Invention Application
- Patent Title: Mechanisms for Deploying and Actuating Airfoil-Shaped Bodies on Unmanned Aerial Vehicles
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Application No.: US14590464Application Date: 2015-01-06
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Publication No.: US20160176503A1Publication Date: 2016-06-23
- Inventor: Jonathan David Gettinger
- Applicant: The Boeing Company
- Applicant Address: US IL Chicago
- Assignee: THE BOEING COMPANY
- Current Assignee: THE BOEING COMPANY
- Current Assignee Address: US IL Chicago
- Main IPC: B64C3/56
- IPC: B64C3/56 ; B64C39/02 ; B64C5/12

Abstract:
Deployment and control actuation mechanisms are incorporated in unmanned aerial vehicles having folding wings and/or folding canards and/or a folding vertical stabilizer. The folding canards and folding vertical stabilizer can be deployed using respective four-bar over-center mechanisms. Elevators pivotably mounted to the folding canards and a rudder pivotably mounted to the folding vertical stabilizer can be controlled by means of respective twist link mechanisms. The folding wings have respective wing roots that are driven by respective gas springs to pivot on bearings about a wing root hub having control servo wire paths.
Public/Granted literature
- US09533758B2 Mechanisms for deploying and actuating airfoil-shaped bodies on unmanned aerial vehicles Public/Granted day:2017-01-03
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