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Safran Aircraft Engines patents

Recent patent applications related to Safran Aircraft Engines. Safran Aircraft Engines is listed as an Agent/Assignee. Note: Safran Aircraft Engines may have other listings under different names/spellings. We're not affiliated with Safran Aircraft Engines, we're just tracking patents.

ARCHIVE: New 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "S" | Safran Aircraft Engines-related inventors




Date Safran Aircraft Engines patents (updated weekly) - BOOKMARK this page
07/20/17 new patent  System for supplying pressurised air installed in an aircraft turbine engine including sealing means
07/20/17 new patent  Outlet guide vane for aircraft turbine engine, presenting an improved lubricant cooling function
07/20/17 new patent  Method and system for evaluating a flow rate of a fluid
07/13/17Method of fabricating a textile structure of varying thickness
07/13/17Method of fabricating a textile structure of varying thickness
07/13/17Method for manufacturing a turbine engine vane made of a composite material, resulting vane and turbine engine including same
07/13/17Lubrication device for a turbine engine
07/13/17Method and a device for controlling thrust from a turbojet
07/13/17Method for modelling a bathtub of a blade
07/06/17Assembly for turbine machine with open rotor contra-rotating propellers, comprising a small duct for the passage of ancillaries
07/06/17Turbine blade with optimised cooling at the trailing edge of same comprising upstream and downstream ducts and inner side cavities
07/06/17Variable-pitch fan with low pitch of a turbine engine
07/06/17Measuring comb for measuring parameters of the gases exiting a turbomachine working section
06/29/17Turbine blade with optimised cooling
06/29/17Turbine blade comprising a central cooling duct and two side cavities connected downstream from the central duct
06/29/17Improved interface for a valve for a cryogenic fluid duct
06/29/17Aircraft flight data evaluation system
06/22/17System for clamping a part and sealing the inner casing of a low pressure rectifier of a turbomachine
06/22/17Device for controlling clearance at the tops of turbine rotating blades
06/22/17Turbomachine comprising a means of uncoupling a fan
06/22/17Method for assessing whether or not a measured value of a physical parameter of an aircraft engine is normal
06/15/17Device for fixing blades with variable pitch of a non-streamlined turbomachine propeller
06/15/17Transport and hoisting structure for a turbomachine
06/15/17Turbine rotor for a gas turbine engine
06/08/17Method for dimensioning a turbomachine
06/08/17Method of monitoring a degradation of a device on board an aircraft including the determination of a counting threshold
06/01/17Method for manufacturing a core for moulding a blade
06/01/17Improved manufacturing a shell mold for production by lost-wax casting of bladed elements of an aircraft turbine engine
06/01/17Turbomachine element comprising an auxiliary sealing means, and testing this element
06/01/17Instrumented flow passage of a turbine engine
06/01/17Method for starting a fan operation test
06/01/17Method and a device for estimating a quality index for a 3d image of a composite material part
05/25/17Mounting of vanes at the periphery of a turbine engine disc
05/25/17Method for creating and repairing a turbomachine component and associated turbomachine component
05/25/17Device and lubricating a turbomachine rolling bearing
05/18/17Method for manufacturing a two-component blade for a gas turbine engine and blade obtained by such a method
05/18/17Propulsion assembly for an aircraft, comprising a gas generator, two offset fans and an air inlet sleeve
05/18/17Propulsion assembly for an aircraft, comprising a gas generator and two offset fans
05/18/17Propulsive wing of an aircraft
05/18/17Aircraft with a propulsion unit comprising a fan at the rear of the fuselage
05/18/17Sealing plate with fuse function
05/18/17Gearbox of aircraft turbine engine
05/18/17Device for measuring aerodynamic magnitudes intended to be placed in a flow passage of a turbine engine
05/18/17Air guidance device for a turbomachine
05/18/17Aircraft turbine engine air intake duct
05/18/17Turbine engine stator vane, fan casing comprising such a vane, thrust reverser system of a turbine engine equipped with such a vane and turbine engine equipped with said vane, said casing or said system
05/11/17Method for producing a low-alloy steel ingot
05/04/17Rotationally symmetrical part for a turbine engine rotor, and related turbine engine rotor, turbine engine module, and turbine engine
05/04/17A turbine engine comprising a drive system for a device such as an accessories case
04/27/17Device for assisting a solid propellant propulsion system of a single-engine helicopter, single-engine helicopter comprising such a device
04/27/17Propulsion assembly for aircraft with a jet engine with a dismountable fan blade
04/20/17Method for assisting with the detection of damage to a turbojet duct
04/13/17System for supplying a turbine engine with fluid having a low pressure pumping assembly comprising two pumps in parallel
04/13/17Ball joint device for a turbine engine
04/06/17Propulsion unit for an aircraft
04/06/17Production maraging steel
04/06/17Turbojet engine with offset fans with a differential system
04/06/17Aviation turbine engine fan assembly including a fitted platform
04/06/17Method for measuring the kinematics of at least one turbomachine rotor
03/30/17Engine for a spacecraft, and spacecraft comprising such an engine
03/30/17Heat-exchange and noise-reduction panel for a propulsion assembly
03/30/17Improved flow-control device with reduced weight
03/23/17Stiffened hub for unshrouded propeller
03/16/17Stator sector for a turbine engine, and a fabricating it
03/16/17Gas turbine engine comprising a starter engaged with a low-pressure body
Patent Packs
03/09/17Supporting tools for winding a fibrous texture, process for producing a fibrous texture and making a fibrous preform of revolution
03/09/17Oil cooler integrated into the pylon
03/09/17Bearing element to cushion axial displacements of a sliding traverse of an injection system for a turbomachine
03/02/17Ring-shaped thermomechanical part for turbine engine
03/02/17Pipe supporting system
02/23/17Composite material vane with integrated aerodynamic covering element and manufacturing method thereof
02/23/17Turbine engine module comprising a casing around a device with a cover for recovering lubricating oil
02/16/17Mould for monocrystalline casting
02/16/17Method for deploying a satellite constellation
02/16/17Modular assembly for a turbine engine
02/16/17Method for detecting an increase in the rating of a low-pressure turbine of an aircraft reactor during a cruising flight phase, and associated device and regulating the cooling air flow rate of a low-pressure turbine
02/09/17Method for synchronising the engines of an airplane with dual intermediate state
02/09/17Turbine engine rotor lock
02/09/17Turbomachine fan frame comprising improved attachment means
02/09/17Riveted assembly and associated production method
Patent Packs
02/02/17Synchronisation of the input data links of a computer
01/26/17Nacelle comprising an exchanger for cooling a stream of fluid
01/26/17Heat treatment of an alloy based on titanium aluminide
01/19/17Protective edge for a blade and manufacturing said edge
01/12/17Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine
01/12/17An improved propellant feed system for a space vehicle
01/12/17Tools for supporting powder preform during a heat treatment
01/12/17Fan rotor for a turbo machine such as a multiple flow turbojet engine driven by a reduction gear
01/12/17Cooling of a main line in a multipoint fuel injection system
01/12/17Turbine engine provided with a lubrication unit
01/12/17A simulating shaping a textile strip on a mold presenting a surface of revolution
01/05/17Unducted propeller turboshaft engine provided with a reinforcing shell integrating pipe segments
12/01/16Mould, particularly injection mould, and injection moulding method using such a mould
12/01/16Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine
12/01/16Method for localised repair of a damaged thermal barrier
11/24/16Lined mold for centrifugal casting
11/24/16Lined centrifugal mould with controlled thermal inertia
11/17/16Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine
06/08/17Instrumented flow passage of a turbine engine
11/24/16Nacelle for an airplane turbojet







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