Class B64C : AEROPLANES; HELICOPTERS
Subclass 1/00: 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)
| Patent # | Title | Filing Date | Issue Date | Patent Owner |
|---|---|---|---|---|
| 12263932 | Aircraft with lifting body fuselage profile | Apr 25, 22 | Apr 01, 25 | Not available |
| 12263948 | Primary structural assembly for an aircraft outside-skin heat exchanger, aircraft having a primary structural assembly, and method for attaching an aircraft outside-skin heat exchanger | Aug 05, 20 | Apr 01, 25 | Airbus Operations GmbH |
| 12257817 | Composite panel structure and method of manufacturing | Mar 30, 20 | Mar 25, 25 | Kawasaki Jukogyo Kabushiki Kaisha |
| 12246816 | Mobile units | May 02, 22 | Mar 11, 25 | Not available |
| 12246831 | Quiet aerial vehicle | Jan 11, 24 | Mar 11, 25 | THE BOEING COMPANY |
| 12240586 | Aircraft fuselage and module for absorbing crash energy in a lower deck, used for transporting passengers, of an aircraft | Mar 29, 23 | Mar 04, 25 | Airbus Operations GmbH |
| 12227281 | Method and apparatus for fabricating reformable stiffening elements | May 23, 23 | Feb 18, 25 | Spirit AeroSystems, Inc. |
| 12227291 | Distributed propulsion system for vertical take off and landing closed wing aircraft | Feb 14, 23 | Feb 18, 25 | Textron Innovations Inc. |
| 12220884 | Methods and devices for supporting of variety of different pre-cured composite stringers | Jun 07, 23 | Feb 11, 25 | The Boeing Company |
| 12220890 | Methods for fabricating solid laminate stringers on a composite panel | Feb 18, 20 | Feb 11, 25 | THE BOEING COMPANY |
| 12221219 | Pressure relief door assembly with temperature-actuated lock | Dec 22, 21 | Feb 11, 25 | Rohr Inc. |
| 12208878 | Door arrangement for use on an aircraft | Jan 11, 22 | Jan 28, 25 | Goodrich Actuation Systems Limited |
| 12186998 | Stringer plug | Nov 02, 18 | Jan 07, 25 | Not available |
| 12179905 | Cladding element having a heating layer in a sandwich construction | Nov 22, 19 | Dec 31, 24 | Airbus Operations GmbH |
| 12172392 | Composite-material aircraft part and method of manufacturing same | Mar 31, 21 | Dec 24, 24 | Kawasaki Jukogyo Kabushiki Kaisha |
| 12168507 | Aircraft structure and associated tools and methods | Mar 31, 21 | Dec 17, 24 | Ahmad AlDarwish |
| 12168525 | Composite-material aircraft part and method of manufacturing same | Jun 03, 21 | Dec 17, 24 | Kawasaki Jukogyo Kabushiki Kaisha |
| 12162600 | Aircraft panel assembly | May 13, 20 | Dec 10, 24 | Airbus Operations Limited; Airbus Operations GmbH; |
| 12162615 | Aircraft equipped with at least one pressure-relief device including a mobile wall retained in a closed position | Jun 13, 23 | Dec 10, 24 | Airbus Operations SAS |
| 12157136 | Sprayable sealant for aircraft parts and assemblies | Feb 07, 22 | Dec 03, 24 | The Patent Well LLC |
| Publication # | Title | Filing Date | Pub Date | Patent Owner |
|---|---|---|---|---|
| 2025/0101,252 | SELF-HEALING COATING, SELF-HEALING AIRCRAFT EXTERNAL SURFACE AND ITS MANUFACTURING METHOD AND REPAIRING METHOD OF AN AIRCRAFT EXTERNAL SURFACE | Jul 19, 24 | Mar 27, 25 | Not available |
| 2025/0100,941 | AUXETIC MATERIALS AND STRUCTURES FOR CERAMIC MATRIX COMPOSITE AIRFOIL MANDRELS | Sep 21, 23 | Mar 27, 25 | Not available |
| 2025/0074,593 | SYSTEMS, METHODS, AND AIRCRAFT FOR MANAGING CENTER OF GRAVITY | Nov 18, 24 | Mar 06, 25 | Not available |
| 2025/0065,346 | CLEAR, RAPID CURE SPRAYABLE FOR AIRCRAFT SURFACES | Nov 14, 24 | Feb 27, 25 | Not available |
| 2025/0065,595 | SANDWICH STRUCTURE, METHOD OF PRODUCING SANDWICH STRUCTURE, AND AIRCRAFT | Aug 12, 24 | Feb 27, 25 | SUBARU CORPORATION; GH CRAFT LTD.; |
| 2025/0058,870 | HYBRID-USE ROTARY-WING AIRCRAFT WITH ALIGNED DRIVETRAIN | Jan 13, 23 | Feb 20, 25 | Not available |
| 2025/0033,298 | COMPOSITE ELEMENT AND METHOD OF MANUFACTURING THE SAME | Oct 09, 24 | Jan 30, 25 | Not available |
| 2025/0030,173 | A PROTECTIVE STRUCTURE | Oct 26, 22 | Jan 23, 25 | Not available |
| 2025/0010,560 | FIBER-REINFORCED COMPOSITE LAYUP | Sep 18, 24 | Jan 09, 25 | Not available |
| 2025/0010,971 | RIGID OPEN COMPOSITE PANEL | Nov 16, 22 | Jan 09, 25 | Not available |
| 2025/0010,996 | AIRCRAFT AND BLI PROPULSION SECTION | Oct 12, 22 | Jan 09, 25 | Not available |
| 2024/0425,193 | AIRCRAFT COOLING DEVICE | Jun 11, 24 | Dec 26, 24 | Not available |
| 2024/0418,206 | Decompression Lock | Oct 28, 22 | Dec 19, 24 | 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 |
| 2024/0400,226 | Method For Joining A Window Frame To A Fuselage Skin Of An Aircraft Made Of A Fiber Composite Material | May 30, 24 | Dec 05, 24 | Premium Aerotec GmbH |
| 2024/0392,820 | FASTENING ELEMENT WITH SELECTIVELY ELONGATABLE BODY | May 03, 24 | Nov 28, 24 | Not available |
| 2024/0375,789 | METHOD FOR MANUFACTURING A BOX-SHAPED STRUCTURE IN COMPOSITE MATERIAL FOR AIRCRAFTS | May 06, 24 | Nov 14, 24 | Not available |
| 2024/0326,354 | METHOD FOR THE MANUFACTURE OF A STRUCTURAL COMPONENT IN COMPOSITE MATERIAL REINFORCED WITH STIFFENING STRINGERS AND STRUCTURAL COMPONENT | Dec 22, 21 | Oct 03, 24 | Not available |
| 2024/0294,252 | Distributed Propulsion System for Vertical Take Off and Landing Closed Wing Aircraft | May 14, 24 | Sep 05, 24 | Not available |
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