| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 01/11/2012 | EP2404824A2 Aircraft structure and Method for producing it |
| 01/11/2012 | EP2403756A1 Decompression assembly for an aircraft |
| 01/11/2012 | EP2403755A2 Connection system, and especially adapter module provided therefor |
| 01/11/2012 | EP2403754A2 Connecting device |
| 01/11/2012 | CN102317153A Longitudinal joint for aircraft fuselage panels made of composite materials |
| 01/11/2012 | CN102317057A Method for producing a shell body and corresponding body |
| 01/11/2012 | CN102310941A Aircraft structural assembly and associated assembling method |
| 01/10/2012 | US8093531 Method of energy beam welding aluminum to titanium |
| 01/10/2012 | US8091833 Vibration isolation devices and associated systems and methods |
| 01/10/2012 | US8091832 Nacelle cowling for turbojet and nacelle comprising at least one such cowling |
| 01/10/2012 | US8091831 Aircraft with door seal arrangement |
| 01/10/2012 | US8091828 Structural element and method of manufacture |
| 01/10/2012 | DE202010013869U1 Innenausstattungselement für Fahrzeugkabinen Interior design element for vehicle cabs |
| 01/10/2012 | CA2531700C Sealing device for a flap track in a belly fairing of an aircraft for a flap-actuating shaft |
| 01/05/2012 | WO2012001207A2 Aircraft fuselage made out with composite material and manufacturing processes |
| 01/05/2012 | WO2012001206A2 Internal structure of aircraft made of composite material |
| 01/05/2012 | WO2012001205A2 Aircraft component comprising panels stiffened with stringers having two types of local flarings |
| 01/05/2012 | US20120001025 Device for fastening systems for an aircraft, adapted in particular to be used in relation to a window |
| 01/05/2012 | US20120001024 Internal structure of aircraft made of composite material |
| 01/05/2012 | US20120001023 Aircraft fuselage made out with composite material and manufacturing processes |
| 01/05/2012 | US20120001022 Jet engine installation |
| 01/05/2012 | CA2804095A1 Aircraft fuselage made out with composite material and manufacturing processes |
| 01/05/2012 | CA2804094A1 Internal structure of aircraft made of composite material |
| 01/04/2012 | EP2401196A1 Signal and energy transmitting support structure |
| 01/04/2012 | EP2401195A2 Distributing power in systems having a composite structure |
| 01/04/2012 | CN102307782A Structure of the load-introduction area in the fuselage rear section of an aircraft |
| 01/04/2012 | CN101180208B Apparatus, system and method for drag reduction |
| 01/03/2012 | US8087615 Window installation method |
| 01/03/2012 | US8087614 Stringer for an aircraft wing and a method of forming thereof |
| 01/03/2012 | US8087607 Airplane configuration |
| 01/03/2012 | CA2649125C Composite wing-body joint |
| 12/29/2011 | WO2011163453A1 Door apparatus and method |
| 12/29/2011 | WO2011127899A3 Aircraft with an integrated energy-absorbing deformation structure and aircraft with such a fuselage |
| 12/29/2011 | US20110315824 Composite structures having integrated stiffeners and method of making the same |
| 12/29/2011 | US20110315823 Fixation mechanism for installing thermal insulation sheets in an aircraft body |
| 12/29/2011 | US20110315822 Door apparatus and method |
| 12/29/2011 | US20110315821 Method for assembling a floor in a cockpit structure previously constructed from a section of aircraft fuselage |
| 12/29/2011 | US20110315820 Aircraft structural assembly and associated assembling method |
| 12/29/2011 | US20110315819 Supersonic Aircraft with Spike for Controlling and Reducing Sonic Boom |
| 12/29/2011 | DE102010051739B3 Verfahren und Vorrichtung zum Herstellen von zylindrischen Großstrukturen Method and apparatus for producing large cylindrical structures |
| 12/29/2011 | DE102010025488A1 Retractable engine for airplanes, has building block secured at low end of circular, uniformly wide motor carrier, which is connected to upper and lower edges by guide elements in halt frame near fuselage aperture |
| 12/29/2011 | DE102010024698A1 Verfahren, Vorrichtung und Anordnung zur Entfernung organischer Verschmutzung von Anströmbereichen eines Luftfahrzeugs Method, apparatus and system for removal of organic pollution of Anströmbereichen an aircraft |
| 12/28/2011 | EP2399824A1 Device for supporting an insulating mattress and attaching systems intended to be mounted in an aircraft |
| 12/28/2011 | EP2399823A1 Attachment assembly including ramps for attaching systems in an aircraft |
| 12/28/2011 | EP2399822A1 Device for supporting an insulated mattress and attaching systems |
| 12/28/2011 | EP2399821A1 Insulated mattress for an aircraft and assembly including such a mattress |
| 12/28/2011 | EP2399820A1 Device for attaching aircraft systems, in particular intended for use about a window |
| 12/28/2011 | EP2399819A1 Device in two parts for supporting an insulating mattress and for attaching systems |
| 12/28/2011 | EP2398636A1 Method for producing a shell body and corresponding body |
| 12/28/2011 | CN202089233U 气动式座舱安全活门排气阀位置指示装置 Pneumatic cockpit safety valve exhaust valve position indicating device |
| 12/28/2011 | CN202089232U Mouth cover covering long truss |
| 12/28/2011 | CN102300703A 用于喷气发动机机舱的结构板的蜂窝芯体结构 Honeycomb core structure structural panels for jet engine nacelle |
| 12/28/2011 | CN102295072A 一种飞机单层空气-液体蒙皮热交换方法 An aircraft single air - liquid skin heat exchange method |
| 12/28/2011 | CN102295071A 一种可伸缩桁架结构及其制作方法 A scalable truss structure and production methods |
| 12/28/2011 | CN102295070A 一种飞机双层空气-液体蒙皮热交换方法 An aircraft double air - liquid skin heat exchange method |
| 12/28/2011 | CN101360648B 可变形的飞机前方耐压舱壁 Deformable pressure bulkhead ahead of the aircraft |
| 12/27/2011 | US8084114 Reinforced rampdown for composite structural member and method for same |
| 12/27/2011 | US8083183 Air discharge device for an aircraft |
| 12/27/2011 | US8083182 Monolithic self-stiffened panels |
| 12/27/2011 | US8083181 Airplane having a fuselage shell and a floor structure |
| 12/27/2011 | US8083175 Loading fitting having intersecting holes in the web side and end |
| 12/27/2011 | US8082707 Air-film vibration damping apparatus for windows |
| 12/22/2011 | US20110309196 Device for holding an insulating blanket and for fastening two-parts systems |
| 12/22/2011 | US20110309194 Mounting System for Attaching a Structural Monument in a Desired Position in an Aircraft Cabin |
| 12/22/2011 | DE102010024120A1 Stützprofil, Verfahren zur Herstellung eines Stützprofils, sowie dessen Verwendung in einem Verfahren zur Herstellung eines verstärkten Fahrzeugrumpfbauteils Supporting profile, process for the preparation of a support profile, and the use thereof in a process for producing a reinforced vehicle body member |
| 12/22/2011 | DE102006058577B4 Motorisch betriebene Frachtantriebseinheit und Verfahren zum Betreiben einer solchen Frachtantriebseinheit A power driven load drive unit, and method for operating such a load drive unit |
| 12/21/2011 | EP2398122A2 Conduit harness holder |
| 12/21/2011 | EP2397402A2 Structural Panel with integrated reinforcement |
| 12/21/2011 | EP1881928B1 Helicopter one-piece door |
| 12/21/2011 | EP1144785B2 Quick release and fastening cover |
| 12/21/2011 | CN202081756U 一种飞机舱门可调式合页 An aircraft adjustable door hinge |
| 12/21/2011 | CN202081715U 一种飞机舱门锁内把手 An aircraft door inside lock knob |
| 12/21/2011 | CN202080434U 轻型旋翼飞机 Light Rotorcraft |
| 12/21/2011 | CN202080431U 一种智能蒙皮 An intelligent skin |
| 12/21/2011 | CN102292210A 制造涡轮喷气发动机舱用的具有孔格芯体的结构的方法 The method has the structure of the cells of the core turbojet engine compartment used for producing |
| 12/21/2011 | CN102285457A 具有辅助动力单元的飞行器后机身尾锥结构 After the aircraft fuselage having an auxiliary power unit tail cone structure |
| 12/21/2011 | CN102285455A 一种飞机机身结构爆破切割防护方法 An aircraft fuselage structure blasting cut protection methods |
| 12/20/2011 | US8082052 Method and apparatus for ensuring the dimensional constancy of multisegment physical structures during assembly |
| 12/20/2011 | US8079550 Auxiliary power unit inlet door actuation mechanism |
| 12/20/2011 | US8079549 Monolithic integrated structural panels especially useful for aircraft structures |
| 12/15/2011 | WO2011154582A2 Procedure for the manufacture of large parts of composite material controlling the thickness of the edges thereof |
| 12/15/2011 | US20110303792 Telescopic strut |
| 12/15/2011 | US20110303791 Fuselage Section of an Aircraft and Method for the Production of the Fuselage Section |
| 12/15/2011 | US20110303786 Silencer for an auxiliary power unit of an aircraft |
| 12/15/2011 | DE102010023496A1 Method for manufacturing body segment of airplane from fiber reinforced composites, involves providing tooling with tooling surface |
| 12/14/2011 | EP2394910A1 Openable aircraft window and aircraft equipped with such a window |
| 12/14/2011 | EP2394909A1 Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
| 12/14/2011 | EP2393652A1 Honeycomb core structure for use in a structural panel for a jet engine nacelle |
| 12/14/2011 | EP2393651A1 Method for manufacturing a structure with cellular cores for a turbojet nacelle |
| 12/14/2011 | EP2185409B1 Aircraft component mounting system |
| 12/14/2011 | CN102282070A 飞机水平稳定面 Aircraft horizontal stabilizer surface |
| 12/14/2011 | CN102282067A 用于连接本体蒙皮的角区段 Horn section for connecting the body skin |
| 12/13/2011 | US8075234 Expandable collet anchor system and method |
| 12/13/2011 | US8074930 Door for opening and closing a door aperture in an aircraft |
| 12/13/2011 | US8074929 Methods and systems for composite structural truss |
| 12/13/2011 | US8074928 Floor system for a fuselage airframe of an aircraft |
| 12/08/2011 | US20110297788 Shell component for an aircraft or spacecraft |
| 12/08/2011 | US20110297787 Dual function door for an aircraft engine nacelle |
| 12/08/2011 | US20110297785 Airframe position adjusting structure |
| 12/08/2011 | US20110297333 Window Shade Assembly |