shooting down the drone, are even more problematic due to the high risk of collateral damage.

In this context, net-based solutions have emerged as a favored alternative for UAV interception. These solutions offer a nondestructive method of containment, mitigating risks associated with traditional interception techniques. The adoption of net-based capture aligns with evolving regulatory frameworks, ethical considerations, and the imperative to safeguard public spaces from unauthorized drone activities.

A current challenge with net-based capture is the need to reload nets and reset the different systems within after each use. Recognizing this, the proposed Nondestructive Drone Capture mechanism introduces a sequential net deployment system coupled with parachute landing for each, allowing authorities to handle multiple rogue drones in a single operational cycle. This innovative solution offers a controlled and effective means of intervention of multiple drones, facilitating the safe retrieval of said captured drones for further investigation and analysis.

Several patents have been issued for drone interception devices, yet each exhibits significant limitations. For instance, a system equipped with multiple net launchers on a rotating platform (US10005556B2) has been developed. While it represents a step towards non-destructive interception, the system's complexity and bulk potentially limit its agility and response time. Moreover, it could inadvertently become entangled, causing damage to both the interceptor and the target.

Another patented invention (KR102152739B1) introduces a drone carrying a chain-type carbon fiber net. Although innovative, this approach could lead to unpredictable outcomes due to difficulties in controlling the net's deployment. Additionally, the system's mechanical trigger mechanism may lack the responsiveness required for dynamic interception scenarios.

A more sophisticated acquisition system for rotor wing UAVs (CN109443097A) integrates a missile launcher with a net and advanced targeting systems. Despite its precision capabilities, the inherent risks associated with launching a projectile in populated areas or near sensitive infrastructure can't be ignored. The system's complexity and the potential for misfires further complicate its practical implementation.

The limitations of existing technologies underscore the urgent need for an improved solution. A method that is nondestructive, precise, and capable of quick deployment is essential in today's environment, where the risks associated with drones are ever-increasing. Any new solution must prioritize safety, minimize the potential for collateral damage, and ensure compliance with stringent regulatory standards.

In light of these considerations, the inventor proposes a high-speed disc-based net launcher for drone capture that addresses the drawbacks of existing methods. The invention focuses on a motor-driven spindle that propels a disc embedded with a net at high velocity, ensuring a targeted and controlled interception. Unlike previous inventions, this design prioritizes the safe neutralization of drones with minimal risk of collateral damage.

The innovative net launcher offers several advantages over prior arts. Its precision and control significantly reduce the risks associated with intercepting drones. The system's design allows for the net to be deployed in a manner that envelops the target drone without causing harm to the surroundings, including people, property, or the drone itself. This is particularly important in scenarios where the drone may be inadvertently operating in restricted airspace.

Moreover, the proposed system is designed to be adaptable and adjustable, capable of being mounted on various platforms and readily reconfigured to address different drone threats. Its modularity and ease of use make it suitable for a range of environments, from urban to rural, and for users with varying levels of expertise.

The nondestructive nature of the drone capture system ensures compliance with emerging laws and regulations governing UAVs. By immobilizing rather than destroying the drone, the system allows for the possibility of retrieving valuable forensic data from the captured drone, which could be critical in investigating and preventing future unauthorized drone usage.

The introduction of the high-speed disc-based net launcher marks a significant leap forward in the field of UAV interception technology. By addressing the need for a method that is both effective and nondestructive, the invention stands to make a substantial impact on the market. It provides an innovative solution to the ever-growing challenges presented by unauthorized drone operations, enhancing safety and security in the modern world.

Brief Summary of the Invention

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.

According to an aspect of the present invention, a high-speed disc-based net launcher is disclosed. The high-speed disc-based net launcher marks a significant leap forward in the realm of aerial interception technologies, particularly in addressing the challenges posed by the unauthorized use of Unmanned Aerial Vehicles (UAVs) or drones.

The first object of this invention is to provide a system that can capture drones and other aerial targets without causing any collateral damage. This aspect is crucial in urban environments and sensitive ecological zones where the risk of collateral damage must be minimized to protect both property and wildlife. The second object of the invention focuses on the precision and accuracy of the system. It is designed to target and capture drones with a high degree of reliability, ensuring that the interception process does not endanger the surrounding environment or the people within it.

A further object of this invention is to offer a nondestructive means of drone interception. Unlike conventional methods that may destroy or significantly damage the target, this system aims to preserve the integrity of the captured drone, allowing for potential forensic analysis and the retrieval of valuable information regarding unauthorized drone operations.

At the heart of the invention is a motor-driven spindle that powers a disc embedded with an interwoven net, poised for launch towards an aerial target. This component of the invention is critical for achieving the desired precision in capturing drones. The system operates through a sequence of well-coordinated steps beginning with the activation of the motor-driven spindle. As the spindle achieves the necessary rotational speed, it facilitates the loading of the disc, which is then released at an optimal moment determined by servo mechanisms integral to the system's design. This release mechanism is finely tuned to ensure the disc is propelled with sufficient force and accuracy towards the target. Upon release, the disc's trajectory is stabilized by weights strategically placed along its rim, harnessing centrifugal force to unfold the net in a controlled manner, thereby enveloping the target without risking entanglement or damage to the surroundings.

The invention stands out for its versatility, offering broad applications across various sectors. In security and surveillance, it serves as an effective countermeasure against potential threats posed by drones, such as unauthorized surveillance or contraband delivery. Wildlife management can also benefit from this technology, as it provides a means to protect sensitive ecological zones from disturbances caused by drones, ensuring the safety of wildlife without resorting to harmful measures. Law enforcement agencies can leverage the system to safely disable drones used in criminal activities, preserving the drone for evidence collection and analysis. This wide range of applications underscores the system's adaptability to different operational needs and environments.

One of the paramount advantages of this system is its nondestructive approach to drone interception. By capturing the drone intact, the system not only minimizes potential damage to the drone and its surroundings but also aligns with ethical standards and regulatory frameworks governing UAV operations. This aspect is particularly important in scenarios where the drone may inadvertently or unknowingly enter restricted airspace, and its recovery is essential for investigative purposes. Furthermore, the system's design emphasizes safety, ensuring that the process of intercepting and neutralizing a drone does not pose additional risks to bystanders or property. This safety feature is complemented by the system's operational efficiency, which allows for rapid deployment and response to unauthorized drone activities, a critical factor in situations requiring immediate action.

The precision and control inherent in the system's design also represent significant advancements over existing interception methods. Traditional approaches often lack the ability to accurately target and capture drones, leading to missed captures or unintended consequences. The high-speed disc-based net launcher, however, utilizes a combination of mechanical and electronic components to achieve a level of accuracy that significantly reduces such risks. This precision is further enhanced by the system's ability to adjust the motor-driven spindle's speed, accommodating various distances and ensuring the net is deployed at the optimal moment for capture.

Another noteworthy feature of the invention is its ease of use. Despite the system's sophisticated design, it requires minimal training to operate, making it accessible to a wide range of users across different sectors. This ease of use does not compromise the system's effectiveness, as it maintains a high level of performance in capturing drones, thanks to its innovative design and operational features.

In summary, the high-speed disc-based net launcher presents a comprehensive solution to the challenges posed by unauthorized drone usage. Its design and operation reflect a deep understanding of the needs and constraints inherent in drone interception tasks. By offering a system that is precise, nondestructive, and versatile, this invention sets a new standard in aerial interception technologies. Its applications span security, wildlife management, and law enforcement, providing these sectors with an effective tool to manage the risks associated with unauthorized drone activities. The system's advantages, including its safety features, operational efficiency, and ease of use, further solidify its position as a significant advancement in the field, promising to make a substantial impact on how drones are monitored and controlled in various operational contexts.

Further objects, features, and advantages of the invention will be readily apparent from the following description of the preferred embodiments thereof, taken in conjunction with the accompanying drawings.

Brief Description of the Drawings

The above and other objects, features and advantages of the invention will become apparent from a consideration of the following detailed description presented in connection with the accompanying drawings in which:

Fig 1 (a) illustrates the front view of block diagram of disk based net launcher, in accordance with an exemplary embodiment of the present invention;

Fig 1 (b) illustrates the isometric view of block diagram of disk based net launcher, in accordance with an exemplary embodiment of the present invention;

Fig 1 (c) illustrates the isometric view of block diagram of disk based net launcher, in accordance with an exemplary embodiment of the present invention;

Fig 2 (a) illustrates the block diagram of Single disk configuration inside disk cartridge, in accordance with an exemplary embodiment of the present invention;

Fig 2 (b) illustrates the block diagram of Multi-Disk Stack without disk cartridge Front view, in accordance with an exemplary embodiment of the present invention;

Fig 2 (c) illustrates the block diagram of Multi-Disk Stack without Disk Cartridge Isometric View, in accordance with an exemplary embodiment of the present invention;

Fig 2 (d) illustrates the block diagram of Multi-Disk Stack inside Disk Cartridge, in accordance with an exemplary embodiment of the present invention;

Fig 3 (a-c) illustrates the block diagrams of launch plate detachable from the holster and fit in the slot of the launch track in multiple angles, in accordance with an exemplary embodiment of the present invention;

Fig 4 (a-d) illustrates the block diagrams of Individual Disk, Presence of Centrifugal fuse and Centrifugal force in action with net deployment, in accordance with an exemplary embodiment of the present invention;

It is appreciated that not all aspects and structures of the present invention are visible in a single drawing, and as such multiple views of the invention are presented so as to clearly show the structures of the invention.

Detailed Description of the Invention

The disclosure herein presents a novel approach to the interception of unmanned aerial vehicles (UAVs), commonly known as drones, through a high-speed disc-based net launcher. This invention is not confined by the conventional limitations associated with drone capture technologies, such as potential harm to bystanders, the drone itself, or surrounding property. It is essential to acknowledge that the scope of this invention extends beyond the specific embodiments and configurations illustrated in the subsequent descriptions and accompanying drawings. The invention is capable of various modifications and alternative forms, embodying the principles and concepts disclosed herein in numerous ways, all within the ambit of the appended claims.

The terminologies and descriptive terms used throughout this document are selected for clarity and should not be interpreted as limiting. The inclusion of terms like "including", "comprising", and "having", along with their respective variations, is intended to be expansive, covering not only the listed components but also their equivalents and additional elements. Similarly, ordinal terms such as "first", "second", and "third" are utilized for differentiation purposes without implying any sequence, priority, or significance.

Embodied within this innovative system is a motor-driven spindle, a cornerstone component, energized by a high-speed motor, which is pivotal to the launcher's operation. This spindle facilitates the precise loading and subsequent release of discs, each embedded with a net designed for the entrapment of aerial targets. A distinctive feature of the spindle is its programmable nature, allowing for adjustments in its rotational speed to accommodate a range of operational distances. This adaptability enhances the launcher's utility across diverse drone interception scenarios, providing a tailored response to each unique situation.

Central to the launcher's functionality is the disc, ingeniously engineered to house an interwoven net. This net, fabricated from materials known for their resilience, such as nylon or Kevlar, ensures the robustness required for effective drone capture. The disc's design is further refined by the strategic placement of weights along its perimeter, contributing to the disc's stability during flight. These weights are pivotal in enabling a centrifugal force-based deployment of the net, ensuring that the target is captured at the optimal moment.

Encapsulating these components is the holster, which serves a role beyond mere protection. It provides essential structural support, maintaining the alignment and stability of the internal mechanisms during the launcher's operation. The holster is designed with accessibility in mind, facilitating straightforward maintenance and rapid reloading, critical for the system's continual readiness.

The precision inherent in the launcher's operation is orchestrated by a series of servo mechanisms. These mechanisms, acting in concert, ensure the timely release of the disc from the spindle, propelling it towards the target along an ideal trajectory. Their operation is synchronized with the spindle's rotational speed, allowing the system to adapt fluidly to the demands of each interception mission, thus ensuring consistent and reliable performance.

An integral aspect of the launcher's design is the rapid automated disc replacement mechanism, epitomizing the system's emphasis on continuous operation and minimal downtime. This feature enables the swift exchange of spent discs for new ones, guaranteeing the launcher's preparedness for subsequent interception attempts, an invaluable attribute in situations necessitating quick response.

This sophisticated launcher represents a paradigm shift in drone interception technology, addressing the nuanced requirements of modern security, wildlife protection, and law enforcement applications. Its effectiveness, coupled with its versatility and adaptability, positions the invention as a premier solution for a wide range of operational environments.

In practical terms, the launcher initiates with the activation of the motor-driven spindle, setting the stage for the disc's loading. As the spindle reaches the requisite speed, the disc, equipped with the net, is primed for release. The attached weights play a crucial role at this juncture, ensuring the disc's stability and contributing to the controlled deployment of the net. This deployment is meticulously timed to maximize the efficiency of the capture, with the net unfurling and expanding towards the drone, ultimately entangling it and neutralizing its mobility.

Transitioning to a more detailed embodiment of the invention, the high-speed disc-based net launcher is depicted across various figures, providing a granular view of the system's components and their interplay.

List of the components of the high-speed disc-based net launcher and their associated reference numerals:
Motor-driven Spindle – (108)
High-speed Motor – (116)
Specialized Discs – (124, 126, 128)
Net Embedded in the Discs – (144)
Motor Mount – (118)
Servo Motor – (114)
Servo Motor Mount – (112)
Holster Bars – (104, 106)
Launch Plate – (122)
Launch Track – (120)
Disc Cartridge – (100)
Cartridge Support – (102)
Centrifugal Fuse – (130)
Extended Arms in the Exploded Disc Parts – (134, 140)

These components and reference numerals outline the structure and function of the high-speed disc-based net launcher, illustrating the system's complexity and the interrelation of its parts.

Referring to Figures 1(a-c), the intricate design of the high-speed disc-based net launcher is showcased, revealing the synergistic assembly of its components. Central to its functionality is the spindle (108), robust and driven by a motor (116), securely positioned on a motor mount (118). This core mechanism is pivotal for the loading and subsequent release of specialized discs (124, 126, 128), each meticulously embedded with a net (144) designed for the effective capture of drones. The release of these discs is meticulously managed by a servo motor (114), strategically mounted on a servo motor mount (112), allowing for precise control over the launching speed as determined by the operator. Integral to the structural integrity of the launcher is a launch plate (122), strategically positioned within the launch track (120), ensuring a seamless trajectory for the discs during launch operations. Complementing this assembly are the holster bars (104, 106), providing essential stability and support to the entire structure, underscoring the launcher's robust design.

In Figure 2 (a-d), the Disc-based High-Speed Net Launcher is further detailed, highlighting the orderly arrangement of the discs (124, 126, 128) within the disc cartridge (100). This configuration ensures a methodical deployment, with only one disc being released onto the launch track at any given time, enhancing the system's efficiency in drone interception. The structural integrity of this assembly is bolstered by the cartridge support (102), which protrudes from the holster, offering additional reinforcement. A critical component in this assembly is the servo motor (114), securely affixed onto the servo motor mount (112), which not only supports the motor but also extends the functionality of the launch plate (122), augmenting the launcher's stability. This harmonious integration of components facilitates the precise maneuvering of the discs, ensuring their efficient deployment towards aerial targets. With discs pre-stacked in place, the launcher ensures seamless continuity in engagements. As soon as the lowest disc is ejected to intercept a target, the next disc swiftly falls into position, ready for immediate deployment. This rapid reloading process minimizes downtime between interceptions, allowing the system to maintain a high level of readiness for consecutive engagements.

Figure 3 (a-c) delves into the operational intricacies of the Disc-based High-Speed Net Launcher, particularly focusing on the launch plate (122). This component is designed for a flawless integration into the launch track (120), enabling a secure and precise fit that is crucial for the launcher's functionality. The meticulous design ensures that once the launch plate (122) is positioned, it, along with the launch track (120), is securely fastened, significantly enhancing the system's structural rigidity. This reinforcement is pivotal for the launcher's performance, ensuring reliable and smooth operation during both the loading and deployment phases of the discs, thereby contributing to the launcher's efficacy in intercepting aerial targets with unmatched precision.

Finally, Figure 4 (a-b) unveils the innovative inclusion of a centrifugal fuse (130) within the disc, a mechanism that plays a vital role in regulating the net's (144) deployment. This feature is instrumental in ensuring a controlled and timed release of the net, optimizing the launcher's effectiveness in capturing aerial targets.

Figure 4c illustrates the curved pathways designed for storing nets in the same orientation. This configuration ensures that the flow of the spinning discs remains undisturbed, thereby preserving their momentum and facilitating seamless transfer to the opening nets. By arranging the nets along curved paths, their opening direction aligns with the spinning disc, enabling smooth interaction between the two components. This alignment is essential for maintaining the efficiency and effectiveness of the launcher, as it ensures optimal utilization of the disc's kinetic energy for interception purposes.

Figure 4 (d) illustrates the arms serve as stabilizers, ensuring the disc remains intact and operational until the centrifugal force initiates their separation, triggering the net's deployment.

Through these illustrations, the high-speed disc-based net launcher's design and operational methodology are comprehensively detailed, highlighting the system's innovative features and its potential to revolutionize drone interception technology with its precision, reliability, and non-destructive approach to aerial target capture.

This comprehensive embodiment, enriched with specific reference numerals and illustrated through detailed figures, provides an in-depth understanding of the high-speed disc-based net launcher's design and functionality. It exemplifies the technical advancements and operational ingenuity embedded within the invention, showcasing its potential to revolutionize the field of drone interception technology.

In the development and evaluation of the high-speed disc-based net launcher, a comprehensive series of tests were conducted to ensure the system's performance, reliability, and safety met the stringent requirements essential for real-world application. The first set of tests focused on the launcher's launch accuracy, a critical aspect of its functionality. These tests involved setting up controlled environments with predefined drone flight paths at varying distances and altitudes. Through a series of drone flights designed to simulate potential target scenarios, the launcher was activated to intercept and capture these drones. The results were promising, demonstrating a high degree of accuracy with the launcher successfully capturing or entangling drones in the majority of test cases, with minimal misses or failed deployments, thereby validating its precision in targeting aerial threats.

In the comprehensive testing of the high-speed disc-based net launcher, launch accuracy was rigorously evaluated, a crucial aspect for effective interception of aerial threats. Controlled environments with predefined drone flight paths at varying distances and altitudes were set up to simulate real-world scenarios. With a 30,000 RPM motor, the launcher swiftly intercepted drones, demonstrating remarkable accuracy within distances of 3-5 meters. Minimal instances of misses or failed deployments were observed, validating its precision. Moreover, the potential for achieving interceptions at even greater distances with higher motor speeds highlights its versatility. These results affirm the reliability and efficacy of the launcher, making it suitable for various environments requiring rapid and accurate aerial threat interception.

Additionally, to optimize interception efficiency, the high-speed disc-based net launcher incorporates a dynamic RPM control system governed by a microcontroller. This intelligent system evaluates the distance of the enemy target and adjusts the motor's RPM accordingly. By dynamically adapting the motor speed based on the target's proximity, the launcher ensures precise interception across varying distances.

Further assessment was carried out to examine the launcher's reliability and durability, especially given the operational demands it would face in practical deployments. This involved subjecting the launcher to continuous operation over extended periods, mimicking the patterns of real-life usage. The tests included a series of rapid consecutive launches to challenge the automated disc replacement mechanism and to gauge the system's resilience. The launcher exhibited commendable performance consistency without significant degradation, and its components showed substantial resistance to wear and tear, confirming the system's durability and long-term reliability.

The launcher's adaptability to various environmental conditions was also rigorously tested. The system was exposed to a range of environmental stressors, including fluctuations in temperature, humidity levels, wind speeds, and precipitation, to evaluate any potential impact on its operational effectiveness. The environmental adaptability tests revealed that the launcher maintained its functionality and performance across diverse conditions, demonstrating its robustness and suitability for deployment in varying climates and settings.

Safety is paramount in the operation of such devices, and as such, the launcher underwent stringent safety and emergency shutdown tests. These tests were designed to ensure that in the event of a malfunction or during an emergency, the system could be quickly and safely deactivated. Fault conditions and emergency scenarios were simulated during operation, and the launcher's response to emergency shutdown commands was immediate and effective, halting all operations without causing harm or damage, thus underscoring the system's built-in safety measures.

Lastly, the efficiency of net deployment and the effectiveness of drone entanglement were evaluated. This involved deploying the launcher against drones equipped with various propeller guards and safety features to represent different target profiles. The launcher's net deployment was swift and consistent, successfully entangling and immobilizing a broad spectrum of drone types, even those equipped with countermeasures. These tests showed minimal instances of net failure or drone escape, highlighting the launcher's capability to neutralize aerial threats efficiently.

The culmination of these tests and the achievement of the desired results affirm the high-speed disc-based net launcher's readiness for practical deployment. Its demonstrated precision, reliability, adaptability, and safety, combined with effective net deployment and entanglement capabilities, make it a formidable solution for addressing unauthorized drone activities, offering assurance in its capacity to perform in real-world scenarios.
,CLAIMS:5. CLAIMS
I/We Claim
1. A high-speed disc-based net launcher device, comprising:
a disk cartridge (100) configured to hold multiple disks stacked in a structured manner;
a cartridge support (102) extending from a holster for supporting said disk cartridge;
holster bars (104, 106) forming said holster;
a spindle (108) operatively connected to a motor (116) and configured to facilitate loading and release of disks;
a rubber belt (110) covers the spindle head where it comes in contact with the disc to increase friction and convert spindle rotational moment to the disc;
a servo motor (114) bolted into a servo motor mount (112), said mount being an extension of a launch plate (122);
a launch track (120) having a slot specifically configured to house said launch plate (122), said launch track (122) and launch plate (120) being bolted together to provide additional support and rigidity;
disks (124, 126, 128) laid on top of each other within said disk cartridge (100), each disk embedded with a net (144);
a centrifugal fuse (130) positioned within said disks to regulate timed net (144) launch;
exploded disk parts (132, 134, 136, 138, 140, 142) containing extended arms configured to maintain disc integrity during launch and prevent premature detonation; and
a net (144) made of nylon or Kevlar, said net being configured for capturing drones and other aerial targets.

2. The device as claimed in claim 1, wherein the motor-driven spindle's rotational speed is adjustable to accommodate.

3. The device as claimed in claim 1, wherein the servo motor (114) is configured to push a loaded disk once the spindle reaches a required rotational speed.

4. The device as claimed in claim 1, comprising a rapid automated disk replacement mechanism configured to facilitate quick reloading of the disk cartridge for continuous interception operations.

5. The device as claimed in claim 1, wherein the launch plate (122) and launch track (120) are bolted together to provide additional support and rigidity to the system.

6. The device as claimed in claim 1, wherein the extended arms of the exploded disk parts are configured to hold the disk in place until centrifugal force separates them upon firing.

7. The device as claimed in claim 1, wherein the net is (144) made of Kevlar, providing enhanced durability and resistance to tearing or puncturing.

8. The device as claimed in claim 1, wherein the holster is configured for mounting onto land vehicles, aerial vehicles, or stationary objects, or as an independent handgun .

9. The device as claimed in claim 1, comprising a gimbal setup enabling tilt control for trajectory adjustment when launching nets, said tilt control being controlled by an onboard microcontroller and servo systems.

10. The device as claimed in claim 1, wherein the net launcher is integrated onto Unmanned Aerial Vehicles (UAVs) or drones for capturing other UAVs or aerial targets.

11. The device as claimed in claim 1, wherein the cartridge support (102) extends from the holster to provide structural reinforcement for the disk cartridge (100).

12. A method for launching a net (144) from a high-speed disc-based net launcher device, comprising the steps of:
activating a motor-driven spindle (108) to rotate at a required speed;
loading a specialized disk embedded with an interwoven net onto the rotating spindle (108);
controlling the release of the loaded disk using a servo motor (114), contingent upon the spindle (108) reaching a required rotational speed;
ejecting the loaded disk from the spindle (108), causing the net (144) to unravel and deploy towards a designated target;
entangling the target with the deployed net (144) to render it non-operational; and
repeating steps for continuous interception operations.

Documents

Application Documents

# Name Date
1 202441019839-PROVISIONAL SPECIFICATION [18-03-2024(online)].pdf 2024-03-18
2 202441019839-FORM FOR STARTUP [18-03-2024(online)].pdf 2024-03-18
3 202441019839-FORM FOR SMALL ENTITY(FORM-28) [18-03-2024(online)].pdf 2024-03-18
4 202441019839-FORM 1 [18-03-2024(online)].pdf 2024-03-18
5 202441019839-EVIDENCE FOR REGISTRATION UNDER SSI(FORM-28) [18-03-2024(online)].pdf 2024-03-18
6 202441019839-EVIDENCE FOR REGISTRATION UNDER SSI [18-03-2024(online)].pdf 2024-03-18
7 202441019839-DRAWINGS [18-03-2024(online)].pdf 2024-03-18
8 202441019839-DRAWING [22-03-2024(online)].pdf 2024-03-22
9 202441019839-COMPLETE SPECIFICATION [22-03-2024(online)].pdf 2024-03-22
10 202441019839-FORM-9 [08-04-2024(online)].pdf 2024-04-08
11 202441019839-FORM 18 [08-04-2024(online)].pdf 2024-04-08
12 202441019839-Proof of Right [11-04-2024(online)].pdf 2024-04-11
13 202441019839-FORM-26 [11-04-2024(online)].pdf 2024-04-11
14 202441019839-FORM 3 [11-04-2024(online)].pdf 2024-04-11
15 202441019839-ENDORSEMENT BY INVENTORS [11-04-2024(online)].pdf 2024-04-11
16 202441019839-STARTUP [05-09-2024(online)].pdf 2024-09-05
17 202441019839-FORM28 [05-09-2024(online)].pdf 2024-09-05
18 202441019839-FORM 18A [05-09-2024(online)].pdf 2024-09-05
19 202441019839-Defence-02-05-2025.pdf 2025-05-02
20 Reply from Defence.pdf 2025-11-11