Patent Assignment
Reel/Frame 039197/0125
Notice of Grant of Security Interest in Patents
Recorded: 2016-06-17
Pages: 16
Assignor
AEROJET ROCKETDYNE, INC., SUCCESSOR-IN-INTEREST TO RPW ACQUISITION LLC
Executed: 2016-06-17
Assignee
BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
901 MAIN STREET, TX1-492-14-06, DALLAS, TEXAS, 75202
Covered Properties
(158)
Electric Propulsion Power Circuit
PCT:
PCT/US2014/040474 ↗
Actuator Controller
PCT:
PCT/US2014/067398 ↗
Hydroxylammonium Nitrate Monopropellant with Burn Rate Modifier
PCT:
PCT/US2015/014951 ↗
Lightweight Munition
PCT:
PCT/US2015/021368 ↗
Fragmenting Nozzle System
PCT:
PCT/US2015/028423 ↗
Turbopump with Axially Curved Vane
PCT:
PCT/US2015/038230 ↗
Dual Stage Catalytic Thruster
PCT:
PCT/US2015/038505 ↗
Power Architecture for Solar Electric Propulsion Applications
PCT:
PCT/US2015/040548 ↗
Liquid Propellant Rocket Engine with Afterburner Combustor
PCT:
PCT/US2015/047073 ↗
Additive Manufacturing Using Pressurized Slurry Feed
PCT:
PCT/US2015/049327 ↗
Rocket Motor with Energetic Grain Having Micro-Voids
PCT:
PCT/US2015/049346 ↗
Propulsion System with Differential Throttling of Electric Thrusters
PCT:
PCT/US2015/056174 ↗
Turbopump Machine with Isolated Cooling Passage Discharge
PCT:
PCT/US2015/059173 ↗
Valve Assembly with Electronic Control
PCT:
PCT/US2015/061037 ↗
Valve Assembly with Adjustable Spring Seat
PCT:
PCT/US2016/014807 ↗
Rocket Thruster Nozzle with Connectors and Brace
PCT:
PCT/US2016/021957 ↗
Hall Thruster with Exclusive Outer Magnetic Core
PCT:
PCT/US2016/021973 ↗
Ignition System
PCT:
PCT/US2016/021985 ↗
Magnetic Latch Valve
PCT:
PCT/US2016/027010 ↗
Magnetic Latch Throttle Valve
PCT:
PCT/US2016/027011 ↗
Nickel Base Superalloy Columnar Grain and Equiaxed Materials with Improved Performance in Hydrogen and Air
Patent:
5,820,700 →
Application:
08/539,091 →
Ramjet/Scramjet Inlet Isolator Unstart Prevention
Patent:
5,806,301 →
Application:
08/570,391 →
Selectively Enabled Watchdog Timer Circuit
Patent:
5,864,663 →
Application:
08/712,915 →
Method for Making a Hydrogen Embrittlement Resistent Y'strengthened Nickel Base Superalloy Material
Patent:
5,976,280 →
Application:
08/759,495 →
Laser Ignition for Liquid Propellant Rocket Engine Injectors
Patent:
9,347,399 →
Application:
08/988,059 →
Fluid-Cooled Turbine Blades
Patent:
6,565,312 →
Application:
10/029,451 →
Controlled Autoignition Propellant Systems
Patent:
9,759,162 →
Application:
10/200,597 →
Fluid Injector and Injection Method
Low-Emission, Staged-Combustion Power Generation
Monitoring System for Turbomachinery
Compact Swirl Augmented Afterburners for Gas Turbine Engines
Combined Cycle Engines Incorporating Swirl Augmented Combustion for Reduced Volume and Weight and Improved Performance
Rocket Motors Having Controlled Autoignition Propellant Systems
Patent:
9,784,545 →
Application:
10/376,297 →
Apparatus and Method for Selecting a Flow Mixture
Cold Spray Nozzle Design
Application of a Mixed Metal Oxide Catalyst to a Metallic Substrate
Methods and Apparatuses for Removing Thermal Energy from a Nuclear Reactor
Patent:
6,768,781 →
Application:
10/405,000 →
Lightning Strike Mitigation System
Method and Apparatus for Mixing Substances
Method and Apparatus for Injecting a Fuel into a Combustor Assembly
Composite Material
Inter-Fluid Seal Assembly and Method Therefor
Gas-Buffered Seal Assembly and Method Therefor
Cascade Ignition of Catalytic Combustors
Fuel Injection Method and Apparatus for a Combustor
Real Time Gear Box Health Management System and Method of Using the Same
Non-Swirl Dry Low Nox (Dln) Combustor
Fluid Injector and Injection Method
Carbo-Nitrided Case Hardened Martensitic Stainless Steels
Cryogenic Bearings
Compact Lightweight Ramjet Engines Incorporating Swirl Augmented Combustion with Improved Performance
Compact Swirl Augmented Afterburners for Gas Turbine Engines
Acoustic Dampers
High Temperature Aluminum Alloys
Aluminum Based Alloy
Method and Apparatus for Mixing Substances
Combustion Wave Ignition for Combustors
Cooling Exchanger Duct
Fuel Injection Method and Apparatus for a Combustor
Electrical Interconnection Having Magnetic Conductive Elements
Single-Stage Hypersonic Vehicle Featuring Advanced Swirl Combustion
Detection of Peroxides and Superoxides with Fast Neutrons
Cold Sprayed Metal Matrix Composites
Cooling Exchanger Ducts
Nano-Particle Wave Heat Pipe
Variable-Ratio Neutron-Gamma Ray Source
Valve System for a Gas Turbine Engine
Valve System for a Gas Turbine Engine
Valve System for a Gas Turbine Engine
Heat Exchanger for a Rocket Engine
High Strength L12 Aluminum Alloys
High Strength L12 Aluminum Alloys
Heat Treatable L12 Aluminum Alloys
High Strength Aluminum Alloys with L12 Precipitates
Dispersion Strengthened L12 Aluminum Alloys
L12 Strengthened Amorphous Aluminum Alloys
High Strength L12 Aluminum Alloys
Method and Composition for Moderated Nuclear Fuel
Apparatus for Mixing Substances
Internally Damped Blade
Non-Integral Platform and Damper for an Airfoil
Cooling Exchanger Duct
Infrared Led Source for Thermal Imaging
Application:
12/844,026 →
Publication:
US 2012/0025079
Valve System for a Gas Turbine Engine
High Strength L12 Aluminum Alloys
Heat Treatable L12 Aluminum Alloys
Heat Exchanger Fin Including Louvers
Method and System for Operating a Flow Battery System Based on Energy Costs
Flow Battery Having a Low Resistance Membrane
Application:
13/023,101 →
Publication:
US 2012/0202099
Structurally Efficient Cooled Engine Housing for Rotary Engines
Flow Battery Having Electrodes with a Plurality of Different Pore Sizes and or Different Layers
System and Method for Operating a Flow Battery System at an Elevated Temperature
System and Method for Sensing and Mitigating Hydrogen Evolution Within a Flow Battery System
Distributed Exhaust System
Integral Oil System
Damper for an Integrally Bladed Rotor
Liquid Fuel with Endothermic Fuel-Cracking Catalyst
Flow Battery Cells Arranged Between an Inlet Manifold and an Outlet Manifold
Application:
13/194,486 →
Publication:
US 2013/0029196
Ejector-Driven Fuel Stabilization System
Method for Processing Biomass
Flow Battery Stack with an Integrated Heat Exchanger
Cyclic Energetic Nitramines Desensitized with Linear Nitramines
Turbine Blade Rail Damper
Catalytically Enhanced Gas Generator System for Rocket Applications
Flow Battery System with Standby Mode
Energy Absorbent Ultrasonic Inspection System with Laser Pointer
Selectable Ramjet Propulsion System
Patent:
9,726,115 →
Application:
13/355,949 →
Laser Configuration for Additive Manufacturing
Application:
13/362,322 →
Publication:
US 2013/0112672
Additive Manufacturing Management of Large Part Build Mass
Application:
13/362,396 →
Publication:
US 2013/0101746
Additive Manufacturing in Situ Stress Relief
Application:
13/362,425 →
Publication:
US 2013/0101728
Energetic Adhesive for Venting Cookoff
Application:
13/415,155 →
Publication:
US 2012/0232189
Rocket Nozzles for Unconventional Vehicles
Extruded Matching Set Radiators
Application:
13/476,450 →
Publication:
US 2013/0306293
Laser Sintered Matching Set Radiators
Application:
13/476,455 →
Publication:
US 2013/0308273
Conductive Emissions Protection
Inducer with Cavitation Instability Controls to Reduce Vibrations and Radial Loads
End-Burning Propellant Grain with Area-Enhanced Burning Surface
System and Method for Sensing and Mitigating Hydrogen Evolution Within a Flow Battery System
Method for Producing a Fragment / Reactive Material Assembly
Combined Cycle Integrated Combustor and Nozzle System
Thermal Stand-Off with Tortuous Solid-Wall Thermal Conduction Path
Pressure-Relief Vent
Composition for Reactive Material
Application:
14/284,465 →
Publication:
US 2015/0337414
Continuous Detonation Wave Turbine Engine
Application:
14/285,068 →
Publication:
US 2015/0308348
Conductive Emissions Protection
Application:
14/458,864 →
Method and System for Operating a Flow Battery System Based on Energy Costs
Propellant with Extended Storage Life
Combined Cycle Propulsion System
Application:
14/790,445 →
Publication:
US 2016/0010485
End-Burning Propellant Grain with Area-Enhanced Burning Surface
Flow Battery Having Electrodes with a Plurality of Different Pore Sizes and or Different Layers
Damper for an Integrally Bladed Rotor
Stored Pressure Driven Cycle
Selectively Submersible Vessel
Ground Based Systems and Methods for Testing Reaction Thrusters
Gas Generator and Process Therefor
Solid Rocket Motor with Integrated Tooling for Vertical Inversion
Application:
62/185,442 →
Preformed Fragment Winding and Encapsulation Process
Application:
62/185,699 →
Nozzle Throat Area Control
Application:
62/191,996 →
Constant Fueldraulic Fuel Flow with Variable Downstream Actuation Load Flow
Application:
62/192,037 →
Fragmenting Nozzle System
Application:
62/202,499 →
Solid Rocket Motor Propellant Grain
Application:
62/202,703 →
Solid Rocket Motor Propellant Barrier
Application:
62/203,492 →
Concentric Energetics for Shock and Impact Mitigation
Application:
62/204,827 →
Composite Polar Boss
Application:
62/206,735 →
Surface Marking for Direct Strain Imaging
Application:
62/209,148 →
Rocket Motor with Energetic Grain Having Micro-Voids with Powder Energetic Disposed Therein
Application:
62/211,601 →
Smart Weather Seal for Solid Rocket Propellant
Application:
62/212,476 →
Short Circuit Protection for Switching Converters
Application:
62/213,726 →
Solar Array Deployment
Application:
62/239,167 →
Articulated Flow Liner for Scissor Ducts Bellows
Application:
62/239,376 →
High Performance Shock Resistant Solid Propellant
Application:
62/239,621 →
LOW GLASS TRANSITION (Tg) PROPELLANT
Application:
62/243,614 →
Transparent/Translucent Rocket Motor Weather Seal
Application:
62/248,458 →
Electronic Weather Seal
Application:
62/248,464 →
Solid Rocket Propellant Barrier
Application:
62/250,307 →
Fragmenting Nozzle System
Application:
62/252,269 →
Metallic Compound Additive for Ammonium Perchlorate Decomposition
Application:
62/257,071 →
Dimer Diol for HTPB Binders
Application:
62/257,093 →
Related Assignments
(14)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Jul 10, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 030774/0529 →
Assignment of Assignor's Interest
Dec 16, 2014
From: SWANSON, JON D.; DAREJEH, HADI
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 034519/0165 →
Change of Name
Mar 17, 2015
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 035220/0461 →
Change of Name
Feb 25, 2016
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 037918/0126 →
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 →
License
Aug 5, 2016
From: UNITED TECHNOLOGIES CORPORATION
To: AEROJET ROCKETDYNE, INC. (F/K/A AEROJET-GENERAL CORPORATION, SUCCESSOR OF RPW ACQUISITION LLC)
Reel/Frame 039595/0315 →
Merger and Change of Name
Oct 18, 2017
From: AEROJET-GENERAL CORPORATION; AEROJET ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 043891/0466 →
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 →
Change of Name
Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
Corrective Assignment to Correct the and Remove Patent Application Number 11886281 and Add Patent Application Number 14846874. to Correct the Receiving Party Address Previously Recorded at Reel: 054062 Frame: 0001. Assignor(S) Hereby Confirms the Change of Address.
Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
Change of Name
Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
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 →
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 →