IP Library Assignment 063710/0928
Patent Assignment
Reel/Frame 063710/0928

Assignment of Assignor's Interest

Recorded: 2023-05-21 Pages: 23
Assignor
LUZINSKI, JOSEPH J
Executed: 2023-05-08
Assignee
BOEING ACE COLLATERAL AGENT, LLC
929 LONG BRIDGE DRIVE, ARLINGTON, VIRGINIA, 22202
Covered Properties (55)
Laminar Flow Wing for Transonic Cruise
Patent: 7,000,870 →
Application: 10/693,411 →
Publication: US 2004/0129837
Highly Swept Canard with Low Sweep Wing Supersonic Aircraft Configuration
Patent: 6,857,599 →
Application: 10/746,744 →
Publication: US 2004/0140395
Lift and Twist Control Using Trailing Edge Control Surfaces on Supersonic Laminar Flow Wings
Patent: 7,004,428 →
Application: 10/762,083 →
Publication: US 2005/0151029
Supersonic Aircraft Jet Engine
Patent: 7,837,142 →
Application: 11/973,813 →
Publication: US 2009/0014597
Highly Efficient Supersonic Laminar Flow Wing
Patent: 7,946,535 →
Application: 11/974,802 →
Publication: US 2009/0206206
Jet nozzle plug with varying, non-circular cross sections
Patent: 8,371,124 →
Application: 12/384,248 →
Publication: US 2010/0139284
Laminar Flow Wing Optimized for Supersonic Cruise Aircraft
Patent: 8,272,594 →
Application: 12/589,424 →
Publication: US 2011/0095137
Aircraft emergency and backup secondary power apparatus
Patent: 8,882,028 →
Application: 12/806,223 →
Publication: US 2011/0067393
Supersonic Aircraft Jet Engine Installation
Patent: 7,967,241 →
Application: 12/807,142 →
Publication: US 2011/0062290
Supersonic aircraft jet engine installation
Application: 12/807,154 →
Publication: US 2022/0073203
Laminar Flow Wing Optimized for Transonic Cruise Aircraft
Patent: 8,448,893 →
Application: 12/931,060 →
Publication: US 2012/0043429
Laminar Flow Wing Optimized for Transonic Cruise Aircraft
Patent: 8,317,128 →
Application: 12/932,091 →
Publication: US 2012/0043430
Generating Inviscid and Viscous Fluid-Flow Simulations Over an Aircraft Surface Using a Fluid-Flow Mesh
Patent: 8,457,939 →
Application: 12/982,744 →
Publication: US 2012/0173219
Generating a Simulated Fluid Flow Over an Aircraft Surface Using Anisotropic Diffusion
Patent: 8,437,990 →
Application: 13/046,469 →
Publication: US 2012/0232860
Highly efficient supersonic laminar flow wing structure
Patent: 9,233,755 →
Application: 13/068,773 →
Highly Efficient Transonic Laminar Flow Wing
Patent: 8,991,768 →
Application: 13/068,774 →
Predicting Transition from Laminar to Turbulent Flow Over a Surface
Patent: 8,538,738 →
Application: 13/069,374 →
Publication: US 2012/0245910
Generating Inviscid and Viscous Fluid Flow Simulations Over a Surface Using a Quasi-Simultaneous Technique
Patent: 8,892,408 →
Application: 13/070,384 →
Publication: US 2012/0245903
Predicting Transition from Laminar to Turbulent Flow Over a Surface Using Mode-Shape Parameters
Patent: 9,494,482 →
Application: 13/850,628 →
Publication: US 2013/0282629
Generating Inviscid and Viscous Fluid-Flow Simulations Over a Surface Using a Fluid-Flow Mesh
Patent: 8,935,140 →
Application: 13/887,189 →
Publication: US 2013/0246027
Generating a Simulated Fluid Flow Over a Surface Using Anisotropic Diffusion
Patent: 9,348,956 →
Application: 13/887,199 →
Publication: US 2013/0246024
Predicting Transition from Laminar to Turbulent Flow Over a Surface
Patent: 9,418,202 →
Application: 14/019,448 →
Publication: US 2014/0019105
Generating Inviscid and Viscous Fluid-Flow Simulations Over an Aircraft Surface Using a Fluid-Flow Mesh
Application: 14/583,070 →
Publication: US 2015/0370933
Predicting Transition from Laminar to Turbulent Flow Over a Surface Using Mode-Shape Parameters
Application: 15/335,303 →
Publication: US 2017/0045417
High Flow Plug Nozzle Apparatus and Method of Using the Same
Application: 15/626,012 →
Methods and Apparatus to Reduce Noise and Vibration in a Hybrid Hydraulic Power Steering System
Application: 15/946,573 →
Publication: US 2019/0308661
Computing Techniques for Three-Dimensional Modeling and Design Analysis
Application: 16/023,162 →
Publication: US 2019/0005185
Real-Time Automated Method and System Enabling Continuous Supersonic Flight While Preventing Ground Level Sonic Boom
Application: 16/750,844 →
Publication: US 2021/0233413
Aircraft Fuselage with Internal Current Return Network
Application: 16/830,866 →
Publication: US 2021/0300588
Aircraft Software Management System
Application: 16/839,171 →
Publication: US 2021/0311713
Composite Aircraft Structures with Dividers for Shielding and Protecting Cables and Wires
Application: 16/844,369 →
Aircraft Body Section with Multilayer Electrically Conductive Structure and Methods of Fabrication
Application: 16/925,425 →
Publication: US 2022/0009613
System and Method to Actively Morph an Aircraft While in Flight for Sonic Boom Suppression and Drag Minimization
Application: 17/563,125 →
Publication: US 2022/0289360
Computing Techniques for Three-Dimensional Modeling and Design Analysis
Application: 17/668,222 →
Publication: US 2022/0300673
Airplane
Patent: 950,465 →
Application: 29/729,608 →
Airplane
Patent: 950,466 →
Application: 29/729,610 →
Airplane
Patent: 950,467 →
Application: 29/729,612 →
Airplane
Patent: 950,468 →
Application: 29/729,616 →
Airplane
Patent: 950,469 →
Application: 29/729,617 →
Airplane
Patent: 950,470 →
Application: 29/729,619 →
Supersonic laminar wing for transonic cruise
Application: 60/424,039 →
Highly swept canard with low sweep wing supersonic aircraft configuration
Application: 60/436,852 →
Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings
Application: 60/441,934 →
Gradient pressure recovery inlet for supersonic aircraft
Application: 60/851,403 →
Surface expansion nozzle integration for supersonic aircraft
Application: 60/851,630 →
Aircraft engine translating inlet assembly
Application: 60/851,841 →
Highly efficient supersonic laminar flow wing
Application: 60/852,929 →
Jet nozzle plug with varying, non-circular cross sections
Application: 61/124,118 →
Aircraft emergency and backup secondary power apparatus
Application: 61/277,030 →
Predicting Transition from Laminar to Turbulent Flow Over a Surface Using Mode-Shape Parameters
Application: 61/635,779 →
Solid Modeler That Provides Spatial Gradients of 3D Cad Models of Solid Objects
Application: 62/482,023 →
Solid Modeler That Provides Spatial Gradients of 3D Cad Models of Solid Objects
Application: 62/482,029 →
Computing Techniques for Three-Dimensional Modeling and Design Analysis
Application: 62/527,627 →
Computing Techniques for Three-Dimensional Modeling and Design Analysis
Application: 62/595,001 →
System to Actively Morph an Aircraft in Real Time While in Supersonic Flight to and from Two Optimzed States 1) Optimized State for Sonic Boom Ground Overpressure Minimization and 2) Optimized State for Drag Minimization for Maximum Range Performance
Application: 63/109,627 →
Related Assignments (23)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest Dec 23, 2003
From: TRACY, RICHARD R.; CHASE, JAMES D.; KROO, ILAN
To: AERION CORPORATION
Reel/Frame 014857/0962 →
Assignment of Assignor's Interest Jan 20, 2004
From: TRACY, RICHARD R.; CHASE, JAMES D.
To: AERION CORPORATION
Reel/Frame 014919/0116 →
Assignment of Assignor's Interest Mar 29, 2005
From: TRACY, RICHARD R.; CHASE, JAMES D.; KROO, ILAN
To: AERION CORPORATION
Reel/Frame 016400/0190 →
Assignment of Assignor's Interest Oct 9, 2007
From: CHASE, JAMES D.; GARZON, GERMAN ANDRES
To: AERION CORPORATION
Reel/Frame 020013/0094 →
Assignment of Assignor's Interest Oct 16, 2007
From: CHASE, JAMES D.; HENDERSON, MICHAEL; STURDZA, PETER
To: AERION COPORATION
Reel/Frame 020032/0506 →
Assignment of Assignor's Interest Apr 3, 2009
From: CHASE, JAMES D.; GARZON, GERMAN ANDRES
To: AERION CORPORATION
Reel/Frame 022536/0640 →
Assignment of Assignor's Interest Oct 26, 2009
From: TRACY, RICHARD R.; STURDZA, PETER; CHASE, JAMES D.
To: AERION CORPORATION
Reel/Frame 023460/0433 →
Assignment of Assignor's Interest Aug 9, 2010
From: CHASE, JAMES D.
To: AERION CORPORATION
Reel/Frame 024844/0264 →
Assignment of Assignor's Interest Jan 25, 2011
From: TRACY, RICHARD R.; CHASE, JAMES D.
To: AERION CORPORATION
Reel/Frame 025728/0900 →
Assignment of Assignor's Interest Feb 16, 2011
From: TRACY, RICHARD R.; CHASE, JAMES D.
To: AERION CORPORATION
Reel/Frame 025883/0875 →
Assignment of Assignor's Interest Mar 11, 2011
From: RODRIGUEZ, DAVID L.; STURDZA, PETER
To: DESKTOP AERONAUTICS, INC.
Reel/Frame 025963/0138 →
Assignment This Is a Corrective Assignment Based on Reel/Frame 025883/0875.We Are Correcting the Title in Assignment. May 12, 2011
From: TRACY, RICHARD R.; CHASE, JAMES D.
To: AERION CORPORATION
Reel/Frame 026640/0430 →
Assignment of Assignor's Interest May 18, 2011
From: CHASE, JAMES D.; STURDZA, PETER; HENDERSON, MICHAEL
To: AERION CORPORATION
Reel/Frame 026448/0549 →
Assignment of Assignor's Interest May 18, 2011
From: CHASE, JAMES D.; STURDZA, PETER; HENDERSON, MICHAEL
To: AERION CORPORATION
Reel/Frame 026429/0293 →
Assignment of Assignor's Interest May 18, 2011
From: RAJNARAYAN, DEV; STURDZA, PETER
To: DESKTOP AERONAUTICS, INC.
Reel/Frame 026298/0877 →
Assignment of Assignor's Interest Jun 10, 2011
From: STURDZA, PETER; MARTINS-RIVAS, HERVE; SUZUKI, YOSHIFUMI
To: DESKTOP AERONAUTICS, INC.
Reel/Frame 026428/0597 →
Assignment of Assignor's Interest Jun 13, 2011
From: RODRIGUEZ, DAVID L.; STURDZA, PETER
To: DESKTOP AERONAUTICS, INC.
Reel/Frame 026435/0560 →
Corrective Assignment to Correct the Property Number Listing U.S. Application Serial Number 13/046,649 to 13/046,469, and Corresponding Title of Invention Previously Recorded on Reel 025963 Frame 0138. Assignor(S) Hereby Confirms the Assignment. Apr 5, 2013
From: RODRIGUEZ, DAVID L.; STURDZA, PETER
To: DESKTOP AERONAUTICS, INC.
Reel/Frame 030165/0043 →
Assignment of Assignor's Interest Apr 9, 2013
From: DESKTOP AERONAUTICS, INC.
To: AERION CORPORATION
Reel/Frame 030180/0896 →
Assignment of Assignor's Interest Jan 15, 2019
From: AERION CORPORATION
To: AERION INTELLECTUAL PROPERTY MANAGEMENT CORPORATION
Reel/Frame 048077/0026 →
License Feb 27, 2020
From: AERION CORPORATION-DESKTOP AERONAUTICS, INC.
To: UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF NASA
Reel/Frame 052045/0510 →
Security Interest Mar 25, 2021
From: AERION CORPORATION; AERION INTELLECTUAL PROPERTY MANAGEMENT CORPORATION
To: BOEING ACE COLLATERAL AGENT LLC, AS COLLATERAL AGENT
Reel/Frame 055724/0653 →
Security Interest Jul 12, 2021
From: AERION CORPORATION; AERION INTELLECTUAL PROPERTY MANAGEMENT CORPORATION
To: BOEING ACE COLLATERAL AGENT LLC, AS COLLATERAL AGENT
Reel/Frame 056819/0235 →