Patent Assignment
Reel/Frame 064424/0050
Termination and Release of Security Interest in Patents
Recorded: 2023-07-28
Pages: 14
Assignor
Assignee
AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
P.O. BOX 13222, SACRAMENTO, CALIFORNIA, 95813-6000
Covered Properties
(128)
Laser Ignition for Liquid Propellant Rocket Engine Injectors
Patent:
9,255,549 →
Application:
08/896,737 →
Hydrostatically Supported Foil Bearing
Patent:
5,885,004 →
Application:
08/979,357 →
Laser Ignition for Liquid Propellant Rocket Engine Injectors
Patent:
9,347,399 →
Application:
08/988,059 →
Tire Track Roughened Orifice Compensated Hydrostatic Bearing
Patent:
6,056,441 →
Application:
08/991,256 →
Convective and Turbulent Shear Mixing Injector
Patent:
6,253,539 →
Application:
09/348,402 →
Annular Bearing with Diffuser and Inlet Flow Guide
Patent:
6,318,896 →
Application:
09/438,089 →
High Suction Performance and Low Cost Inducer Design Blade Geometry
Patent:
6,435,829 →
Application:
09/497,578 →
Composite Rotor Having Recessed Radial Splines for High Torque Applications
Patent:
6,595,751 →
Application:
09/590,548 →
Integral propulsion and power radiant cavity receiver
Patent:
6,311,476 →
Application:
09/590,624 →
Thruster Device Responsive to Solar Radiation and Associated Methods
Patent:
6,421,998 →
Application:
09/592,724 →
Turbine Blisk Rim Friction Finger Damper
Patent:
6,375,428 →
Application:
09/636,536 →
Article Having Imbedded Cavity
Article Having Dampening Member Installed into an Imbedded Cavity
Variable-Gravity Anti-Vortex and Vapor-Ingestion-Suppression Device
Rotating Solar Concentrator
Patent:
6,557,804 →
Application:
10/007,403 →
Apparatus and Method for Initiating a Combustion Reaction with Slurry Fuel
Combined Thrust and Power Generator for a Satellite
Split Blade Frictional Damper
Thruster Device Responsive to Solar Radiation and Associated Methods
Method and Apparatus for a Rocket Engine Power Cycle
Patent:
7,216,477 →
Application:
10/098,955 →
Turbine Blade Assembly with Pin Dampers
Turbine Blade Assembly with Stranded Wire Cable Dampers
Diffuser Having a Variable Blade Height
Combustion Chamber Having a Multiple-Piece Liner and Associated Assembly Method
Method for Forming a Tube-Walled Article
Torch Igniter
Compact, Lightweight High-Performance Lift Thruster Incorporating Swirl-Augmented Oxidizer/Fuel Injection, Mixing and Combustion
Apparatus and Method for Electroplating a Metallic Film on a Rocket Engine Combustion Chamber Component
Method and Apparatus for a Substantially Coaxial Injector Element
Direct Illumination Free Piston Stirling Engine Solar Cavity
Patent:
6,735,946 →
Application:
10/324,699 →
Compact Lightweight Ramjet Engines Incorporating Swirl Augmented Combustion with Improved Performance
Apparatus for Mixing Fluids
Design and Assembly of a Catalyst Bed Gas Generator for the Catalytic Decomposition of High Concentration Hydrogen Peroxide Propellants and the Catalytic Combustion of Hydrocarbon/Air Mixtures
High-Temperature Catalyst for Catalytic Combustion and Decomposition
Method of Generating Thrust and Electrical Power from an Optical Solar Image
Engine Spectrometer Probe and Method of Use
Thermal Cycle Engine Boost Bridge Power Interface
Hypergolic Azide Fuels with Hydrogen Peroxide
Method and Apparatus for Solar Power Conversion
Variable-Gravity Anti-Vortex and Vapor-Ingestion-Suppression Device
Trough-Stirling Concentrated Solar Power System
Bi-Propellant Injector with Flame-Holding Zone Igniter
Diffusion Bonded Composite Material and Method Therefor
Method and Apparatus for Producing a Refined Grain Structure
Thruster Device Responsive to Solar Radiation and Associated Methods
Bearing Cup Rotational Lock Assembly
Methods and Apparatuses for Removing Thermal Energy from a Nuclear Reactor
Solar Electrolysis Power Co-Generation System
System and Fabrication Method for Actively Cooling High Performance Components
Inducer Tip Vortex Suppressor
Advanced L-Channel Welded Nozzle Design
Inlet Partial Blades for Structural Integrity and Performance
High Temperature Power Supply
Combustion Wave Ignition for Combustors
Inducer with Shrouded Rotor for High Speed Applications
Torch Igniter
Fluid Injector and Injection Method
High Speed Rotor Assembly Shroud
Gaseous Oxygen Resonance Igniter
Spherical Flange Assembly
Shaft Seal Assembly and Method
Deployable Electromagnetic Concentrator
Rocket Engine Nozzle and Method of Fabricating a Rocket Engine Nozzle Using Pressure Brazing
Thermal Cycle Engine with Augmented Thermal Energy Input Area
Injector Assembly Having Multiple Manifolds for Propellant Delivery
Method and Apparatus for Solar Power Conversion
Piezo-Resonance Igniter and Ignition Method for Propellant Liquid Rocket Engine
Method and Apparatus for Solar Power Conversion
Spherical Flange Assembly
Method and Apparatus for a Rocket Engine Power Cycle
Constant Moment Testing Device for Elongated Members
System and Method for Detecting Onset of Structural Failure
Fully Shielded Backshell for Electrical Connector
Fuel Cell Instrumentation System
Resonance Driven Glow Plug Torch Igniter and Ignition Method
Application:
11/756,642 →
Publication:
US 2008/0299504
Locking Fastening Apparatus
Ultra-Compact, High Performance Aerovortical Rocket Thruster
Compact, High Performance Swirl Combustion Rocket Engine
Damper Root Ring
Characteristic X-Ray Computed Laminography System for Home Made Explosives (Hme) Detection
Neutron-Gamma Ray Tomography
Method of Animating Structural Vibration Under Operational Conditions
Rocket Engine Power Cycle
Brazed Nano-Grained Aluminum Structures
Extended Range Projectile
Patent:
7,823,510 →
Application:
12/120,345 →
Guided Projectile
Igniter/Thruster with Catalytic Decomposition Chamber
Sequence Diagram System
Low Velocity Injector Manifold for Hypergolic Rocket Engine
Method of Fabricating a Rocket Engine Nozzle Using Pressure Brazing
Solid state heat pipe heat rejection system for space power systems
Passive Electrical Components with Inorganic Dielectric Coating Layer
Spherical Flange Assembly
Patent:
43,080 →
Application:
12/370,887 →
Superalloy Powder, Method of Processing, and Article Fabricated Therefrom
Piezo-Resonance Igniter and Ignition Method for Propellant Liquid Rocket Engine
Cooling Device and Method with Synthetic Jet Actuator
Panel Assembly for a Space-Based Power Generation System
Failure Detection System Risk Reduction Assessment
Method of Processing a Bimetallic Part
Injector Assembly Having Multiple Manifolds for Propellant Delivery
Nuclear Fuel
Structure Having Nanophase Titanium Node and Nanophase Aluminum Struts
High Temperature Flexible Electrode
Application:
12/879,608 →
Publication:
US 2012/0060886
Substrate Having Laser Sintered Underplate
Optical Power Converter
HIGH TEMPERATURE STABLE NANOCRYSTALLINE SiGe THERMOELECTRIC MATERIAL
Center-Tapped Solar Array and Power Distribution System for Same
Thrust Chamber and Rocket Engine System
Method for Treating a Porous Article
Method for Manufacturing a Ceramic Composite Article
Airfoil Tip Shroud Damper
Patent:
8,105,039 →
Application:
13/078,567 →
Power Converter
Thermoelectric Power Converter Support Structure
Rotary Engine with Exhaust Gas Supplemental Compounding
Charge Balancing Topology
Launch Abort and Orbital Maneuver System
Apparatus for Electrical Isolation of Metallic Hardware
A Method of Assembling a Thermal Expansion Compensator
Scissor Duct Flex Joint Damper
Fluid Separation System with Reduced Fouling
Self Retaining Anti-Rotation Key
Nitrous Oxide System for Producing Breathing Air
System for Bypassing and Isolating Electrical Power Cells
Blade Shroud for Fluid Element
Solar Receiver
Ceramic Article and Additive Processing Method Therefor
Application:
13/475,275 →
Publication:
US 2013/0307201
Tuned Damper Member
Patent:
8,544,597 →
Application:
13/484,595 →
Fuel-Cracking Diesel Engine System
Related Assignments
(14)
Other recorded transfers of the patents in this record — the chain of ownership.
Change of Name
Jul 30, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 030902/0313 →
Change of Name
May 8, 2014
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 032845/0909 →
Change of Name
Aug 5, 2014
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 033474/0766 →
Change of Name
Feb 25, 2016
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 037918/0042 →
Change of Name
Feb 25, 2016
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 037918/0126 →
Change of Name
May 14, 2016
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 038707/0175 →
Assignment of Assignor's Interest
May 17, 2016
From: VAN DAAM, THOMAS J; HOSKING, TIMOTHY J
To: THE BOEING COMPANY
Reel/Frame 038619/0742 →
Assignment of Assignor's Interest
May 17, 2016
From: FRYE, PATRICK E; CARROLL, JOSEPH P; SHOJI, JAMES M
To: THE BOEING COMPANY
Reel/Frame 038618/0599 →
Notice of Grant of Security Interest in Patents
Jun 17, 2016
From: AEROJET ROCKETDYNE, INC., SUCCESSOR-IN-INTEREST TO RPW ACQUISITION LLC
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 039197/0125 →
Notice of Succession of Agency (Intellectual Property)
Jun 20, 2016
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS THE RESIGNING AGENT
To: BANK OF AMERICA, N.A., AS THE SUCCESSOR AGENT
Reel/Frame 039079/0857 →
Release of Security Interest
Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
Notice of Grant of Security Interest in Patents
Sep 27, 2018
From: AEROJET ROCKETDYNE OF DE, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 047157/0231 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 064423/0993 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064424/0109 →