Patent Assignment
Reel/Frame 046678/0455
Change of Name
Recorded: 2018-04-22
Pages: 5
Assignor
HERAKLES
Executed: 2016-08-11
Assignee
SAFRAN CERAMICS
RUE DE TOUBAN, LE CINQ CHEMINS, 33185 LE HAILLAN, FRANCE
Covered Properties
(94)
Composite Material with Ceramic Matrix and Sic Fiber Reinforcement, Method for Making Same
Patent:
6,291,058 →
Application:
09/308,960 →
Method and Machine for Producing Multiaxial Fibrous Webs
Patent:
6,585,842 →
Application:
09/381,941 →
System for Activating an Adjustable Tube by Means of an Elastic Ring for a Thrust Nozzle
Patent:
6,378,294 →
Application:
09/647,454 →
System for Activating a Steerable Thrust-Vectoring Nozzle for a Jet Propulsion System Using Several Circumferentially Distributed Elastic Assemblies
Patent:
6,385,965 →
Application:
09/647,455 →
Protecting Composite Material Parts Against Oxidation
Stand-Off for Fixing Thermal Protection Panels
Method and Installation for Treating Effluent Gas Containing Hydrocarbons
Method and Machine for Producing Multiaxial Fibrous Webs
Method and Device for Producing a Textile Web by Spreading Tows
Combustion Chamber Sealing Ring, and a Combustion Chamber Including Such a Ring
Chemical Vapour Infiltration Method for Densifying Porous Substrates Having a Central Passage
Method and Installation for the Densification of Substrates by Means of Chemical Vapour Infiltration
Method for Monitoring the Course of a Process Using a Reactive Gas Containing One or Several Hydrocarbons
Method of Siliciding Thermostructural Composite Materials, and Parts Obtained by the Method
Method of Making a Multi-Perforated Part Out of Ceramic Matrix Composite Material
Making Composite Material Parts from Blanks Made by Reinforcing a Fiber Structure and/or Bonding Fiber Structures Together
Method of Manufacturing a Part Out of Impervious Thermostructural Composite Material
Method For Soldering Composite Material Parts
Application:
11/630,577 →
Publication:
US 2008/0190552
Mixer for Separate-Flow Nozzle
Obtaining Fiber Textures of Carbon by Carbonizing a Cellulose Precursor
Method for Chemical Infiltration in the Gas Phase for the Densification of Porous Substrates with Pyrolytic Carbon
Method of Densifying Thin Porous Substrates by Chemical Vapor Infiltration, and a Loading Device for Such Substrates
Method for Making a Part of Composite Material with Ceramic Matrix and Resulting Part
Protection Against the Oxidation of Composite Materials Containing Carbon
Composite Material Component with Silicon-Containing Ceramic Matrix, Protected Against Corrosion
Fiber Reinforcing Texture for Making a Composite Material Part
Reinforcing Fiber Texture with Multiple-Satin Weaving for a Composite Material Part
Method of Siliciding Thermostructural Composite Materials, and Parts Obtained by the Method
Gas Turbine Combustion Chamber Having Inner and Outer Walls Subdivided into Sectors
Process for Manufacturing a Part Made of a Ceramic Matrix Composite Containing Matrix Phases for Healing and Deflecting Cracks
Process for Manufacturing a Thermostructural Composite Part
Composite Material Part with a Silicon-Containing Ceramic Matrix Protected Against Corrosion
Method of Fabricating a Thermostructural Composite Material Part, and a Part Obtained Thereby
Method of Manufacturing a Cmc Flow Mixer Lobed Structure for a Gas Turbine Aeroengine
Turbine Ring Assembly for Gas Turbine
Turbine Ring Assembly for Gas Turbine
Method for Assembling End to End Two Parts Having Different Thermal Expansion Coefficients and Assembly Thus Obtained
Cmc Mixer with Structural Outer Cowling
Exhaust System for Gas Turbine
Process for Producing a Self-Healing Layer on a Part Made of a C/C Composite
Flexible Abutment Links for Attaching a Part Made of Cmc
Method for Producing Parts Made of a Thermostructural Composite Material
Composite Material Turbine Engine Vane, and Method for Manufacturing Same
Production of a Fibrous Structure with Variable Thickness by 3D Weaving
Method for Manufacturing a Complexly Shaped Composite Material Part
Method for Smoothing the Surface of a Part Made from a Cmc Material
Method for Processing Ceramic Fibers
Environmental Barrier for a Refractory Substrate Containing Silicon
Process for Smoothing the Surface of a Part Made of Cmc Material
Composite Material Part Having a Ceramic Matrix, and Method for Manufacturing Same
Application:
13/393,978 →
Publication:
US 2012/0164430
Method of Densifying Thin Porous Substrates by Chemical Vapor Infiltration, and a Loading Device for Such Substrates
Method of Fabricating a Thermostructural Composite Material Part, and a Part Obtained Thereby
Fiber Reinforcing Texture for Making a Composite Material Part
Low-Thickness Thermostructural Composite Material Part, and Manufacture Method
Turbine Engine Turbine Blade Made of a Ceramic-Matrix Composite with Recesses Made by Machining
Fiber Preform for a Turbine Ring Sector, and Its Method of Fabrication
Turbomachine Blades or Vanes Having Complementary Even/Odd Geometry
Turbomachine Blade or Vane Having Complementary Asymmetrical Geometry
Composite Material Turbomachine Engine Blade or Vane, Compressor Stator Segment or Turbine Nozzle Segment Incorporating Such Vanes and Method for Manufacturing Same
Composite Turbomachine Blade with In-Built Root
Turbine Engine Rotor Including Blade Made of Composite Material and Having an Added Root
Assembly Providing a Connection That Is Self Tightening with Temperature
Assembly Providing a Connection That Is Self Tightening with Temperature
Device for Loading Porous Substrates of Three-Dimensional Shape in Order to be Densified by Directed Flow Chemical Vapor Infiltration
Fastening Assembly Including a Fastening Device and a Hollow Part
Application:
14/353,840 →
Publication:
US 2014/0332604
Method of Fabricating a Turbine or Compressor Guide Vane Sector Made of Composite Material for a Turbine Engine, and a Turbine or a Compressor Incorporating Such Guide Vane Sectors
Method of Fabricating a Part Out of Cmc Material
Method of Fabricating a Composite Material Turbine Engine Vane with Incorporated Platforms
Hollow-Blade Turbine Vane Made from Composite Material, Turbine or Compressor Including a Nozzle or Guide Vane Assembly Formed by Such Blades, and Turbomachine Comprising Same
Ceramic Matrix Composite Material Part
Method of Treating Ceramic Fibers by Phosphating
Exhaust with an Acoustic Attenuation System
Structure for Fastening After-Body Parts of an Aeroengine
Method for the Treatment of Silicon Carbide Fibres
A Loader Device and an Installation for Densifying Stackable Frustoconical Porous Preforms
Chemical Vapour Infiltration Apparatus Having a High Loading Capacity
Method for the Brazing of Parts Made from a Composite Material, Incorporating a Slug in the Bond
Method for Brazing Parts Made from a Composite Material, with Anchoring of the Brazed Joint
Method for Manufacturing a Part Made of Cmc
Method of Locally Treating a Part Made of Porous Composite Material
Application:
14/434,496 →
Publication:
US 2015/0275671
Process for Smoothing the Surface of a Part Made of Cmc Material
Method for the Production of a Curved Ceramic Sound Attenuation Panel
Method for Producing a Curved Honeycomb Structure Made from Composite Material
Method for Producing a Composite Material with a Carbide Matrix
Application:
14/785,142 →
Publication:
US 2016/0060752
Rotor Disk Blade with Friction-Held Root, Rotor Disk, Turbomachine and Associated Assembly Method
Environmental Barrier for a Refractory Substrate Containing Silicon
Turbine Ring Assembly with Inter-Sector Connections
Turbine Ring Assembly with Sealing
Part Made from Oxide/Oxide Composite Material for 3-D Reinforcing and Method for Manufacture of Same
Sized Yarn Intended to Undergo a Textile Operation
Method for Treating Waste Gas Containing Polycyclic Aromatic Hydrocarbons
Stator Sector for a Turbine Engine, and a Method of Fabricating It
A Cvi Densification Installation Including a High Capacity Preheating Zone
Process for Manufacturing a Multiperforated Composite Part
Related Assignments
(9)
Other recorded transfers of the patents in this record — the chain of ownership.
Partial Transfer of Assets Agreement
Jan 10, 2014
From: SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION - SNECMA
To: LEXVALL
Reel/Frame 031968/0405 →
Change of Name
Jan 14, 2014
From: LEXVALL
To: SNECMA MOTEURS
Reel/Frame 031959/0577 →
Assignment of Assignor's Interest
Jan 24, 2014
From: SNECMA MOTEURS
To: LEXVALL 8
Reel/Frame 032040/0568 →
Change of Name
Jan 27, 2014
From: LEXVALL 8
To: SNECMA PROPULSION SOLIDE
Reel/Frame 032125/0681 →
Merger
Jan 29, 2014
From: SNECMA PROPULSION SOLIDE
To: HERAKLES
Reel/Frame 032135/0709 →
Merger
Apr 22, 2018
From: SNECMA PROPULSION SOLIDE
To: HERAKLES
Reel/Frame 046678/0308 →
Change of Name
May 16, 2018
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 045825/0950 →
Change of Name
May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
Corrective Assignment to Correct the Cover Sheet to Remove Application Nos. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 Previously Recorded on Reel 046479 Frame 0807. Assignor(S) Hereby Confirms the Change of Name.
Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →