- Patent Title: Automatic envelope limiting based on detected hydraulic failures
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Application No.: US15696345Application Date: 2017-09-06
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Publication No.: US11442446B2Publication Date: 2022-09-13
- Inventor: Christopher A. Thornberg , Derek H. Geiger , Joseph T. Driscoll , Ole Wulff
- Applicant: Sikorsky Aircraft Corporation
- Applicant Address: US CT Stratford
- Assignee: Sikorsky Aircraft Corporation
- Current Assignee: Sikorsky Aircraft Corporation
- Current Assignee Address: US CT Stratford
- Agency: Michael Best & Friedrich LLP
- Main IPC: G05D1/00
- IPC: G05D1/00 ; B64C27/56 ; B64C27/64 ; B64C27/57 ; G05D1/08 ; B64C13/50

Abstract:
A rotary-wing aircraft and system for flying a rotary-wing aircraft. The aircraft includes a servo system for actuating a rotor of the aircraft. A hydraulic system provides hydraulic power to the servo system, and a sensor measures a parameter of the hydraulic system. A processor determines a condition of the hydraulic system from the parameter and enforces an effective flight envelop based on the condition of the hydraulic system in order to fly the aircraft within the effective flight envelope.
Public/Granted literature
- US20190072952A1 AUTOMATIC ENVELOPE LIMITING BASED ON DETECTED HYDRAULIC FAILURES Public/Granted day:2019-03-07
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