Invention Grant
- Patent Title: System, kit and method for indicating the pressure in an aircraft landing gear shock absorber
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Application No.: US14404243Application Date: 2013-05-23
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Publication No.: US09771166B2Publication Date: 2017-09-26
- Inventor: Fraser Wilson , Stephen Briancourt , Scott Wallis
- Applicant: AIRBUS OPERATIONS LIMITED
- Applicant Address: GB Bristol
- Assignee: AIRBUS OPERATIONS LIMITED
- Current Assignee: AIRBUS OPERATIONS LIMITED
- Current Assignee Address: GB Bristol
- Agency: Hauptman Ham LLP
- Priority: GB1209502.2 20120529
- International Application: PCT/GB2013/051363 WO 20130523
- International Announcement: WO2013/178999 WO 20131205
- Main IPC: B64D45/00
- IPC: B64D45/00 ; B64C25/58 ; F16F9/32 ; G01L7/16 ; G01L9/00 ; G01M17/04 ; G01B11/14 ; B64C25/02 ; G01L19/08 ; B64F5/60

Abstract:
A system for indicating the pressure in an aircraft landing gear shock absorber is provided, the system comprising a source of collimated light and a target, the source of collimated light being attached to the aircraft, and being operable to emit light onto the target; the position of the point of incidence of the light emitted from the source of collimated light on the target being indicative of the pressure in the aircraft landing gear shock absorber. A kit for making such a system and a method of indicating the pressure in an aircraft landing gear are also provided.
Public/Granted literature
- US20150166195A1 SYSTEM, KIT AND METHOD FOR INDICATING THE PRESSURE IN AN AIRCRAFT LANDING GEAR SHOCK ABSORBER Public/Granted day:2015-06-18
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