Patent Assignment
Reel/Frame 030750/0283
Assignment of Assignor's Interest
Recorded: 2013-07-08
Pages: 13
Assignor
UNITED TECHNOLOGIES CORPORATION
Executed: 2013-06-14
Assignee
RPW ACQUISITION LLC
1209 ORANGE STREET, WILMINGTON, DELAWARE, 19801
Covered Properties
(79)
Coolable Rocket Nozzle for a Rocket Engine
Patent:
5,582,000 →
Application:
07/308,157 →
Method and Apparatus for Increasing Combustion Chamber Pressure in a High Pressure Expander Cycle Rocket Engine
Patent:
5,410,874 →
Application:
07/617,332 →
Rocket Nozzle for a Rocket Engine
Patent:
5,683,033 →
Application:
07/629,112 →
High Rate Electrophoresis Process for Ceramic Coated Fibers
Patent:
5,302,265 →
Application:
07/637,718 →
Ceramic Fibers Produced by Electrophoretic Deposition of Particles
Patent:
5,580,835 →
Application:
07/637,848 →
Ceramic Coated Fibers
Patent:
5,306,560 →
Application:
07/637,849 →
Electrophoresis Process for Preparation of Ceramic Fibers
Patent:
5,336,381 →
Application:
07/637,850 →
Rocket Engine Auxiliary Power System
Patent:
5,873,241 →
Application:
07/704,537 →
Cryogenic Fluid Manifold
Patent:
5,564,753 →
Application:
07/770,216 →
Method of Making a Tubular Thermal Structure
Patent:
5,467,528 →
Application:
07/812,318 →
Method of a Making a Diffusion Bonded Rocket Chamber
Patent:
5,386,628 →
Application:
07/812,319 →
Beneficial Use of Class 1.1 Rocket Propellant
Patent:
5,291,831 →
Application:
08/038,773 →
Hexagonal Cluster Nozzle for a Rocket Engine
Patent:
5,343,698 →
Application:
08/054,915 →
Method and Apparatus for Cutting Blocks of Solid Energetic Materials
Patent:
5,881,619 →
Application:
08/080,890 →
Stator Assembly for a Rotary Machine Having a Centrifugal on Impeller and Volute
Patent:
5,332,359 →
Application:
08/134,726 →
Electrophoresis Process for Preparation of Ceramic Fibers
Patent:
5,366,687 →
Application:
08/165,129 →
Pressure-Fed Rocket Booster System
Patent:
5,444,973 →
Application:
08/166,425 →
Process for the Electrophoretic Deposition of Defect-Free Metallic Oxide Coatings
Patent:
5,415,748 →
Application:
08/200,611 →
Method of Simultaneously Forming Rocket Thrust Chamber Cooling Tubes
Patent:
5,477,613 →
Application:
08/213,306 →
Method of Making Cooled Rocket Combustion Chamber Construction
Patent:
5,473,817 →
Application:
08/213,391 →
Rocket Preburner Injector with Tailored Gas Temperature Profile
Patent:
5,566,544 →
Application:
08/250,243 →
Tube Rocket Thrust Chamber Construction and Method
Patent:
5,557,928 →
Application:
08/291,385 →
Fabrication of Rocket Thrust Chambers
Patent:
5,546,656 →
Application:
08/346,646 →
Scramjet Fuel Injection System Having Independent Fuel Supplies for Supersonic and Hypersonic Operation
Patent:
5,660,040 →
Application:
08/359,808 →
Method for Making a Cobalt-Boride Dispersion-Strengthened Copper
Patent:
5,534,086 →
Application:
08/432,061 →
Preparation of Alumina-Silica Sol Gel Compositions
Patent:
5,591,380 →
Application:
08/437,486 →
Gamma Strengthened Single Crystal Turbine Blade Alloy for Hydrogen Fueled Propulsion Systems
Patent:
5,679,180 →
Application:
08/493,610 →
Process for Preparing Spherical Energetic Compounds
Patent:
5,801,453 →
Application:
08/661,437 →
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 →
Liquid Oxygen Gasifying System for Rocket Engines
Patent:
5,918,460 →
Application:
08/850,259 →
Method Manufacturing Solid Rocket Motors
Patent:
6,408,760 →
Application:
08/993,811 →
Apparatus for Preparing Spherical Energetic Compounds
Patent:
5,962,803 →
Application:
09/047,678 →
Ignition System for Rocket Engines
Patent:
6,082,098 →
Application:
09/069,133 →
Hydrostatic Bearing with Compensatory Fluid Injection
Patent:
6,053,636 →
Application:
09/189,335 →
Method of Repairing a Rocket Thrust Chamber
Patent:
6,131,280 →
Application:
09/201,476 →
Catalyst Bed
Gas Generator for Producing Adjustable Flow
Method for Preparing Refractory Carbides
Adaptable Solid-Hybrid Rocket for Crew Escape and Orbital Injection Propulsion
Heat Exchanger Panel
Rocket Propulsion System
Scram Jet Engine Design
Variable Geometry Inlet Design for Scram Jet Engine
Hypergolic Fuel System
Propulsion System with Integrated Rocket Accelerator
Rocket Engine Tubular Chamber with Single Piece Jacket
Rocket Engine Combustion Chamber
Multichannel Hall Effect Thruster
Advanced L-Channel Welded Nozzle Design
Enhanced Performance Torroidal Coolant-Collection Manifold
Reduced Gain Thrust Control Valve
Cooling Scheme for Scramjet Variable Geometry Hardware
High Temperature Dynamic Seal for Scramjet Variable Geometry
Staged Emitter-Attractor Ion Drive
Energetic Detonation Propulsion
Cryogenic Insulation
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
Booster Rocket Engine Using Gaseous Hydrocarbon in Catalytically Enhanced Gas Generator Cycle
Rocket Engine Combustion Chamber
Solar Tracker
Coaxial Ignition Assembly
Heat Exchange Injector for Use in a Rocket Engine
High temperature molten salt receiver
Dual-Function Stirling Engine System
Three Component Injector for Kerosene-Oxygen Rocket Engine
Supercritical CO2 Turbine for Use in Solar Power Plants
Rocket Engine Power Cycle
Recast Removal Method
Fastener Assembly for Connecting Rocket Engine Nozzles
Conductive Emissions Protection
Nano-Grained Aluminum Alloy Bellows
Agglomerator with Ceramic Matrix Composite Obstacles
Centrifugal Impeller
Application:
13/299,718 →
Publication:
US 2013/0129524
Injector Having Multiple Impingement Lengths
Application:
13/467,238 →
Publication:
US 2013/0074472
Related Assignments
(5)
Other recorded transfers of the patents in this record — the chain of ownership.
Merger/Change of Name
Jul 8, 2013
From: RPW ACQUISITION LLC
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 030754/0248 →
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, 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, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
Reel/Frame 064424/0087 →