Patents
Patents for B64C 7 - Structures or fairings not otherwise provided for (830)
11/2005
11/22/2005US6966524 Aircraft engine nacelles and methods for their manufacture
11/16/2005EP1595067A2 Recessed engine nacelle
11/15/2005US6964397 Nacelle chine installation for drag reduction
11/10/2005US20050247821 Transition shim between structure for fastening a wing to a fuselage of an aircraft, and aircraft having such a shim
11/10/2005DE202005014077U1 Load-limiting securing arrangement for ceiling mounting of equipment in aircraft has mounting rails each having side attached to support structure, with side able to deform while keeping equipment attached to support structure
11/09/2005EP1593594A1 Transition shim between a means for fastening a wing to a fuselage of an aircraft and the wing, and aircraft comprising such a shim
11/03/2005US20050242237 Vtol aircraft external load drag reduction system
11/03/2005DE10339030B4 Tragstruktur für eine ein- und ausfahrbare Klappe und deren Verwendung Support structure for an extendable and retractable flap and its use
10/2005
10/26/2005EP1588938A1 Aerodynamic fairing for an aircraft landing gear
10/20/2005CA2503097A1 Aerodynamic flow deflector for aircraft landing gear
09/2005
09/27/2005US6948682 Lifting body aircraft and reentry vehicle
09/20/2005US6945031 Recessed engine nacelle
09/15/2005WO2005085065A1 Static port skin applique apparatus and method
09/06/2005US6938854 Integrated and/or modular high-speed aircraft
09/01/2005WO2005024218A3 Recessed engine nacelle
08/2005
08/18/2005US20050178885 Method and apparatus for supporting aircraft components, including actuators
07/2005
07/27/2005EP1556275A1 Landing gear
07/07/2005WO2005061323A1 Aircraft fluid cooling system and an aircraft provided with said system
06/2005
06/14/2005CA2146812C Protective device for a control surface hinge, as for an aircraft
06/02/2005US20050116116 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
05/2005
05/26/2005WO2004099602A3 Self-aligning thrust reverser system lock assembly
05/06/2005WO2005044661A2 Supersonic aircraft with aerodynamic control
04/2005
04/26/2005US6883806 Notched blade seal for high performance aircraft
03/2005
03/31/2005US20050067525 Aircraft thickness/camber control device for low sonic boom
03/31/2005DE10339030A1 Tragstruktur für eine ein- und ausfahrbare Klappe und deren Verwendung Support structure for an extendable and retractable flap and its use
03/17/2005WO2005024218A2 Recessed engine nacelle
03/10/2005WO2005021375A1 Support structure for a retractable and extendable flap, and use of said structure
03/03/2005US20050045764 Canard position and dihedral for boom reduction and pitch/directional control
02/2005
02/15/2005US6854687 Nacelle integration with reflexed wing for sonic boom reduction
01/2005
01/25/2005US6845943 Apparatuses and methods for preventing foreign object damage to aircraft engines
01/20/2005WO2004081103A3 Method for lowering the melt viscosity of an aromatic sulfone polymer composition, and method for manufacturing an aircraft component
01/20/2005US20050011993 Nacelle chine installation for drag reduction
01/06/2005US20050001095 Self-aligning thrust reverser system lock assembly
12/2004
12/23/2004US20040255572 Aircraft engine in which there is a small clearance separating the fan cowls and the thrust inverter cowls
12/22/2004EP1488999A1 Aircraft engine cowling with reduced gap
11/2004
11/18/2004WO2004099602A2 Self-aligning thrust reverser system lock assembly
10/2004
10/21/2004WO2004089743A1 Landing gear door assembly
10/21/2004WO2004089742A1 Landing gear
09/2004
09/23/2004WO2004081103A2 Method for lowering the melt viscosity of an aromatic sulfone polymer composition, and method for manufacturing an aircraft component
09/22/2004CN1167577C Self check test for test-control and electronic system of co-axled double rotary wing pilotless helicoper
09/07/2004US6786451 Aircraft landing gear having an independent low-noise fairing system
09/01/2004CN1525920A Integrated and/or modular high-speed aircraft
08/2004
08/26/2004US20040164204 Recessed engine nacelle
08/04/2004EP1192077B1 Aircraft noise reduction apparatus
07/2004
07/29/2004US20040144889 Aircraft engine nacelles and methods for their manufacture
06/2004
06/03/2004US20040104301 Aeroplane provided with noise-reducing means, as well as a landing gear and blowing means
05/2004
05/13/2004WO2004039671A1 Landing gear
05/04/2004US6729583 Device for articulating a flap to an aircraft aerodynamic surface
04/2004
04/29/2004US20040079836 Apparatuses and methods for preventing foreign object damage to aircraft engines
04/20/2004CA2193789C Spherical mating fairings for hingeline applications
03/2004
03/10/2004EP1396422A1 Aircraft engine nacelle with a landing gear bay and method for its manufacture
01/2004
01/29/2004US20040016845 Integrated and/or modular high-speed aircraft
01/21/2004EP1382526A1 Aircraft noise reduction device
12/2003
12/18/2003US20030230677 Device for articulating a flap to an aircraft aerodynamic surface
12/17/2003EP1371552A1 Articulation device for connecting a flap to an aircraft aerodynamic surface
12/16/2003US6663368 Spherical gear pump
11/2003
11/26/2003EP1365081A2 Structural element with rib-receiving member
11/25/2003US6651928 Aircraft engine nacelles and methods for their manufacture
10/2003
10/15/2003EP1351855A2 Integrated and/or modular high-speed aircraft
09/2003
09/16/2003US6619587 Aircraft noise reduction apparatus
09/04/2003US20030164423 Aircraft landing gear having an independent low-noise fairing system
09/03/2003EP1340676A1 Aircraft landing gear with an autonomous aero-acoustic fairing system
08/2003
08/27/2003EP1066195B1 Permanently connected remote latch mechanism
06/2003
06/24/2003US6581877 Aircraft with ventral fairing and seal for such an aircraft
06/10/2003US6575407 Subdermally-reinforced elastomeric transitions
06/10/2003US6575406 Integrated and/or modular high-speed aircraft
06/05/2003US20030102406 Aircraft noise reduction apparatus
04/2003
04/23/2003CN1412081A Aircraft
04/23/2003CN1412080A Aircraft
04/10/2003DE20300316U1 Conically extending surface profiles by their combination and position in relation to each other and together with parallel side surfaces create symmetrical housing
04/03/2003WO2003026961A1 Notched blade seal for high performance aircraft
04/02/2003EP1206382B1 A fairing arrangement for an aircraft
03/2003
03/27/2003WO2002079031A3 Integrated and/or modular high-speed aircraft
03/27/2003US20030057659 Notched blade seal for high performance aircraft
03/25/2003US6536711 Single aperture conformal aircraft bays
02/2003
02/11/2003US6517289 Inflatable vibration reducing fairing
01/2003
01/09/2003US20030006344 Aircraft with ventral fairing and seal for such an aircraft
01/08/2003EP1273512A1 Aircraft with belly fairing seal
10/2002
10/10/2002WO2002079031A2 Integrated and/or modular high-speed aircraft
10/10/2002CA2434163A1 Integrated and/or modular high-speed aircraft
09/2002
09/25/2002EP1025375B1 Elastic spring element
09/17/2002US6450457 Fairing arrangement for an aircraft
08/2002
08/28/2002EP0888497B1 System and method for diverting boundary layer air
07/2002
07/25/2002US20020096598 Integrated and/or modular high-speed aircraft
07/17/2002CN1358649A Self-check test for test-control and electronic system of axle-shared double-rotary wing pilotless helicopter
06/2002
06/25/2002US6409123 Aircraft wing structure profiled suspension pylon
05/2002
05/28/2002US6394389 Aircraft lift arrangement
05/22/2002EP1206382A1 A fairing arrangement for an aircraft
05/02/2002EP1066195A4 Permanently connected remote latch mechanism
04/2002
04/30/2002US6378804 Aircraft wing structure profiled suspension pylon
04/30/2002US6378802 Enhance aerodynamic profile
04/24/2002EP0923488B1 Detachable integral aircraft tailcone and power assembly
04/18/2002US20020043590 Subdermally-reinforced elastomeric transitions
04/03/2002EP1192077A1 Aircraft noise reduction apparatus
04/02/2002US6364254 Aircraft airfoil with close-mounted engine and leading edge high lift system
03/2002
03/28/2002US20020037231 Spherical gear pump
03/19/2002US6357733 Elastic spring element
01/2002
01/16/2002CN1077858C Hinged shaft radome
10/2001
10/17/2001EP1145953A1 Airfoiled engine pylon for aircraft wing
10/11/2001US20010028019 Aircraft wing structure profiled suspension pylon
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