Patent Assignment
Reel/Frame 046082/0606
Change of Name
Recorded: 2018-05-06
Pages: 9
Assignor
SAGEM DÉFENSE SÉCURITÉ
Executed: 2016-05-12
Assignee
SAFRAN ELECTRONICS & DEFENSE
18/20 QUAI DU POINT DU JOUR, 92100 BOULOGNE-BILLANCOURT, FRANCE
Covered Properties
(239)
Gyroscopic Sensor and Rotation Measurement Apparatus Constituting an Application Thereof
Patent:
6,474,161 →
Application:
09/720,103 →
Wheel Assembly Provided with a Pressure Sensor
Gyroscopic Sensor
Method for Managing Ground Assistance Teams of Locomotive Vehicles and Data Transmission System Therefor
Installation for Measuring Pressure of at Least One Aeroplane Wheel Tyre
Electromechanical Actuators
Resonator Paticularly for a Vibrating Gyroscope
Valve Control Device
Appliance for Reading Identification Connectors
Method for Implementing a Resonator Under Electrostatic Forces
Hemispherical Resonator with Divided Shield Electrode
Cooled Photosensitive Cell
Device for Powering Equipment, and an Equipment Power Supply System
One-Way Connection Device Suitable for Use in an Ethernet Network
Ventilation System for Electrical of Electronic Equipment
Method of Compensating Anisotropy in a Vibrating-Bell Inertial Rotation Sensor
Vibrating Resonator Inertial Rotation Sensor
Method of Exchanging Information Between Two Networks Operating Under Different Routing Protocols
Method of Exchanging Information Under Ip Protocol with Data Substitution in the Tos Field
Method of Controlling a Laser Gyro by the Amplitude of the Winking Signal
Method of Loading Files from a Client to a Target Server and Device for Implementing the Method
Secure Transmitting Method, a System, a Firewall, and a Router Using the Method
Method for Implementing a Resonator Under Electrostatic Forces
Method for Implementing a Resonator Under Electrostatic Forces
Imaging Device with Focus Switching Means for Day and Night Vision
Valve Control Device
Refrigerating Machine Using the Stirling Cycle
Cooled Cryostat Device
Rotors of High Power Engines
Improvement to the Materials of the Cylinders of Active-Piston Actuators
Materials of Active-Piston Actuators
Inertial Sensor with Disturbing Current Reduced by Reducing the Width and the Spacing of Tracks in Critical Zones
Changer of Spherical Field
Device for Moving a Body Linearly Between Two Predetermined Positions
Device for Remotely Controlling Aircraft Control Surfaces
Device for Artificially Restoring an Opposing Force for a Device for Remotely Controlling Aircraft Control Surfaces
Method of Managing the Supply of Electrical Power, an Electrical Power Supply Circuit, and a Method of Powering an Appliance When Cold
Battery, Electrical Equipment, and a Powering Method Implementing Means for Short-Circuiting the Battery
Method of Charging a Battery, and a Corresponding Charger and Battery
Hybrid Inertial Navigation System Based on a Kinematic Model
Method for Temperature-Compensated Gyrometric Measurement and Gyrometric Measurement Device Using Same
Piezoelectric-Motor-Driven Two-Axis Orientation Turret
Device for Countering and Tracking a Threat in the Form of a Homing-Head Missile
Method of Determining a Speed of Rotation of an Axially Symmetrical Vibrating Sensor, and a Corresponding Inertial Device
Method of Locating a Vehicle from Satellite Data
Device with Integrated Electronic Components Provided with a Partition for Separating Ventilated Zones
Illuminator for a Photolithography Device
Selective Connection Device Allowing Connection of at Least One Peripheral to a Target Computer and a Selective Control System Comprising Such a Device
Measurement by Gyroscopic System
Device for Protecting the Engageable Elements of a Connector
Undercarriage Fitted with a Communication Device Between a Wheel and the Undercarriage
Method of Managing Additional Filters in a Satellite Navigation System
Method of Determining a Speed of Rotation of an Axially Symmetrical Vibrating Sensor, and a Corresponding Inertial Device
Method of Aligning an Axisymmetric Vibrating Sensor Inertial Navigation System and Corresponding Inertial Navigation System.
Method of Determining a Heading in the Geographical North Direction by Means of an Inertial Unit
System for Protecting the Engagable Elements of a Connector
Method for Calibrating a Scale Factor in an Axisymmetrical Vibrating Gyrometer
Resonator for a Vibratory Sensor of an Angular Parameter
Gyroscopic Measurement by a Vibratory Gyroscope
Method for Maintenance of an Array of Bolometer-Type Detectors
Infrared Camera and Method for Observing a Scene
Method for Measuring an Acceleration Using a Piezoelectric Vibrating Accelerometer
Method and System for Detecting Multiple Paths in a System of Satellite Navigation
Acoustic Headset
Bidirectional Gateway with Enhanced Security Level
Method for Monitoring the Output of an Electromechanical Actuator of the Rotary-Linear Type
Ac/Dc Converter Having Isolating Transformer with Three Secondary Windings
Method of Correcting the Gain of a Capacitive Member, and a Device for Implementing the Method
Vibrating Sensor Having Two Channels Activated in Sequence
Rotolinear Actuator with Satellite Rollers
Mass Memory Device and Storage System
Application:
12/864,484 →
Publication:
US 2010/0299476
Correction of Captured and Stabilized Images
Drift-Compensated Inertial Rotation Sensor
Active Damping Circuit for Electric Chopper Circuit
Assembly of Actuators and of a System for Supplying Electrical Power from a Network
Stabilization of Captured Images
Avionic System Comprising a Controller and at Least One Peripheral That Are Linked by a Line Mutualized for Power and Data
Device for Reconstructing the Clock of an Nrz Signal, and Associated Transmission System
Method for Controlling a Sensor with a Quick-Start Vibrating Resonator
Calibration of Gyroscopic Systems with Vibratory Gyroscopes
Secure Avionics Equipment and Associated Method of Making Secure
Calibration of Vibratory Gyroscope
Actuator with Load Cell
Hybridization Device with Segregated Kalman Filters
Integrated Closed-Loop Hybridization Device Built in by Construction
Electric Motor Braking System for Rotolinear Actuator
Electrical Pack with Separate Control and Power Modules
Modular Electrical Card for Power Components
Rotary-Linear Actuator with Optimised Rollers
Engine and Pod Assembly for an Aircraft, Equipped with an Anti-Icing Device Including a Source of Radiation and Pulse Control Unit Connected to the Source of Radiation
Photosensitive Resin Composition and Cured Film
Aircraft Flight Control System Comprising a Connecting Rod Provided with a Sensor
Engine Power Supply Circuit, and Flight Control Member Provided with Such a Circuit
Actuator System for a Mobile Panel of a Nacelle of a Turbojet
Method and System for Conserving Operating Data of a Vehicle
Aircraft Engine Nacelle Comprising a Mobile Cowl Moved by Electric Motors
Acquisition Method with Improved Multi-Frequency Correlation
Device for Actuating a Control Surface of an Aircraft
Excitation Circuit for Dc Sensors
Method of Determining Navigation Parameters for a Carrier and Hybridization Device
Method of Determining Navigation Parameters for a Carrier and Hybridization Device Associated with Kalman Filter Bank
Method and System for Determining Protection Limits with Integrated Extrapolation Over a Given Time Horizon
Method for Determining the Navigation Speed of a Carrier and Hybridization Device
Vibrating Gyroscope and Treatment Process
Method of Detecting Parasitic Movements While Aligning an Inertial Unit
Application:
13/497,218 →
Publication:
US 2012/0185205
Variable Damping Circuit for a Synchronous Servomotor
Aircraft Throttle Control Device Including a Cam Coupling
Application:
13/500,824 →
Aircraft Throttle Control Device Including an Engaging Roller Coupling
Electronic Control Unit Having a Real-Time Core Managing Partitioning
Method and Device for Long-Duration Navigation
Assembly of Apparatuses for Implementing Data Transmission via the Human Body
Application:
13/502,482 →
Publication:
US 2012/0198596
Resonator with a Partial Metal-Plated Layer
Angular Position Sensor and Assembly Comprising a Rotary System and Such a Sensor
Resonator Including a Passivation Layer, a Vibrating Sensor Including Such a Resonator, and a Method of Manufacture
Gyroscopic Sensor
Gyroscopic Sensor and Method for Manufacutring Such a Sensor
Method of Determining Heading by Turning an Inertial Device
Method of Determining Heading by Turning an Inertial Device
Method for Detecting the Failure of a Frequency Sensor, and Circuit for Implementing Said Method
Device for Displaying Critical and Non-Critical Information, and Aircraft Including Such a Device
Device for Connecting Two Apparatuses via an Ethernet Link, and Docking Station for One of Said Apparatuses
Method for Detecting a Breakdown in a Switching Current Source and Corresponding Power Source
Global and Dense Motion Estimation
Device for Controlling an on-Board Apparatus
Secure Procedure for Accessing a Network and Network Thus Protected
Method of Angular Measurement by Means of a Vibrating Sensor to Which Modulated Controls Are Applied
Method and Device for Angular Measurement with Compensation of Non-Linearities
Calibration of Vibrating Gyroscope
Gyroscopic Measurement in a Navigation System
Gyroscopic Measurement by a Gyroscope Vibrating in Precession
Power Supply and Control Device for Actuators, Corresponding Actuation Assembly, and Aircraft Comprising Such a Device
Device for Generating Return Forces for Sticks Such as Aircraft Control Sticks
Low-Noise Bioccular Digital Vision Device
Application:
13/807,885 →
Publication:
US 2013/0100262
Method of Detecting a Fault in a Permanent-Magnet Alternator and Power Supply Device Comprising a Detector Module
Method for Detecting and Excluding Multiple Failures in a Satellite
Method and System for Analysing Flight Data Recorded During a Flight of an Aircraft
Application:
13/813,014 →
Publication:
US 2013/0218823
Passive Mechanical Athermalization Device, and Related Optical System
Method and Device for Detecting and Excluding Multiple Satellite Failures in a Gnss System
Optoelectronic Device for Observing and/or Aiming at a Scene, Comprising a Rangefinder, and Related Range-Finding Method
Actuation System for a Propulsive Unit of an Airplane
System for Motorized Displacement of a Mobile Element, Method of Driving Such a System and Method of Testing Such a System
Electronic Card, an Electronic Device Including Such a Card, and a Method of Protecting an Electronics Card
Predictive Maintenance Method for a Cooled Detection Module, and Related Module
Inertial Unit Having Vibrating Gyros Mounted on a Carousel, and an Angle-Measurement Method
Module for Converting Voltage Between a High-Voltage Electrical Network of an Aircraft and an Energy Storage Element
Device for Actuating an Item of Equipment That Can Be Controlled Automatically or Manually, with Detection of Take-Up of Manual Control
Device for Multiple Ethernet Connection to a Computer Unit and Computer Unit Assembly and Equipment Linked Together
Application:
13/992,974 →
Publication:
US 2013/0268684
Vibrating Gyroscope and Corresponding Manufacturing Process
High-Resolution Compact Gamma Burst Detector
Method of Operating Actuators Simultaneously for Moving Aircraft Flaps, an Aircraft Flap Drive Device, and an Aircraft Provided with Such a Device
High-Resolution Imaging System
Method for Updating a Value of Orientation with Respect to North or for Improving the Initialization of Such a Value in an Apparatus Comprising an Image Sensor
Assembly for the Electronic Processing of Data with Mutualized Resources
Detection and Correction of Carrier Phase Inconsistency During the Tracking of a Radio Navigation Signal
Method and Device for Connecting to a High Security Network
Method and System for Detecting a Short Circuit Affecting a Sensor
Fluxgate with Laminar Damping of the Pendulum and Method of Assembling a Fluxgate
Inertial Navigation System Using Hybrid Navigation via Integrated Loose Coupling
Method for Correcting the Voltage Measured Across the Terminals of a Sensor
Orientation Device Including Means for Detecting That the Device Is Lying Flat on a Support
Method of Calibrating an Inertial Assembly Comprising a Dynamic Phase Between Two Static Phases
Method for Remotely Determining an Absolute Azimuth of a Target Point
Garment for Ballistic Protection and Carrying Equipment
Removable Communication Cartridge That Can Be Detached from an Equipment, Equipment, Assembly and System Corresponding Thereto
Method for Managing Access to a Shared Communication Medium
Ac/Dc Converter with Galvanic Insulation and Signal Corrector
Multiaxis Drive Device and Control Instrument Fitted with Such a Device
Actuator Having a Multiphase Motor, and a Method of Controlling Such an Actuator
Method of Sequencing on a Multicore Processor
Search for a Target in a Multispectral Image
An Electromechanical Actuator for an Aircraft Control Surface, and an Aircraft Provided with Such an Actuator
Mechanical Member
Device for Connecting Two Pieces of Equipment via an Ethernet Link, and a Docking Station for Such a Piece of Equipment
Method of Analysing Flight Data
A Method for Analyzing Flight Data Recorded by an Aircraft in Order to Cut Them Up into Flight Phases
Application:
14/389,958 →
Publication:
US 2015/0331975
Device and Method for Active Control of a Force Feedback for a Control Device
Actuating Device for Moving a Thrust Reverser
Actuating Device for Moving a Movable Cover of a Thrust Reverser
Aircraft Avoidance Method and Drone Provided with a System for Implementing Said Method
Electronic Module for a Piece of Vehicle-Borne Aeronautic Equipment and a Piece of Aeronautic Equipment for an Aeronautic Vehicle
Method for the Management of Task Execution in a Computer System
Electronic Power Module Arrangement
Joystick for Controlling an Aircraft
Joystick for Controlling an Aircraft
Device for Linking an Electrical Member to a Communication Line
Electric Circuit for Cutting Off an Electric Power Supply Having Transistors and Fuses
Electric Circuit for Cutting Off an Electrical Supply with Relay and Fuses
Electrical Circuit for Cutting Off an Electric Power Supply Comprising Transistors and Fuses Having Redundant Logic
Electromechanical Actuator with Anti-Blocking Means
Photolithographic Illuminator That Is Telecentric in Two Directions
Photolithographic Illuminator Device Enabling Controlled Diffraction
Pressure Sensor Made from Nanogauges Coupled to a Resonator
Configurable Generic Electrical Facility
Application:
14/434,061 →
Publication:
US 2015/0241874
Actuating Device Including a Primary Locking Device
Pcmcia Card for Transferring Flight Data
Lightning Protection Component
Energizing Hydrogenerator
Magnetic Brake Having Reduced-Notching Hysteresis
Application:
14/442,309 →
Publication:
US 2016/0285352
Method for Integrity Monitoring of Satellite Measurements
Method and Device for Determining the Propagation Time of a Surface Acoustic Wave Filter
Application:
14/647,815 →
Publication:
US 2015/0293204
Method for Calibrating an Inertial Navigation System with a Limited Mechanical Turning Range
Input/Output Device Transferring Receiving Data to Control Device Over Physical Ethernet Connection Using Frame Construction with Udp/Ip and Mac Transmission Layers
Method for Demodulating at Least One Frame Consisting of a Succession of Bits Coded According to a Manchester Code
Device for Detecting an Angular Travel of a Vehicle Control Member
Application:
14/651,121 →
Publication:
US 2015/0330810
Redundant Electric Circuit for Cutting Off the Power Supply to a Piece of Equipment
Method for Comparing Two Inertial Units Integral with a Same Carrier
Application:
14/655,523 →
Publication:
US 2016/0116302
Estimation of the Movement of an Image
Method and Device for Filtering Transactions for an on-Chip System
Application:
14/772,059 →
Publication:
US 2016/0019180
Method for Monitoring Communications for an on-Chip System
Application:
14/772,060 →
Publication:
US 2016/0019175
Bandwidth Control Method for an on-Chip System
System for Detection and Imaging by Spectral Analysis in Several Wavelength Bands
Actuation Device for Moving a Movable Cover of a Thrust Reverser
Electric Motor Having a Low Short-Circuit Torque, Drive Device with a Plurality of Motors and Method for Producing Such a Motor
Integrity Control Method and Merging/Consolidation Device Comprising a Plurality of Processing Modules
Application:
14/785,295 →
Publication:
US 2016/0084655
Device for Differential Acquistion of Current and Method of Controlling Such an Acquisition Device
Method for Controlling a Piezoelectric Device Having a Piezoelectric Element Mounted on a Substrate
Device for Controlling the Power of an Engine and for Controlling a Thrust Reverser Device
Stator Comprising a Split Core and Method for Producing Such a Stator
Component and Method for Managing Communication
Method for the Autonomous Calibration of an Inertial Rig Used in Static Mode
Actuation Device for Moving a Movable Cowling of a Thrust-Reverser
Fly-By-Wire Control System for Aircraft
Method of Managing Consistency of Caches
Device for Driving Actuators for a Thrust Reverser, Comprising a Disengageable Manual Drive Unit
Device for Driving Actuators for a Thrust Reverser, Selectively Allowing Motorised or Manual Driving
Actuating device for displacing a part of the empennage of a helicopter
Device for Transmitting Movement to a Position Senser and Corresponding Device for Sensing Position
Telescopic Actuator and Aircraft Engine Comprising Such an Actuator
Application:
15/022,833 →
Publication:
US 2016/0229546
Method for Viewing a Multi-Spectral Image
Flight Control Device for an Aircraft
Actuator Device for Moving a Movable Cowl of a Thrust Reverser
Sensor with Moving Sensitive Element Having Mixed Vibrating and Pendular Operation, and Methods for Controlling Such a Sensor
Alignment Method for an Inertial Unit
Detection and Correction of Carrier Phase Inconsistency During the Tracking of a Radio Navigation Signal
Application:
15/053,565 →
Publication:
US 2016/0178753
Analysis of a Multispectral Image
Analysis of a Multispectral Image
Electric Actuator with a Manual Drive Means
Device with Two Interlocked Gear Trains
Actuating Device for Moving a Movable Cover of a Thrust Reverser
Related Assignments
(6)
Other recorded transfers of the patents in this record — the chain of ownership.
Merger
Oct 25, 2012
From: SNECMA SERVICES
To: SNECMA
Reel/Frame 029191/0943 →
Assignment of Assignor's Interest
Oct 25, 2012
From: HISPANO SUIZA
To: SAGEM DEFENSE SECURITE
Reel/Frame 029192/0547 →
Change of Name
Dec 8, 2016
From: MESSIER-BUGATTI-DOWTY
To: SAFRAN LANDING SYSTEMS
Reel/Frame 040851/0908 →
Transfer of Patent Resulting from a Partial Contribution of Assets
May 6, 2018
From: SAGEM SA
To: SAGEM DÉFENSE SÉCURITÉ
Reel/Frame 047020/0060 →
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 →