Invention Grant
- Patent Title: Landing gear actuation control system
- Patent Title (中): 起落架起动控制系统
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Application No.: US12729290Application Date: 2010-03-23
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Publication No.: US08418958B2Publication Date: 2013-04-16
- Inventor: Royston Alan Evans
- Applicant: Royston Alan Evans
- Applicant Address: GB
- Assignee: GE Aviation Systems Limited
- Current Assignee: GE Aviation Systems Limited
- Current Assignee Address: GB
- Agency: Global Patent Operation
- Priority: GB0906464.3 20090415
- Main IPC: B64C25/22
- IPC: B64C25/22 ; F15B13/02 ; B66F3/24

Abstract:
A hydraulic control system for an aircraft landing gear system has a hydraulic pressure source connected to a hydraulic fluid pressure transmission line, and at least one hydraulic actuator for extending and/or retracting a landing gear. A supply valve and a direction valve are arranged in series along the hydraulic fluid pressure transmission line. The supply valve and direction valve are adjustable to control the hydraulic pressure supplied to the at least one hydraulic actuator. The control system also controls uplock actuators.
Public/Granted literature
- US20100264265A1 LANDING GEAR ACTUATION CONTROL SYSTEM Public/Granted day:2010-10-21
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