Patent Assignment
Reel/Frame 039079/0857
Notice of Succession of Agency (Intellectual Property)
Recorded: 2016-06-20
Pages: 26
Assignor
WELLS FARGO BANK, NATIONAL ASSOCIATION, AS THE RESIGNING AGENT
Executed: 2016-06-17
Assignee
BANK OF AMERICA, N.A., AS THE SUCCESSOR AGENT
901 MAIN STREET, TX1-492-14-06, DALLAS, TEXAS, 75202
Covered Properties
(217)
Combustible Compositions for Air-Augmented Rocket Engines
Patent:
6,736,912 →
Application:
05/783,919 →
Rocket Engine Auxiliary Power System
Patent:
5,873,241 →
Application:
07/704,537 →
Method and Apparatus for Cutting Blocks of Solid Energetic Materials
Patent:
5,881,619 →
Application:
08/080,890 →
Process for Preparing Spherical Energetic Compounds
Patent:
5,801,453 →
Application:
08/661,437 →
Rocket-Ramjet Engine Casing Port Closure
Patent:
5,784,877 →
Application:
08/745,641 →
Apparatus and Method for Simulating Rocket-to-Ramjet Transition in a Propulsion System
Patent:
5,831,155 →
Application:
08/758,867 →
A Closed Electron Drift Hall Effect Plasma Accelerator with All Magnetic Sources Located to the Rear of the Anode
Patent:
5,751,113 →
Application:
08/760,952 →
Hall Effect Plasma Accelerator
Patent:
5,847,493 →
Application:
08/761,948 →
Hall Effect Plasma Thruster
Patent:
5,845,880 →
Application:
08/763,692 →
Method of Inductive Bonding Sintered Compacts of Heavy Alloys
Patent:
5,760,378 →
Application:
08/843,903 →
Liquid Oxygen Gasifying System for Rocket Engines
Patent:
5,918,460 →
Application:
08/850,259 →
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 →
Tire Track Roughened Orifice Compensated Hydrostatic Bearing
Patent:
6,056,441 →
Application:
08/991,256 →
Method Manufacturing Solid Rocket Motors
Patent:
6,408,760 →
Application:
08/993,811 →
Chemically Active Fire Suppression Composition
Patent:
6,024,889 →
Application:
09/015,359 →
Apparatus for Preparing Spherical Energetic Compounds
Patent:
5,962,803 →
Application:
09/047,678 →
Three Axis Thruster
Patent:
6,173,565 →
Application:
09/058,314 →
Rocket Engine with One-Piece Combustion Chamber Step Structure, and Its Fabrication
Patent:
6,079,101 →
Application:
09/076,032 →
High Performance Rocket Engine Having a Stepped Expansion Combustion Chamber and Method of Making the Same
Patent:
6,397,580 →
Application:
09/112,390 →
Rocket Motor Case Using Plank Sections and Methods of Manufacturing
Patent:
7,484,353 →
Application:
09/119,516 →
Method and Apparatus for Selectively Distributing Power in a Thruster System
Patent:
6,031,334 →
Application:
09/143,294 →
Castable Double Base Solid Rocket Propellant Containing Ballistic Modifier Pasted in an Inert Polymer
Patent:
6,024,810 →
Application:
09/166,942 →
Hydrostatic Bearing with Compensatory Fluid Injection
Patent:
6,053,636 →
Application:
09/189,335 →
Magnetic Flux Shaping in Ion Accelerators with Closed Electron Drift
Patent:
6,208,080 →
Application:
09/191,749 →
Multistage Ion Accelerators with Closed Electron Drift
Patent:
6,215,124 →
Application:
09/251,530 →
Convective and Turbulent Shear Mixing Injector
Patent:
6,253,539 →
Application:
09/348,402 →
Axial Flow Catalyst Pack
Patent:
6,746,651 →
Application:
09/371,973 →
Apparatus to Separate Gas from a Liquid Flow
Patent:
6,342,092 →
Application:
09/414,223 →
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 →
Uniform Gas Distribution in Ion Accelerators with Closed Electron Drift
Patent:
6,612,105 →
Application:
09/674,463 →
Article Having Imbedded Cavity
Catalyst Bed
Gas Generator for Producing Adjustable Flow
Article Having Dampening Member Installed into an Imbedded Cavity
Rocket Vehicle Thrust Augmentation Within Divergent Section of Nozzle
Method for Preparing Refractory Carbides
Solid Rocket Motor Bolted Thrust Takeout Structure
Apparatus to Separate Gas from a Liquid Flow
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
Heat Exchanger Panel
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 →
High Performance Rocket Engine Having a Stepped Expansion Combustion Chamber and Method of Making the Same
Turbine Blade Assembly with Pin Dampers
Turbine Blade Assembly with Stranded Wire Cable Dampers
Solid Propellant Formulations and Methods and Devices Employing the Same for the Destruction of Airborne Biological and/or Chemical Agents
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
Hall Effect Thruster with Anode Having Magnetic Field Barrier
Patent:
6,982,520 →
Application:
10/241,820 →
Compact, Lightweight High-Performance Lift Thruster Incorporating Swirl-Augmented Oxidizer/Fuel Injection, Mixing and Combustion
Variable Geometry Inlet Design for Scram Jet Engine
Apparatus and Method for Electroplating a Metallic Film on a Rocket Engine Combustion Chamber Component
Nozzle with Spiral Internal Cooling Channels
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 →
Diversion of Combustion Gas Within a Rocket Engine to Preheat Fuel
Compact Lightweight Ramjet Engines Incorporating Swirl Augmented Combustion with Improved Performance
Hypergolic Fuel System
Expander Cycle Rocket Engine with Staged Combustion and Heat Exchange
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
Propulsion System with Integrated Rocket Accelerator
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
Rocket Engine Tubular Chamber with Single Piece Jacket
Rocket Engine Combustion Chamber
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
Multichannel Hall Effect Thruster
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
Enhanced Performance Torroidal Coolant-Collection Manifold
Integrated Air Inlet System for Multi-Propulsion Aircraft Engines
Inducer with Shrouded Rotor for High Speed Applications
Torch Igniter
Fluid Injector and Injection Method
High Speed Rotor Assembly Shroud
Gaseous Oxygen Resonance Igniter
Reduced Gain Thrust Control Valve
Cooling Scheme for Scramjet Variable Geometry Hardware
High Temperature Dynamic Seal for Scramjet Variable Geometry
Single Phase Tungsten Alloy
Spherical Flange Assembly
Shaft Seal Assembly and Method
Staged Emitter-Attractor Ion Drive
Energetic Detonation Propulsion
Cryogenic Insulation
Deployable Electromagnetic Concentrator
Method of Assembling a Rocket Engine with a Transition Zone Between the Combustion Chamber and the Coolant System
Cold Gas Dynamic Spraying of High Strength Copper
Semi-Axisymmetric Scramjet Flowpath with Conformal Nozzle
Rocket Chamber Heat Exchanger
Rocket Engine Nozzle and Method of Fabricating a Rocket Engine Nozzle Using Pressure Brazing
Booster Rocket Engine Using Gaseous Hydrocarbon in Catalytically Enhanced Gas Generator Cycle
Thermal Cycle Engine with Augmented Thermal Energy Input Area
Thrust Augmentation in Plug Nozzles and Expansion-Deflection Nozzles
Method for Making a Multilayer Composite Pressure Vessel
Hall Effect Thruster with Anode Having Magnetic Field Barrier
Injector Assembly Having Multiple Manifolds for Propellant Delivery
Method and Apparatus for Solar Power Conversion
Nozzle Assembly for Rocket and Ramjet Applications
Rocket Engine Combustion Chamber
Piezo-Resonance Igniter and Ignition Method for Propellant Liquid Rocket Engine
Method and Apparatus for Solar Power Conversion
Piston Tank with Compound Piston for High Loading and Expulsion Efficiency
Coaxial Ignition Assembly
Helicon Hall Thruster
Patent:
7,436,122 →
Application:
11/437,279 →
Heat Exchange Injector for Use in a Rocket Engine
Dual-Function Stirling Engine System
Three Component Injector for Kerosene-Oxygen Rocket Engine
Nozzle with Temperature-Responsive Throat Diameter
Core Burning for Scramjet Engines
Method and Apparatus for a Rocket Engine Power Cycle
Combined Cycle Integrated Combustor and Nozzle System
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
Co-Sintered Multi-System Tungsten Alloy Composite
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
Two-Piece Aft Closure for a Rocket Motor Case
Combined Cycle Missile Engine System
Brazed Nano-Grained Aluminum Structures
Multi-Functional Pulse-Divided Rocket
Pintle-Controlled Propulsion System with External Ring Actuator
Single Phase Tungsten Alloy for Shaped Charge Liner
Rocket Nozzles for Unconventional Vehicles
Extended Range Projectile
Patent:
7,823,510 →
Application:
12/120,345 →
Guided Projectile
Igniter/Thruster with Catalytic Decomposition Chamber
Recast Removal Method
Slow Cook Off Rocket Igniter
Sequence Diagram System
Fastener Assembly for Connecting Rocket Engine Nozzles
Low Velocity Injector Manifold for Hypergolic Rocket Engine
Conductive Emissions Protection
Nano-Grained Aluminum Alloy Bellows
Method of Fabricating a Rocket Engine Nozzle Using Pressure Brazing
Solid state heat pipe heat rejection system for space power systems
Multilayer Composite Pressure Vessel and Method for Making the Same
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
High Voltage Multiple Phase Power Supply
Injector Assembly Having Multiple Manifolds for Propellant Delivery
Propulsion System With Movable Thermal Choke
Nuclear Fuel
Integrated Air Inlet System for Multi-Propulsion Aircraft Engines
Patent:
43,731 →
Application:
12/871,125 →
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
Co-Sintered Multi-System Tungsten Alloy Composite
Application:
12/952,426 →
Publication:
US 2011/0064600
Center-Tapped Solar Array and Power Distribution System for Same
Combined Cycle Integrated Combustor and Nozzle System
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
Catalyst, Gas Generator, and Thruster with Improved Thermal Capability and Corrosion Resistance
Application:
13/151,155 →
Publication:
US 2012/0304620
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
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
(19)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Jul 8, 2013
From: UNITED TECHNOLOGIES CORPORATION
To: RPW ACQUISITION LLC
Reel/Frame 030750/0283 →
Merger/Change of Name
Jul 8, 2013
From: RPW ACQUISITION LLC
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 030754/0248 →
Change of Name
Jul 30, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 030902/0313 →
Merger
Dec 5, 2013
From: AEROJET-GENERAL CORPORATION
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 031726/0655 →
Change of Name
May 8, 2014
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 032845/0909 →
Change of Name
Feb 25, 2016
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 037918/0042 →
Merger and Change of Name
May 14, 2016
From: AEROJET-GENERAL CORPORATION; AEROJET ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 038596/0682 →
Merger and Change of Name
May 15, 2016
From: AEROJET-GENERAL CORPORATION; AEROJET-GENERAL CORPORATION
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 038596/0912 →
Assignment of Assignor's Interest
May 17, 2016
From: GUIMONT, JOHN
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 038621/0131 →
Assignment of Assignor's Interest
May 18, 2016
From: FIGGE, IRVING EDWARD, SR; GRAHAM, PHILLIP HENRY
To: ATLANTIC RESEARCH CORPORATION
Reel/Frame 038634/0126 →
Assignment of Assignor's Interest
May 18, 2016
From: GUIMONT, JOHN
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 038638/0517 →
Assignment of Assignor's Interest
Jun 17, 2016
From: HUGHES ELECTRONICS CORPORATION
To: THE BOEING COMPANY
Reel/Frame 038945/0604 →
Release of Security Interest
Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE, INC. (F/K/A AEROJET-GENERAL CORPORATION)
Reel/Frame 039594/0887 →
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 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 064424/0050 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
Reel/Frame 064424/0271 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
Reel/Frame 064424/0238 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
Reel/Frame 064424/0180 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
Reel/Frame 064424/0087 →