Patent Assignment
Reel/Frame 044787/0425
Assignment of Assignor's Interest
Recorded: 2017-11-10
Pages: 29
Assignor
SNECMA
Executed: 2016-06-30
Assignee
AIRBUS SAFRAN LAUNCHERS SAS
60-62 RUE CAMILLE DESMOULINS, ISSY LES MOULINEAUX, 92130, FRANCE
Covered Properties
(63)
Electrolytic Igniter for Rocket Engines Using Liquid Propellants
Electrolytic Igniter for Rocket Engines Using Monopropellants
Device for Damping the Lateral Forces Due to Jet Separation Acting on a Rocket Engine Nozzle
Rocket Engine Nozzle System
Bundle Comprising Two Pairs of Tanks, and an Airborne Launcher Including Such a Bundle
Tank Having a Piston Pressurized by Hot Gas
Pump Having an Axial Balancing Device
Liquid Propellant Rocket Engine with a Propulsion Chamber Shutter
Device for injecting a mono-propellant with a large amount of flow rate modulation
Device for Injecting Mono-Propellant at a Flow Rate That Can Be Modulated with an Injection Speed That Is Stable
Device for Adjusting an Operating Variable of an Engine
Method and a Device for Calculating a Starting or Stop Sequence for an Engine
Device and a Method for Applying a Coating on a Workpiece by Electrodeposition
Thruster Comprising a Plurality of Rocket Motors
Deployable Divergent Nozzle for a Propulsive Unit
Rocket Engine with Cryogenic Propellants
Rocket Engine with Cryogenic Propellants
Convex Thermal Shield for Rocket Engine with Extendable Divergent Nozzle
Combustion Chamber Comprising a Condensation-Proof Barrier on a Regenerative Circuit
Turbine Machine Casing with Reinforced Sealing
Fastener Fitting Between the Movable Portion of a Deployable Diverging Bell for a Thruster and a Mechanism for Deploying Said Movable Portion
Failure Detection and Locating System and Engine Containing the Same
Controlled Isolation Valve Having Reinforced Sealing
Combustion Chamber Provided with a Tubular Element
Turbopump, in Particular for Feeding Rocket Engines
Rocket Motor Combustion Chamber Injection Head
Injector for Mixing Two Propellants Comprising at Least One Injection Element with a Tricoaxial Structure
System for Reducing the Dynamic Behavior of the Movable Segment of a Deployable Nozzle for a Rocket Engine
Cryogenic Thruster Assembly Using Regenerative Heating from Main and Settling Thrusters
Method of Heating a Cryogenic Liquid
Application:
14/346,594 →
Publication:
US 2015/0063409
Device for Heating a Fluid
Pressurizing Device and Method
Jet Propulsion Device and Fuel Supply Method
Rocket Engine with Optimized Fuel Supply
Application:
14/372,883 →
Publication:
US 2014/0373507
Spacecraft Fitted with a De-Orbiting Device Comprising a Detonation Engine
Turbopump
Turbopump
Application:
14/408,357 →
Publication:
US 2015/0143797
Device and a Method for Feeding a Rocket Engine Propulsion Chamber
Application:
15/141,431 →
Publication:
US 2016/0237951
Cooling Method for a Turbo Pump in a Rocket Engine Using a Cryogenic Fluid
Application:
14/420,947 →
Publication:
US 2015/0204597
Propulsion Assembly for Rocket
Application:
14/648,411 →
Publication:
US 2015/0308384
Two-Mode Ignitor and a Two-Mode Method of Injection for Igniting a Rocket Engine
Application:
14/422,790 →
Publication:
US 2015/0233324
Propulsion Chamber for a Rocket and Method for Producing Such a Chamber
Application:
15/029,920 →
Publication:
US 2016/0312744
Turbopump with Anti-Vibration System
Method and a Device for Feeding a Rocket Engine
Method and Device for Thermally Insulating a Piece of Equipment
Propellant Feed Circuit and a Cooling Method
Application:
14/760,175 →
Publication:
US 2015/0354505
A Propellant Feed Circuit and a Cooling Method
Threaded Rod for System for Deploying a Deployable Divergent Segment of a Thruster
Low-Cost High-Performance Annular Metallic Seal for High Pressures and Large Diameters
System and a Method for Feeding a Rocket Engine
Application:
14/760,186 →
Publication:
US 2015/0354503
Device for Connecting Two Segments of a Propelling Nozzle
Application:
14/902,141 →
Publication:
US 2016/0169155
Device for Self-Pressurization of a Tank
Application:
15/024,466 →
Publication:
US 2016/0222918
Device for Pressurizing Propellant Tanks of a Rocket Engine
Device for Pressurizing a Propellant Tank of a Rocket Engine
Device for Feeding a Rocket Engine with Propellant
Application:
14/909,920 →
Publication:
US 2016/0195039
Centrifugal Pump, in Particular for Supplying Power to Rocket Engines
A Propulsion Assembly and a Method of Feeding Propellants
Application:
15/034,215 →
Publication:
US 2016/0281641
Method for Controlling a Propulsion System
Application:
15/107,700 →
Publication:
US 2016/0319772
Autogenous Pressurizer Device for a Propellant Tank
Application:
15/031,484 →
Publication:
US 2016/0237952
A Device for Feeding a Rocket Engine Propulsion Chamber with Propellant
Application:
15/037,780 →
Publication:
US 2016/0290284
Thermal Protection System for a Cryogenic Tank of a Space Vehicle
Application:
15/111,989 →
Publication:
US 2016/0341362
Feed System and a Method of Suppressing the Pogo Effect
Application:
15/348,691 →
Publication:
US 2017/0058836
Feed System and a Method of Suppressing the Pogo Effect
Related Assignments
(18)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Jan 28, 2009
From: VUILLAMY, DIDIER; GAZAVE, ROBERT
To: SNECMA
Reel/Frame 022168/0369 →
Assignment of Assignor's Interest
Apr 15, 2009
From: CONRARDY, JEAN-MARIE; PEYRISSE, DANIEL; LE LOUEDEC, DOMINIQUE
To: SNECMA
Reel/Frame 022549/0806 →
Assignment of Assignor's Interest
Jun 24, 2009
From: EVEN, PHILIPPE; BEAUVERGER, PHILIPPE; BRANCHET, CHRISTELLE; MILLON, FREDERICK
To: SNECMA
Reel/Frame 022867/0637 →
Assignment of Assignor's Interest
Aug 27, 2009
From: PEYRISSE, DANIEL; LE LOUEDEC, DOMINIQUE; CONRARDY, JEAN-MARIE
To: SNECMA
Reel/Frame 023154/0075 →
Assignment of Assignor's Interest
Aug 28, 2009
From: GOISLOT, HERVE
To: SNECMA
Reel/Frame 023165/0637 →
Assignment of Assignor's Interest
Aug 28, 2009
From: GOISLOT, HERVE
To: SNECMA
Reel/Frame 023165/0651 →
Assignment of Assignor's Interest
Aug 28, 2009
From: GOISLOT, HERVE
To: SNECMA
Reel/Frame 023165/0654 →
Assignment of Assignor's Interest
Sep 18, 2009
From: THOMAS, JEAN-LOUIS; LE CLEAC'H, ALAIN
To: SNECMA
Reel/Frame 023253/0307 →
Assignment of Assignor's Interest
Oct 2, 2009
From: VALENTIAN, DOMINIQUE
To: SNECMA
Reel/Frame 023320/0373 →
Assignment of Assignor's Interest
Oct 2, 2009
From: VALENTIAN, DOMINIQUE
To: SNECMA
Reel/Frame 023320/0366 →
Assignment of Assignor's Interest
Oct 15, 2009
From: LE GONIDEC, SERGE
To: SNECMA
Reel/Frame 023374/0905 →
Assignment of Assignor's Interest
Nov 12, 2009
From: LE GONIDEC, SERGE; FAYE, OLIVIER
To: SNECMA
Reel/Frame 023505/0901 →
Assignment of Assignor's Interest
Apr 5, 2011
From: CONRARDY, JEAN-MARIE; PEYRISSE, DANIEL
To: SNECMA
Reel/Frame 026075/0619 →
Assignment of Assignor's Interest
Oct 28, 2011
From: BOUFFLERT, SEBASTIEN; JUHEL, NICOLAS; FAYOLLE, PATRICE; LAFFITE, STEPHANE
To: SNECMA
Reel/Frame 027141/0127 →
Assignment of Assignor's Interest
Dec 6, 2011
From: CONDAMINET, OLIVIER; STEPHANT, ROMAIN; JAMES, PHILIPPE
To: SNECMA
Reel/Frame 027340/0573 →
Assignment of Assignor's Interest
Apr 30, 2012
From: DOBEK, OLIVIER; LE DORTZ, DANIEL
To: SNECMA
Reel/Frame 028128/0293 →
Assignment of Assignor's Interest
May 1, 2012
From: DOBEK, OLIVIER; LE DORTZ, DANIEL
To: SNECMA
Reel/Frame 028134/0935 →
Change of Name
Nov 20, 2017
From: AIRBUS SAFRAN LAUNCHERS SAS
To: ARIANEGROUP SAS
Reel/Frame 044800/0080 →