Class B64C : AEROPLANES; HELICOPTERS
Subclass 1/06: 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) Frames; Stringers; Longerons
| Patent # | Title | Filing Date | Issue Date | Patent Owner |
|---|---|---|---|---|
| 12263946 | Installment system for overhead bins | Nov 18, 22 | Apr 01, 25 | Textron Innovations Inc. |
| 12257817 | Composite panel structure and method of manufacturing | Mar 30, 20 | Mar 25, 25 | Kawasaki Jukogyo Kabushiki Kaisha |
| 12252271 | Methods and systems for assembly and installation of airframe crown modules | Nov 10, 21 | Mar 18, 25 | The Boeing Company |
| 12247554 | Environmental aspect control assembly | Oct 10, 23 | Mar 11, 25 | THE BOEING COMPANY |
| 12246852 | Frame installation station for aircraft fuselage segments | Nov 10, 21 | Mar 11, 25 | The Boeing Company |
| 12246817 | Thermoplastic cover panel for a structure in an interior space of an aircraft | Jun 16, 23 | Mar 11, 25 | Airbus Operations GmbH |
| 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 |
| 12234033 | Modular container transport systems | Sep 05, 23 | Feb 25, 25 | Biosphere Aerospace, LLC |
| 12227306 | Flying vehicle systems and methods | Nov 01, 22 | Feb 18, 25 | Workhorse Group Inc. |
| 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 |
| 12221203 | System for installing decoration panels to an aircraft ceiling assembly | Feb 13, 24 | Feb 11, 25 | THE BOEING COMPANY |
| 12214857 | Beaded composite structural web | Mar 22, 23 | Feb 04, 25 | Textron Innovations Inc. |
| 12214876 | Cover panel | Aug 11, 21 | Feb 04, 25 | Airbus Operations Limited |
| 12194651 | Cut-out processes for moving-line structure assembly | Nov 10, 21 | Jan 14, 25 | The Boeing Company |
| 12195163 | Modular line assembly for installation in an aircraft fuselage | Dec 01, 23 | Jan 14, 25 | Airbus Operations GmbH |
| 12195165 | Helicopter tail folding mechanism | Nov 28, 23 | Jan 14, 25 | TUSAS—TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI |
| 12195162 | Helicopter tail folding system | Nov 28, 23 | Jan 14, 25 | TUSAS- TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI |
| Publication # | Title | Filing Date | Pub Date | Patent Owner |
|---|---|---|---|---|
| 2025/0108,908 | AIRCRAFT TANK DEVICE FOR INCREASING A FLIGHT RANGE AND A WING AREA OF AN AIRCRAFT AS WELL AS AIRCRAFT | Sep 16, 24 | Apr 03, 25 | Airbus Operations GmbH |
| 2025/0100,668 | Raised Decorative Laminate Panel and Method | Sep 22, 23 | Mar 27, 25 | Not available |
| 2025/0100,669 | AIRCRAFT FUSELAGE WING ATTACHMENT CUTOUT CONFIGURATIONS INCORPORATING PERIMETER BOX BEAMS | Dec 16, 21 | Mar 27, 25 | Not available |
| 2025/0083,791 | DRY FIBER CONSTRUCTION OF A BLENDED WING BODY AIRCRAFT AND METHOD OF MANUFACTURE | Sep 07, 23 | Mar 13, 25 | JETZERO, INC. |
| 2025/0083,792 | CIRCUMFERENTIAL SKIN JOINTS FOR AEROSPACE STRUCTURES, METHODS OF ASSEMBLING THE JOINTS, AND METHODS OF MANUFACTURING FUSELAGE MEMBERS THAT DEFINE THE JOINTS | Sep 07, 23 | Mar 13, 25 | Not available |
| 2025/0083,835 | METHOD FOR MANUFACTURING A MONOLITHIC COMPONENT | Sep 05, 24 | Mar 13, 25 | Not available |
| 2025/0074,593 | SYSTEMS, METHODS, AND AIRCRAFT FOR MANAGING CENTER OF GRAVITY | Nov 18, 24 | Mar 06, 25 | Not available |
| 2025/0066,010 | PANELS | Aug 16, 24 | Feb 27, 25 | B/E AEROSPACE (UK) LIMITED |
| 2025/0058,489 | Cut-Out Processes for Moving-Line Structure Assembly | Nov 04, 24 | Feb 20, 25 | Not available |
| 2025/0058,872 | COMPACT PERSONAL FLIGHT VEHICLE | Nov 06, 24 | Feb 20, 25 | Not available |
| 2025/0058,894 | SYSTEM AND METHOD FOR TETHERED UNMANNED AERIAL VEHICLE TAKEOFF, LANDING, AND STORAGE | Nov 06, 24 | Feb 20, 25 | Not available |
| 2025/0033,298 | COMPOSITE ELEMENT AND METHOD OF MANUFACTURING THE SAME | Oct 09, 24 | Jan 30, 25 | Not available |
| 2025/0033,317 | STIFFENING STRUCTURE AND METHOD FOR STIFFENING A SHEET ELEMENT | Oct 02, 24 | Jan 30, 25 | Photon AG |
| 2025/0026,465 | ASSEMBLY COMPRISING AT LEAST ONE CONNECTING ELEMENT AND AT LEAST TWO CONTACT SURFACES PROVIDED WITH ASPERITIES, AIRCRAFT COMPRISING AT LEAST ONE SUCH ASSEMBLY | Jul 10, 24 | Jan 23, 25 | Not available |
| 2025/0026,466 | CABIN LINING ELEMENT FOR AN AIRCRAFT CABIN AND RIB FOR AN AIRCRAFT FUSELAGE STRUCTURE | Oct 02, 24 | Jan 23, 25 | Not available |
| 2025/0030,173 | A PROTECTIVE STRUCTURE | Oct 26, 22 | Jan 23, 25 | Not available |
| 2025/0010,972 | STRUCTURAL SHAPE MODE INFLUENCERS | Jul 05, 23 | Jan 09, 25 | Not available |
| 2025/0002,175 | MOUNTING INTERFACE FOR TRUSSWORK | Jun 11, 24 | Jan 02, 25 | Not available |
| 2024/0418,318 | SEGMENTED VACUUM JACKETED TANK SYSTEM AND METHOD OF USING THE SAME | Jun 17, 23 | Dec 19, 24 | THE BOEING COMPANY |
| 2024/0417,055 | ROD WITH ATTACHMENT SOCKETS FOR A TRUSS STRUCTURE OF A VEHICLE | Jun 05, 24 | Dec 19, 24 | Not available |
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