Patent Assignment
Reel/Frame 046678/0487
Change of Name
Recorded: 2018-04-22
Pages: 4
Assignor
LABINAL POWER SYSTEMS
Executed: 2016-05-03
Assignee
SAFRAN ELECTRICAL & POWER
PARC D'ACTIVITÉ ANDROMÈDE, 1, RUE LOUIS BLÉRIOT, CS 80049, 31702 BLAGNAC CEDEX, FRANCE
Covered Properties
(72)
Electrical Connection Device and Power Distribution Apparatus Comprising It
Electromechanical Turbojet Thrust Reverser with Continuous Position Control
Maintenance and Inhibition Plate for a Thrust Reverser
Turbojet Electromechanical Thrust Reverser with Synchronized Locking Devices
Turbojet Electromechanical Thrust Reverser with Servo-Controlled Door Displacement
System for Modifying the Structure of an Electrical Harness
12-Pulse Converter Including a Filter Choke Incorporated in the Rectifier
Device for Cutting and Marking a Metal Cable
Electrical Cabinet Including a Wiring Support
Turbomachine with Integral Generator/ Starter
Electrical Power Supply Arrangement for an Aircraft
System for Powering and Controlling Electrical Equipment of an Aircraft Engine or Its Environment
Distributed Architecture for a Gas-Turbine Starter/Generator
Electrical Power Supply Circuit in an Aircraft for Electrical Equipment Including a De-Icing Circuit
Turbomachine with Integral Generator/Starter
Storage Device for the Overlength of an Optical Fiber or Other Type of Cable
Support Device for an Electrical Harness Passing Through a Structure
Electronic Control Module for a Jfet Transistor
Cable Way for Aircraft with a Structure Made of Composite Material
Expandable Cableway for Aircraft with a Structure Made of Composite Material
Device for Supporting and Securing a Piece of Equipment on an Aircraft Engine or Nacelle Case
Method of Extending the Individual Electromagnetic Shielding of Electrical Strands in a Twisted-Strand Cable to an Electrical Connector
Connection Device Between an Electrical Cable and a Conducting Structure, Especially for a Current Return Circuit
Electrical System for Starting Up Aircraft Engines
Turbine Engine Starter/Generator, and Method for the Control Thereof
Device for Control of a Pmsm
Aircraft Including an Electric Starter-Generator for the or Each Turbojet, an Undercarriage Fitted with an Electric Motor for Taxiing, an Electricity Converter, and an Electricity Distribution Unit Connecting the Electricity Converter to the Starter-Generator and the Electric Motor
Method and Device for Controlling a Polyphase Electrical Machine
Actuating Blades of an Unducted Fan
Power Supply Circuit for an Aircraft De-Icing System
Voltage Inverter and Method of Controlling Such an Inverter
Electric Power Supply for Apparatuses Supported by the Rotor of an Aircraft Engine
Electrical Power Supply for Equipment Carried by a Rotary Support
Printed Circuit Comprising at Least One Ceramic Component
Aircraft Power Supply Circuit Including an Asynchronous Machine
Method and Architecture for Processing Electrical Energy Regenerated from an Aircraft
Module for Converting Voltage Between a High-Voltage Electrical Network of an Aircraft and an Energy Storage Element
Simplified Control Method for a Three-Phase Ac Voltage-Dc Voltage Converter
Rotary Mechanical System with Contactless Actuation
Application:
14/357,623 →
Publication:
US 2014/0322017
Electronic Device with Cooling by a Liquid Metal Spreader
Connection, Method, Equipotential Shunt Connection and Equipotential Bonding Current Return Network in a Non-Conductive Architecture
Application:
14/372,802 →
Publication:
US 2014/0354043
Control of a Permanent-Magnet Electric Machine
Device for Supplying Electrical Power to an Aircraft on the Ground
Three-Phase-Two-Phase Stationary Transformer with Forced Linked Flux
Turbine Engine Incorporating Thermoelectric Generators
Current Return Connecting Loom and Method for Mounting on a Composite Fuselage Frame
Application:
14/396,574 →
Publication:
US 2015/0136478
Method for Connecting the Conductors of a Flexible Bonded (Equipotential) Connection Layer
Three Phase Rotary Transformer with Free Linked Fluxes
Magnetically Shielded Three-Phase Rotary Transformer
Magnetically Shielded Three Phase Rotary Transformer Having Three Magnetic Cores
Three-Phase/Two-Phase Rotary Transformer
Control and Power Supply System for Helicopter Turbine Engines
Electrical Circuit for the Interconnection of an Electrical Component, Such as a Power Component
Method and Configuration for an Auxiliary Power Engine to Deliver Propulsive and/or Non-Propulsive Energy in a Helicopter Architecture
Device and Method for Monitoring an Electrical Network
Three-Phase/Two-Phase Rotary Transformer Including a Scott Connection
Coiled Power Device Comprising a Winding of a First Coiling and a Winding of a Second Coiling Which Cover the Same Portion of a Magnetic Core Member
Electromechanical Actuation and/or Generation System Including an Electrical Insulation Between the Electrical Source and the Load
System and Method for Monitoring a Meshed Current Return Network of an Aircraft
Application:
14/438,772 →
Publication:
US 2015/0293163
Method for Converting Alternating Current into Direct Current and Related Device
Dc-Dc High Voltage Converter
Measurement of the Homogeneous Temperature of a Coil by Increasing the Resistance of a Wire
A System for Recovering and Converting Kinetic Energy and Potential Energy as Electrical Energy for an Aircraft
Manufacture of Coils for Electrotechnical Components Using Strips of Unsealed Anodized Aluminum
Electrical Power Distribution Assembly for an Aircraft
Protective Sheath for an Electrical Harness in Order to Prevent the Deterioration of Same
Electrical Connector for Detecting Discontinuities in an Electrical Network
Assistance Device and Method for a Power Generation System of an Aircraft
A Method of Characterizing a Bundle of Electric Cables
Starter-Generator Brush
Electrically Controlled Switching Device Including Shape Memory Alloy Element
Method for Cooling an Electricity Generator and Device for Performing Said Method
Application:
15/104,941 →
Publication:
US 2017/0005548
Related Assignments
(5)
Other recorded transfers of the patents in this record — the chain of ownership.
Transfer of Patent Rights
Feb 11, 2015
From: HISPANO SUIZA
To: LABINAL POWER SYSTEMS
Reel/Frame 034948/0716 →
Transfer of Patent Rights
May 12, 2015
From: HISPANO SUIZA
To: LABINAL POWER SYSTEMS
Reel/Frame 035654/0789 →
Change of Name
Apr 22, 2018
From: LABINAL
To: LABINAL POWER SYSTEMS
Reel/Frame 047111/0012 →
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 →