Class B64C : AEROPLANES; HELICOPTERS
Subclass 1/38: Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (aerodynamical features common to fuselages, wings, stabilising surfaces, or the like B64C 23/00; flight-deck installations B64D) Constructions adapted to reduce effects of aerodynamic or other external heating
| Patent # | Title | Filing Date | Issue Date | Patent Owner |
|---|---|---|---|---|
| 12187408 | Door assembly | Apr 20, 21 | Jan 07, 25 | Bae Systems PLC |
| 12129030 | Fire resistant aerial vehicle for suppressing widespread fires | Dec 14, 18 | Oct 29, 24 | INCAENDIUM INITIATIVE CORPORATION |
| 12115881 | Non-integral battery cold plate | Feb 10, 21 | Oct 15, 24 | Textron Innovations Inc. |
| 12110096 | Active cooling of windward surface of craft | Feb 11, 22 | Oct 08, 24 | THE BOEING COMPANY |
| 12103702 | Removeable fuselage shield for an aircraft | Oct 15, 20 | Oct 01, 24 | General Electric Company |
| 12009590 | Cover for a vehicle, in particular for a supersonic or hypersonic vehicle | Jul 10, 20 | Jun 11, 24 | MBDA FRANCE |
| 11975814 | System and method to actively morph an aircraft while in flight for sonic boom suppression and drag minimization | Dec 28, 21 | May 07, 24 | Boeing Ace Collateral Agent, LLC |
| 11939040 | Systems and methods for operating a door of an aircraft | Mar 10, 22 | Mar 26, 24 | The Boeing Company |
| 11912393 | Aircraft drag reduction system including an internally cooled motor system and aircraft using same | Jan 28, 22 | Feb 27, 24 | Joby Aero, Inc. |
| 11873073 | Fuel cooled multi-function aperture | Feb 26, 21 | Jan 16, 24 | HAMILTON SUNDSTRAND CORPORATION |
| 11858613 | Aerospace vehicles with coatings for heat radiation and associated methods | Nov 23, 20 | Jan 02, 24 | General Electric Company |
| 11835072 | Ultrasonic airflow severing resistance reducing device for vehicles | Feb 09, 22 | Dec 05, 23 | Not available |
| 11834196 | System and method for control for unducted engine | Oct 15, 20 | Dec 05, 23 | General Electric Company |
| 11820490 | Methods, apparatus, and articles of manufacture for actuating control surfaces of an aircraft | May 23, 22 | Nov 21, 23 | THE BOEING COMPANY |
| 11814174 | Layered fuselage shield | Oct 15, 20 | Nov 14, 23 | General Electric Company |
| 11753178 | Systems and methods for removing heat from aircraft components | Nov 12, 19 | Sep 12, 23 | General Electric Company |
| 11745847 | System and method for cooling a leading edge of a high speed vehicle | Dec 08, 20 | Sep 05, 23 | General Electric Company |
| 11542867 | Supersonic air intake passage capable of achieving synchronous adjustment of capturing area and throat area | Aug 14, 18 | Jan 03, 23 | Nanjing University of Aeronautics and Astronautics |
| 11535355 | Aerodynamic body for supersonic speed | Feb 28, 20 | Dec 27, 22 | The Boeing Company |
| 11506067 | Gas turbine engine with clutch assembly | Jun 17, 20 | Nov 22, 22 | General Electric Company |
| Publication # | Title | Filing Date | Pub Date | Patent Owner |
|---|---|---|---|---|
| 2025/0108,915 | METHOD AND SYSTEM FOR REDUCING A TEMPERATURE DIFFERENTIAL ACROSS A FLIGHT VEHICLE | Sep 29, 23 | Apr 03, 25 | THE BOEING COMPANY |
| 2025/0100,671 | VEHICLE HAVING A BODY WITH A NOSE SECTION | Sep 22, 23 | Mar 27, 25 | Not available |
| 2025/0001,903 | Non-Integral Battery Cold Plate | Sep 12, 24 | Jan 02, 25 | Not available |
| 2024/0417,101 | GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY | Aug 28, 24 | Dec 19, 24 | Not available |
| 2024/0401,490 | PROPULSION SYSTEM AND METHOD FOR OPERATION | Aug 09, 24 | Dec 05, 24 | Not available |
| 2024/0262,517 | Aircraft Electric Motor Cooling System | Feb 24, 24 | Aug 08, 24 | Not available |
| 2024/0002,033 | TRANSPIRATIONAL COOLING PANEL | Jun 29, 22 | Jan 04, 24 | Not available |
| 2023/0373,611 | METHODS, APPARATUS, AND ARTICLES OF MANUFACTURE FOR ACTUATING CONTROL SURFACES OF AN AIRCRAFT | May 23, 22 | Nov 23, 23 | Not available |
| 2023/0278,695 | SYSTEMS FOR COOLING A LEADING EDGE OF A HIGH SPEED VEHICLE | Mar 07, 22 | Sep 07, 23 | Not available |
| 2023/0059,838 | HEAT INPUT REDUCING STRUCTURE FOR AIRCRAFT, HEAT INPUT REDUCING SYSTEM, AIRCRAFT, AND AIRCRAFT MANUFACTURING METHOD | Jan 22, 21 | Feb 23, 23 | MITSUBISHI AIRCRAFT CORPORATION |
| 2022/0185,446 | SYSTEM AND METHOD FOR COOLING A LEADING EDGE OF A HIGH SPEED VEHICLE | Dec 14, 20 | Jun 16, 22 | Not available |
| 2022/0169,362 | Aircraft Drag Reduction System And Aircraft Using Same | Jan 28, 22 | Jun 02, 22 | Not available |
| 2021/0094,671 | REINFORCED SUPERPLASTIC FORMED AND DIFFUSION BONDED STRUCTURES | Sep 30, 19 | Apr 01, 21 | The Boeing Company |
| 2020/0140,058 | ELECTRONIC SPEED CONTROLLER ASSEMBLY, POWER SYSTEM, AND UNMANNED AERIAL VEHICLE | Dec 24, 19 | May 07, 20 | Not available |
| 2019/0329,858 | Aircraft Drag Reduction System And Internally Cooled Electric Motor System And Aircraft Using Same | Mar 16, 19 | Oct 31, 19 | Not available |
| 2019/0300,144 | HEAT SHIELD ASSEMBLY AND MOUNTING THEREOF ON AIRCRAFT | Mar 29, 18 | Oct 03, 19 | Not available |
| 2019/0054,998 | FAIRING ASSEMBLY AND METHOD THEREFOR | Aug 15, 17 | Feb 21, 19 | Not available |
| 2016/0114,879 | Superconductive Hypersonic Liquefaction Nosecone | Nov 24, 15 | Apr 28, 16 | Not available |
| 2014/0106,164 | RADIATIVE SURFACE | Oct 11, 13 | Apr 17, 14 | THALES, UNIVERSITE DE CERGY-PONTOISE, |
| 2012/0312,923 | MITIGATING TRANSONIC SHOCK WAVE WITH PLASMA HEATING ELEMENTS | Jun 08, 11 | Dec 13, 12 | LOCKHEED MARTIN CORPORATION |
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