Patents for B64D 27 - Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby (3,375)
09/2008
09/16/2008CA2376126C Tandem powered power tilting aircraft
09/16/2008CA2314570C Power plant for propeller aircraft
09/11/2008US20080217502 Monolithic Framework Engine Mounting Structure
09/11/2008US20080217468 Mast for an aircraft nacelle incorporating means for limiting the appearance of vibrations, in particular in certain flight regimes, at a high mach number and low lift
09/11/2008US20080217467 Assembly For Aircraft Comprising a Wing System Element as Well as an Attachment Mast
09/11/2008US20080216483 Engine Assembly for Aircraft Comprising an Engine as Well as a Device for Locking Said Engine
09/10/2008CN101263055A Method for mounting an aircraft engine on a rigid structure of a strut for locking the engine
09/10/2008CN101263054A Strut for locking the engine of an aircraft
09/04/2008US20080210811 Aircraft Engine Unit
09/04/2008DE4435060B4 Vorrichtung an Antrieben für extrem hoch fliegende Luftfahrzeuge Device on drives for extremely high-flying aircraft
09/03/2008EP1506354B1 Fusible link comprising damper and backstop
09/02/2008US7419121 Integrated mount duct for use with airborne auxiliary power units and other turbomachines
08/2008
08/28/2008WO2008080135A3 Flight dynamics for an aircraft
08/28/2008US20080203219 Hydrogen powered aircraft
08/27/2008CN101253094A System for connecting a crossbar to an aircraft engine pylon
08/21/2008US20080197262 Engine Mounting Structure for an Aircraft
08/21/2008US20080197233 Engine Mounting Structure For an Aircraft
08/21/2008DE10300621B4 Strahlantriebsverfahren zB für ein Segelflugzeug Jet propulsion methods, eg for a glider
08/14/2008WO2008097325A2 Airfoil having a movable control surface
08/14/2008WO2008096073A2 Aircraft fuselage
08/14/2008US20080191088 Aircraft Jet Engine Pylon Suspension Attachment
08/14/2008US20080191087 Low-Noise Aircraft, Particularly at Take-Off and Landing
08/14/2008US20080190096 Fluid mixer with an integral fluid capture ducts forming auxiliary secondary chutes at the discharge end of said ducts
08/14/2008CA2673443A1 Aircraft fuselage
08/13/2008EP1954563A1 Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft
08/07/2008WO2008054521A3 Long endurance hydrogen powered vehicle
08/07/2008US20080187809 Energy storage system
08/07/2008US20080185475 Solar-powered aircraft
08/06/2008EP1539573B1 Torsionally de-coupled engine mount system
08/06/2008CN100408823C Connector assembly for mounting a gas turbine engine
08/05/2008US7407133 Using imbalanced thrust in a multi-engine jet aircraft
07/2008
07/30/2008CN101233047A Improved primary engine strut structure of an aircraft
07/30/2008CN101233046A Assembly for aircraft comprising a wing system element as well as an attachment mast
07/29/2008CA2389008C Aircraft and method for operating an aircraft
07/17/2008US20080169378 Engine Fastener Of A Mounting System Interposed Between An Attachment Strut And An Aircraft Engine
07/17/2008US20080169377 Mounting device for an aircraft engine comprising two thrust recovery rods with a double rear mechanical connection
07/17/2008US20080169375 Vertically movable flying body
07/16/2008EP1943145A2 Turbojet engine front fastening device provided with a strut for fixing to an aircraft
07/16/2008EP1943144A1 Aircraft having a reduced environmental impact
07/16/2008EP1942846A2 Stabilizing power source for a vehicle
07/15/2008US7398945 Cast unitized primary truss structure and method
07/10/2008WO2008081098A1 Aircraft with rear annular tail
07/10/2008WO2008048830A3 Apparatus and method pertaining to light-based power distribution in a vehicle
07/10/2008US20080166613 Energy storage system
07/10/2008US20080166603 Energy storage system
07/10/2008CA2670649A1 Aircraft with rear annular tail
07/09/2008EP1940682A1 Engine assembly for aircraft
07/09/2008CN100400808C Reciprocating fluid engine
07/03/2008WO2008080135A2 Flight dynamics for an aircraft
07/03/2008WO2008043903A3 Bypass turbojet engine nacelle
07/03/2008US20080156930 Engine Mount For an Aircraft, to be Placed Between an Engine and an Engin Mounting Structure
06/2008
06/26/2008US20080149761 Main wing structure of aircraft
06/26/2008US20080149760 Flight dynamics for an aircraft
06/26/2008DE10037539B4 Einstellbarer Schwenkrotor-Abwärts-Stop mit geringer Höhe Adjustable tilt rotor-down stop of low height
06/25/2008EP1934093A1 Nut system and aircraft engine mounting structure comprising same
06/19/2008US20080142641 Airplane configuration
06/19/2008US20080142637 Electric connector assembly having a device for protection against pollution
06/18/2008EP1931568A1 Rigid framework for aircraft engine mounting structure and engine mounting structure comprising same
06/18/2008EP1931567A1 Turbojet engine mounting structure for aircraft
06/18/2008CN101203425A Engine mount for an aircraft, to be placed between an engine and an engin mounting structure
06/12/2008US20080135679 Turbine engine mounting arrangement
06/11/2008EP1929140A1 Two-shackle aircraft engine rear attachment
06/11/2008EP1928742A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure
06/11/2008EP1928741A1 Monolithic framework engine mounting structure
06/11/2008EP1928740A1 Strut for locking the engine of an aircraft
06/11/2008EP1928739A1 Method for mounting an aircraft engine on a rigid structure of a strut for locking the engine
06/11/2008EP1928738A1 Engine mounting structure interposed between an aircraft wing system and said engine
06/11/2008EP1928736A1 Engine assembly for aircraft comprising an engine as well as a device for locking said engine
06/11/2008EP1789320B1 Turbojet pylon for aircraft
06/05/2008WO2008065065A1 Propulsion device with a plurality of energy converters for an aircraft
06/05/2008WO2008064881A1 Propulsion device for operation with a plurality of fuels for an aircraft
06/05/2008US20080128547 Two-stage hypersonic vehicle featuring advanced swirl combustion
06/05/2008DE102006056356A1 Drive device for aircraft, has energy converters which are attached for supplying drive unit with operating powers, where drive unit is attached for producing form feed using one operating power
06/05/2008DE102006056355A1 Drive device for aircraft, has energy converter e.g. gas turbine, for providing operating power of drive unit by two different fuels such as kerosene and hydrogen, and drive unit generating feed rate by operating power
06/05/2008DE102006056354A1 Hybrid drive device for aircraft, has gas turbine unit and electric motor arranged such that drive unit is supplied with operating power of gas turbine unit or motor, and drive unit producing form feed using one of operating powers
06/05/2008CA2665132A1 Propulsion device for operation with a plurality of fuels for an aircraft
06/05/2008CA2663357A1 Propulsion device with a plurality of energy converters for an aircraft
06/04/2008CN100391566C Toy airplane assembly having a microprocessor for assisting flight
05/2008
05/29/2008US20080121756 Unconventional Integrated Propulsion Systems and Methods for Blended Wing Body Aircraft
05/29/2008US20080121755 Rankine-Brayton engine powered solar thermal aircraft
05/29/2008US20080121754 Damage-tolerant attachment system for an aircraft engine
05/29/2008DE19919626B4 Flugzeug mit Verbundflächen Aircraft with composite surfaces
05/27/2008US7377832 Electric powered flying wing toy
05/21/2008EP1922250A1 System for connecting a crossbar to an aircraft engine pylon
05/21/2008EP1814783B1 System for fixing an engine pylon to an aircraft wing
05/21/2008CN101181933A Double-power driven single-wing fixed-wing aircraft
05/14/2008EP1921007A2 A turbine engine mounting arrangement
05/14/2008CN101180213A Engine assembly for aircraft
05/08/2008WO2008054521A2 Long endurance hydrogen powered vehicle
05/08/2008US20080105782 Mounting system for use in mounting a gas turbine engine
05/08/2008US20080105781 Aircraft with reduced environmental impact
05/07/2008EP1918199A2 Aicraft airframe architecture
05/07/2008EP1918065A1 Engine mount bearing sleeve repair
05/07/2008CN100386246C Electric-based secondary power system architectures for aircraft
05/07/2008CN100386245C Transportation means for marine, land and air
04/2008
04/30/2008EP1916406A2 Aircraft propulsion systems
04/30/2008CA2590892A1 Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof
04/29/2008US7364118 Propulsion arrangement
04/24/2008WO2008046872A1 Aircraft with hybrid aerodynamic and space flight, and associated flight control method
04/22/2008US7360986 System for blocking a main shaft of an engine having a fusible bearing
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