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Techspace Aero S a patents

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

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Date Techspace Aero S a patents (updated weekly) - BOOKMARK this page
03/02/17Vortex-injector casing for an axial turbomachine compressor
01/26/17Perforated drum of a compressor of an axial turbine engine
12/29/16Axial turbomachine compressor casing
11/24/16Fuelling connection module for space launch vehicle
11/24/16Blade and shroud with socket for a compressor of an axial turbomachine
11/24/16Autoclave cryogenic electromagnetic valve for a space launch vehicle
11/10/16Composite splitter lip for axial turbomachine compressor
10/20/16De-icing splitter lip for axial turbomachine compressor
10/13/16Preform draping for a composite compressor casing of an axial turbine engine
10/06/16Test bench for an aircraft turbojet engine, with shutters
09/22/16Cooling of turbine engine by evaporation
09/08/16Composite compressor blade for an axial-flow turbomachine
06/02/16Electromagnetic valve for high-pressure cryogenic gas
05/26/16Abradable composition and seal of an axial-flow turbomachine compressor casing
05/19/16Internal shroud for a compressor of an axial-flow turbomachine
05/19/16Test bench for an axial turbine engine with a vertical wind power engine
05/12/16Mixed stator for an axial turbine engine compressor
04/28/16Compressor for an axial turbine engine with double contra-rotating rotors
04/28/16Lattice type blade of an axial turbine engine compressor
04/21/16Insulating test engine hood for a turbine engine on a test bench
04/21/16Splitter nose with plasma de-icing for axial turbine engine compressor
04/14/16Axial turbomachine compressor outer casing with seal
04/14/16Compressor of axial turbine engine with contra-rotating rotor
03/17/16Composite casing for axial turbomachine low-pressure compressor
03/17/16Dynamometer for a test stand for an aircraft turbomachine
02/04/16Application of a connection joint to a stator stage by means of inflatable bladders
01/28/16Blade with branches for an axial-flow turbomachine compressor
01/28/16Axial turbomachine compressor blade with branches at the base and at the head of the blade
01/28/16Blading with branches on the shroud of an axial-flow turbomachine compressor
01/28/16Vane with sealed lattice in a shroud of an axial turbomachine compressor
01/07/16Guide vane assembly vane box of an axial turbine engine compressor
12/31/15Axial turbomachine compressor inner shell
12/10/15Mould for an abradable track beneath the inner shroud of an axial-flow turbomachine compressor
10/29/15Blade retaining ring for an internal shroud of an axial-flow turbomachine compressor
10/29/15Integral bent housing for an axial turbomachine compressor
10/15/15Composite casing for a compressor of an axial-flow turbomachine
10/15/15Faceted housing for axial turbomachine compressor
09/24/15Aerospace electrovalve for high-pressure cryogenic gas
07/09/15Composite housing with a metallic flange for the compressor of an axial turbomachine
06/25/15Final-stage internal collar gasket of an axial turbine engine compressor
06/25/15Strip for abradable in a compressor turbine
06/18/15Composite annular casing of a compressor for a turbo machine
05/21/15Annular cover delimiting a turbomachine lubrication chamber
04/16/15Piezoelectric damper system for an axial turbomachine rotor
03/12/15Provisional retention of metal sheet on a mold by microwelds
03/05/15Turbomachine axial compressor seal with a brush seal
01/08/15Splitter nose with a sheet that forms a surface to guide the flow and acts as a de-icing duct
01/08/15Stator blade sector for an axial turbomachine with a dual means of fixing
12/25/14Piston-controlled anti-siphon valve
12/25/14Axial turbomachine compressor drum with dual means of blade fixing
12/04/14Blade with an s-shaped profile for an axial turbomachine compressor
11/27/14Tank and manufacturing same
11/13/14Turbomachine lubrication system with an anti-siphon valve for windmilling
11/13/14Air bleed system for an axial turbomachine
11/13/14Turbomachine stator internal shell with abradable material
11/06/14Axial turbomachine stator with ailerons at the blade roots
10/02/14Stator blades of an axial turbocompressor and manufacturing process
08/07/14Attaching the blades of an axial turbocompressor to the compressor drum
06/26/14Blade-retaining plate with internal cut-outs for a turbomachine stator
06/12/14Axial turbomachine blade with platforms having an angular profile
05/29/14Axial turbomachine stator with segmented inner shell
05/29/14Axial turbomachine blade with platforms having an angular profile
05/15/14Radial fixing and positioning flanges for shells of axial turbine compressor housings
04/17/14Drum blade lock in a circumferential rotor groove
03/20/14Attaching the blades to the drum of an axial turbocompressor
Patent Packs
09/12/13Two-material one-piece cutting tool
06/27/13Solenoid actuator with magnetic sleeving
05/23/13Axial turbomachine compressor outer casing
05/02/13Co-injected composite shell for an axial turbomachine compressor
03/21/13Monitoring overfilling in an aeroplane engine lubrication system
12/20/12Process for friction welding blades to the drum of an axial compressor and a corresponding device
10/04/12Gas flow separator with a thermal bridge de-icer
09/06/12External segmented shell capable of correcting for rotor misalignment in relation to the stator
07/05/12Integration of a surface heat-exchanger with regulated air flow in an airplane engine
07/05/12Composite-material vane
05/31/12Abradable for stator inner shroud
05/24/12Advanced air and oil circuit architecture for turbomachine
05/24/12Method for monitoring the oil system of a turbomachine
12/29/11Compressor rectifier architecture
12/29/11Lightened axial compressor rotor
Patent Packs
10/06/11Method for manufacturing a rectifier
06/23/11Architecture of a compressor rectifier
04/07/11Method for manufacturing a heat exchanger and exchanger obtained by the method
12/23/10Method for manufacturing vanes integrated into a ring and rectifier by the method
12/23/10Method for manufacturing braided preforms
08/26/10Automatic shut-off valve for the oil circuit in an airplane engine
07/01/10Combined pumping and separating machine for the oil circuit of a turbojet
06/24/10Guide vane architecture
06/24/10Manufacture of complex composite parts
06/25/09Recirculation valve in an aircraft engine
06/25/09Heat exchange system in a turbomachine
06/25/09Method for controlling the consumption and for detecting leaks in the lubrication system of a turbine engine







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