Inventor · disambiguated record
Jonathan Langridge
Also filed as: LANGRIDGE JONATHAN · LANGRIDGE JONATHAN DAVID ROBERT
5 granted patents·1 pending application·2 citations·filing 2013–2019
62Inventor score
Top patents by PatentIndex Score
6 records- 0159US9249755B2Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzleSNECMA·Filed 2013·Granted Feb 2, 2016·2 cites·15 claims
- 0255US11274632B2Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner faceSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Mar 15, 2022·0 cites·10 claims
- 0350US10837706B2Heat exchanger fitted with upstream cover to reduce disturbance to fluid flow in a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 17, 2020·0 cites·7 claims
- 0445US10302043B2Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner faceSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted May 28, 2019·0 cites·8 claims
- 0539US10036349B2Afterbody for a turbojet engine comprising a nozzle provided with a thrust reverser system that incorporates a crown of noise-reducing chevronsSNECMA·Filed 2014·Granted Jul 31, 2018·0 cites·18 claims
- 0639US2016215727A1Afterbody for a mixed-flow turbojet engine comprising a lobed mixer and chevrons with a non-axisymmetric inner surfaceSNECMA·Filed 2014·Application pending·0 cites
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