Inventor · Arpajon, FR

Bruno Robert Gaully

27Patents
5h-index
25Co-inventors
65Inventor score

Filing activity: Jun 15, 2009 → May 4, 2020

Most-cited inventions

PatentTitleAreaCited byStatus
US8333546B2 System for controlling at least two variable-geometry equipments of a gas turbine engine, particularly by cam mechanism Mechanical Engineering; Lighting; Heating 21 Active
US9476690B2 Method for controlling the clearance at the tips of blades of a turbine rotor Mechanical Engineering; Lighting; Heating 19 Active
US8591173B2 System for controlling variable geometry apparatuses in a turbine engine Emerging Cross-Sectional Technologies 9 Active
US8690521B2 System for controlling variable geometry equipment for a turbine engine, especially by bellcranks Mechanical Engineering; Lighting; Heating 9 Active
US8740547B2 System for controlling variable geometry equipment of a gas turbine engine particularly comprising a barrel link Emerging Cross-Sectional Technologies 9 Active
US10571316B2 Method and system for determining the flow rate of air collected from an aircraft engine Emerging Cross-Sectional Technologies 4 Active
US8858164B2 Air discharge system for an aeronautical turbine engine compressor Emerging Cross-Sectional Technologies 3 Active
US8979705B2 Method and system for controlling aircraft engine starter/generator Emerging Cross-Sectional Technologies 3 Active
US8936429B2 Control unit and a method for controlling blade tip clearance Mechanical Engineering; Lighting; Heating 3 Active
US8328500B2 System for controlling variable-geometry equipments of a turbomachine, particularly by articulated bellcranks Mechanical Engineering; Lighting; Heating 3 Active
US8337140B2 System for controlling at least two variable-geometry equipments of a gas turbine engine, particularly by rack Mechanical Engineering; Lighting; Heating 2 Active
US9790807B2 Turbomachine comprising a monitoring system comprising a module for engaging a protection function of the turbomachine and monitoring method Mechanical Engineering; Lighting; Heating 2 Active
US9310276B2 Method and device for determining the air bleed on an aircraft turbojet engine Emerging Cross-Sectional Technologies 2 Active
US9182310B2 Method and a device for correcting a measurement of the pressure of a gas stream flowing in an aircraft engine Mechanical Engineering; Lighting; Heating 1 Active
US9194755B2 Device for measuring temperature in a primary stream flow passage of a bypass turbojet Physics 1 Active
US10578030B2 Method and device for adjusting a threshold value of a fuel flow rate Mechanical Engineering; Lighting; Heating 1 Active
US8757018B2 Device for changing the transmission ratio between a turbine shaft and a shaft of a starter-generator of an aeroengine Emerging Cross-Sectional Technologies 1 Active
US9261024B2 Method and a device for producing a setpoint signal Mechanical Engineering; Lighting; Heating 1 Active
US8690520B2 System for controlling variable geometry equipment of a gas turbine engine especially comprising a guiding track connection Mechanical Engineering; Lighting; Heating 1 Active
US9027355B2 Mechanical drive device for driving the high pressure sub assembly of an airplane engine Emerging Cross-Sectional Technologies 1 Active
US9447735B2 Method of controlling a turbomachine Mechanical Engineering; Lighting; Heating 1 Active
US9821736B2 Device for ventilating and supplying electrical power to an aircraft engine computer Electricity 0 Active
US11873890B2 Oil system for a turbine engine Emerging Cross-Sectional Technologies 0 Active
US9194302B2 Control of a fuel metering device for turbomachine Emerging Cross-Sectional Technologies 0 Active
US8682627B2 Estimating a stream temperature in a turbojet Physics 0 Active

Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.