Invention Grant
- Patent Title: Aircraft assembly including deflection sensor
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Application No.: US15833549Application Date: 2017-12-06
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Publication No.: US10654564B2Publication Date: 2020-05-19
- Inventor: Valerijan Cokonaj , Laura Collett
- Applicant: Safran Landing Systems UK LTD
- Applicant Address: GB
- Assignee: Safran Landing Systems UK LTD
- Current Assignee: Safran Landing Systems UK LTD
- Current Assignee Address: GB
- Agency: RatnerPrestia
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@2d77c36d
- Main IPC: B64C25/58
- IPC: B64C25/58 ; B64D45/00 ; G01C19/5776 ; B64C25/02

Abstract:
An aircraft assembly having a first region, a second region spaced from the first region by a flexible region, and a deflection sensor. The first region has greater positional stability than the second region such that the second region deflects further from its default position than the first region during in-use loads. The deflection sensor includes a first gyroscope at the first region to generate a first signal representing rotation of the first region about one or more orthogonal axes, and a second gyroscope at the second region to generate a second signal representing rotation of the second region about the one or more axes. The second gyroscope is synchronised in time with the first. A controller subtracts one of the first and second signals from the other to obtain a differential signal representing deflection of the second region relative to the first due to flexing of the flexible region.
Public/Granted literature
- US20180170531A1 AIRCRAFT ASSEMBLY INCLUDING DEFLECTION SENSOR Public/Granted day:2018-06-21
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