Inventor · disambiguated record
Bruno Robert Gaully
Also filed as: GAULLY BRUNO · GAULLY BRUNO ROBERT
27 granted patents·1 pending application·133 citations·filing 2009–2020
95Inventor score
Files withGAULLY BRUNO ROBERT8COLOTTE BAPTISTE BENOIT6SNECMA4SAFRAN AIRCRAFT ENGINES3BONNEAU DAMIEN1
Top patents by PatentIndex Score
28 records- 0189US9476690B2Method for controlling the clearance at the tips of blades of a turbine rotorJAVELOT CHRISTOPHE·Filed 2012·Granted Oct 25, 2016·20 cites·7 claims
- 0285US8333546B2System for controlling at least two variable-geometry equipments of a gas turbine engine, particularly by cam mechanismCOLOTTE BAPTISTE BENOIT·Filed 2009·Granted Dec 18, 2012·24 cites·10 claims
- 0380US8591173B2System for controlling variable geometry apparatuses in a turbine engineBOURU MICHEL ANDRE·Filed 2009·Granted Nov 26, 2013·13 cites·13 claims
- 0478US11873890B2Oil system for a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jan 16, 2024·2 cites·14 claims
- 0575US10571316B2Method and system for determining the flow rate of air collected from an aircraft engineSAFRAN AIRCRAFT ENGINES·Filed 2013·Granted Feb 25, 2020·5 cites·9 claims
- 0673US8690521B2System for controlling variable geometry equipment for a turbine engine, especially by bellcranksCOLOTTE BAPTISTE BENOIT·Filed 2009·Granted Apr 8, 2014·14 cites·10 claims
- 0772US8740547B2System for controlling variable geometry equipment of a gas turbine engine particularly comprising a barrel linkCOLOTTE BAPTISTE BENOIT·Filed 2009·Granted Jun 3, 2014·12 cites·11 claims
- 0871US8979705B2Method and system for controlling aircraft engine starter/generatorGALIVEL JEAN PIERRE·Filed 2010·Granted Mar 17, 2015·5 cites·13 claims
- 0969US8936429B2Control unit and a method for controlling blade tip clearanceGAULLY BRUNO ROBERT·Filed 2012·Granted Jan 20, 2015·5 cites·5 claims
- 1068US8757018B2Device for changing the transmission ratio between a turbine shaft and a shaft of a starter-generator of an aeroengineGAULLY BRUNO ROBERT·Filed 2010·Granted Jun 24, 2014·2 cites·9 claims
- 1164US9790807B2Turbomachine comprising a monitoring system comprising a module for engaging a protection function of the turbomachine and monitoring methodSNECMA·Filed 2013·Granted Oct 17, 2017·4 cites·8 claims
- 1264US8858164B2Air discharge system for an aeronautical turbine engine compressorCOLOTTE BAPTISTE·Filed 2009·Granted Oct 14, 2014·4 cites·11 claims
- 1363US9261024B2Method and a device for producing a setpoint signalGAULLY BRUNO ROBERT·Filed 2011·Granted Feb 16, 2016·3 cites·8 claims
- 1463US9194755B2Device for measuring temperature in a primary stream flow passage of a bypass turbojetGAULLY BRUNO ROBERT·Filed 2011·Granted Nov 24, 2015·2 cites·10 claims
- 1561US9310276B2Method and device for determining the air bleed on an aircraft turbojet engineSNECMA·Filed 2013·Granted Apr 12, 2016·2 cites·9 claims
- 1659US8328500B2System for controlling variable-geometry equipments of a turbomachine, particularly by articulated bellcranksCOLOTTE BAPTISTE BENOIT·Filed 2009·Granted Dec 11, 2012·6 cites·12 claims
- 1757US9447735B2Method of controlling a turbomachineGAULLY BRUNO ROBERT·Filed 2011·Granted Sep 20, 2016·1 cites·7 claims
- 1854US10578030B2Method and device for adjusting a threshold value of a fuel flow rateSAFRAN AIRCRAFT ENGINES·Filed 2013·Granted Mar 3, 2020·1 cites·11 claims
- 1951US9903277B2Method for monitoring a fuel circuit shut-off valveSNECMA·Filed 2013·Granted Feb 27, 2018·1 cites·8 claims
- 2051US9182310B2Method and a device for correcting a measurement of the pressure of a gas stream flowing in an aircraft engineGAULLY BRUNO ROBERT·Filed 2011·Granted Nov 10, 2015·1 cites·10 claims
- 2151US8337140B2System for controlling at least two variable-geometry equipments of a gas turbine engine, particularly by rackCOLOTTE BAPTISTE BENOIT·Filed 2009·Granted Dec 25, 2012·3 cites·10 claims
- 2250US9821736B2Device for ventilating and supplying electrical power to an aircraft engine computerSNECMA·Filed 2013·Granted Nov 21, 2017·0 cites·10 claims
- 2349US9027355B2Mechanical drive device for driving the high pressure sub assembly of an airplane engineCOLOTTE BAPTISTE BENOÍT·Filed 2010·Granted May 12, 2015·1 cites·9 claims
- 2448US8690520B2System for controlling variable geometry equipment of a gas turbine engine especially comprising a guiding track connectionCOLOTTE BAPTISTE BENOIT·Filed 2009·Granted Apr 8, 2014·2 cites·12 claims
- 2546US8682627B2Estimating a stream temperature in a turbojetDJELASSI CEDRIK·Filed 2009·Granted Mar 25, 2014·0 cites·7 claims
- 2638US9194302B2Control of a fuel metering device for turbomachineGAULLY BRUNO ROBERT·Filed 2011·Granted Nov 24, 2015·0 cites·10 claims
- 2737US2013177414A1Method and system for controlling the clearance at the blades tips of a turbine rotorBONNEAU DAMIEN·Filed 2011·Application pending·0 cites
- 2833US9732764B2Device and method for positioning variable-geometry equipment for a turbomachine, using a relative-measurement jackGAULLY BRUNO ROBERT·Filed 2010·Granted Aug 15, 2017·0 cites·6 claims
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