Invention Grant
- Patent Title: Control system and method for landing gear extension/retraction
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Application No.: US16556651Application Date: 2019-08-30
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Publication No.: US11136114B2Publication Date: 2021-10-05
- Inventor: Martin Griffith Rowlands , Maxwell William Jones , Graham King , Trevor Anthony Brighton , Matthew Gadd
- Applicant: Airbus Operations Ltd.
- Applicant Address: GB Bristol
- Assignee: Airbus Operations Ltd.
- Current Assignee: Airbus Operations Ltd.
- Current Assignee Address: GB Bristol
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: GB1703403 20170302
- Main IPC: B64C25/26
- IPC: B64C25/26 ; B64C25/16

Abstract:
A control system has first and second processing modules for controlling retraction and extension of an aircraft landing gear assembly. The processing modules operate independently providing redundancy. Each processing module is configured to perform a first sequence of steps for retracting the landing gear assembly and a second sequence of steps for extending the landing gear assembly. A step of switching control from one processing module to the other (e.g. an avionics side changeover step) is performed (a) as part of the first sequence of steps, but only after the landing gear assembly has been retracted, or (b) as part of the second sequence of steps. By ensuring that the step of switching control is performed at such times, and not for example between initiation of the first sequence of steps and the retraction of the landing gear assembly, the landing gear assembly may be retracted sooner after such initiation.
Public/Granted literature
- US20200055592A1 CONTROL SYSTEM AND METHOD FOR LANDING GEAR EXTENSION/RETRACTION Public/Granted day:2020-02-20
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