Invention Grant
- Patent Title: Aircraft landing gear fluid gauge
- Patent Title (中): 飞机起落架流量计
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Application No.: US14357071Application Date: 2012-11-01
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Publication No.: US09562584B2Publication Date: 2017-02-07
- Inventor: Kyle Schmidt
- Applicant: Messier-Dowty Limited
- Applicant Address: GB Gloucester
- Assignee: Safran Landing Systems UK LTD
- Current Assignee: Safran Landing Systems UK LTD
- Current Assignee Address: GB Gloucester
- Agency: RatnerPrestia
- Priority: GB1119493.3 20111111
- International Application: PCT/GB2012/052723 WO 20121101
- International Announcement: WO2013/068725 WO 20130516
- Main IPC: F16F9/32
- IPC: F16F9/32 ; B64C25/60 ; F16F9/06

Abstract:
An oleo-pneumatic shock absorber having a casing, a rod slidably mounted in the casing, first and second fluids in the casing, and a gauge. The gauge has a substrate positioned on the shock absorber. The substrate has a first region with a slot sized to fit an ultrasonic transducer arranged to encompass a range of possible oil levels within the shock absorber, a second region corresponding to a range of possible extension states of the shock absorber and a third region comprising one or more traces. Each trace corresponds to a temperature value and is indicative of an optimum relationship between the oil levels and the range of extension states at the respective temperature value associated with the trace.
Public/Granted literature
- US20140312171A1 GAUGE Public/Granted day:2014-10-23
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