- 专利标题: INTEGRATED THRUST REVERSER AND BRAKE CONTROL FOR AN AIRCRAFT
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申请号: US18071141申请日: 2022-11-29
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公开(公告)号: US20240175409A1公开(公告)日: 2024-05-30
- 发明人: David Wasselin , Nancy Poisson , Brian V. Winebrenner , Bradley C. Schafer , Ramesh Rajagopalan
- 申请人: Raytheon Technologies Corporation
- 申请人地址: US CT Farmington
- 专利权人: Raytheon Technologies Corporation
- 当前专利权人: Raytheon Technologies Corporation
- 当前专利权人地址: US CT Farmington
- 主分类号: F02K1/76
- IPC分类号: F02K1/76 ; B64D31/09 ; B64D45/00 ; B64D45/04 ; B64F5/60 ; G05D1/617 ; G05D1/654 ; G05D109/22
摘要:
A system of an aircraft includes a thrust reverser control configured to control deployment of one or more thrust reversers of the aircraft, a brake control configured to control operation of one or more brakes of the aircraft, and a controller. The controller is configured to detect a landing condition of the aircraft, determine one or more thrust reverser deployment and brake control parameters for one or more current conditions at a target location of the aircraft, and control the one or more thrust reversers and the one or more brakes upon landing at the target location based on the one or more thrust reverser deployment and brake control parameters. The controller can modify one or more control parameters of the aircraft based on detecting a change in the one or more current conditions at the target location or a fault condition of the aircraft.
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