Log in
Enquire now
‌

US Patent 12129057 UAV structural elements quick release fastening system

OverviewStructured DataIssuesContributors

Contents

Patent abstractTimelineTable: Further ResourcesReferences
Is a
Patent
Patent
1

Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
1
Patent Number
121290571
Patent Inventor Names
Maksym Makarchuk1
Hryhorii Yehoshyn1
Roman Franchuk1
Dmytro Vrachynskyi1
Yevhen Sedochenko1
Yevhenii Doroshenko1
Date of Patent
October 29, 2024
1
Patent Application Number
179256211
Date Filed
March 25, 2021
1
Patent Citations
‌
US Patent 10807710 Electrical connection structure, tail rod quick release structure and UAV having the same
1
‌
US Patent 10870479 Multi-architecture modular unmanned aerial system
1
‌
US Patent 11447246 Modular aircraft with vertical takeoff and landing capability
1
‌
US Patent 11292596 Unmanned aerial vehicle
1
‌
US Patent 11554847 Lock apparatus and related methods for use with drones
1
‌
US Patent 7699261 Small unmanned airborne vehicle airframe
1
‌
US Patent 9957035 Un-manned aerial vehicle having adjustable wing module, tail, and landing gear
1
Patent Primary Examiner
‌
Benjamin P Lee
1
CPC Code
‌
F16B 21/02
1
‌
B64F 5/10
1
‌
B64C 1/26
1
‌
B64C 2211/00
1
‌
F16B 21/04
1
Patent abstract

The UAV structural elements' quick-release fastening system, which includes at least two tail booms coupling with a center wing section/fuselage of a UAV and a tail assembly by at least two quick-release coupling elements from the center wing's section side and at least two coupling elements from tail assembly's side, the UAV wiring elements. The docking chucks are used as the quick-release coupling elements. Coupling and fixing the tail booms with a tail assembly realized by the tail assembly docking chucks and a bayonet mount. Coupling and fixing the tail booms with a center wing section/fuselage of a UAV is realized by the center wing section docking chucks and the center wing section fixing pins or by the center wing section docking chucks and bayonet mount. The system is generally used in a UAV design with integral or dismountable tail assembly.

Timeline

No Timeline data yet.

Further Resources

Title
Author
Link
Type
Date
No Further Resources data yet.

References

Find more entities like US Patent 12129057 UAV structural elements quick release fastening system

Use the Golden Query Tool to find similar entities by any field in the Knowledge Graph, including industry, location, and more.
Open Query Tool
Access by API
Golden Query Tool
Golden logo

Company

  • Home
  • Press & Media
  • Blog
  • Careers
  • WE'RE HIRING

Products

  • Knowledge Graph
  • Query Tool
  • Data Requests
  • Knowledge Storage
  • API
  • Pricing
  • Enterprise
  • ChatGPT Plugin

Legal

  • Terms of Service
  • Enterprise Terms of Service
  • Privacy Policy

Help

  • Help center
  • API Documentation
  • Contact Us
By using this site, you agree to our Terms of Service.