Matches 1 - 50 out of 345 1 2 3 4 5 6 7 >


Match Document Document Title
US20130256453 RAM AIR TURBINE STOW ABORT ASSEMBLY  
An example ram air turbine stow abort assembly includes a release pin movable between an engaged position that prevents rotation of a drive shaft and a released position that allows rotation of...
US20120001019 PYLON FOR ATTACHING A GAS TURBINE ENGINE  
A pylon is provided for attachment of a gas turbine engine to a wing of an aircraft. The gas turbine engine comprises a core fairing surrounding a core generator and defining a nozzle for...
US20130015291 FIRE RESISTANT STRUCTURAL MOUNT YOKE AND SYSTEM  
A mount yoke assembly comprises a first main hanger bracket and a first anchor bracket. The first main hanger bracket includes a first receiving portion for a first auxiliary power unit (APU)...
US20150239568 PYLON SHAPE WITH GEARED TURBOFAN FOR STRUCTURAL STIFFNESS  
A gas turbine includes a mounting structure for mounting the engine to a pylon. A propulsor section includes a fan having a fan diameter. A geared architecture drives the fan. A generator section...
US20110127370 FAN COWL SUPPORT FOR A TURBO FAN ENGINE  
A fan cowl support for an aircraft having an engine pylon, an engine fan case and an engine fan cowl. The fan cowl support includes a support having a forward end connected to the engine fan case...
US20130221155 ENGINE ATTACHMENT PYLON  
An engine attachment pylon for mounting an aircraft engine to an aircraft structure while minimising vibrations induced into the engine attachment pylon during flight and operation of the engine....
US20150232188 AIRCRAFT  
An aircraft with a turbofan engine including an engine body and a fan, wherein the turbofan engine is supported on an airframe via a pylon, an igniter cable is interposed between an ignition plug...
US20110127367 FAN COWL SUPPORT FOR A TURBOFAN ENGINE  
A fan cowl support for an aircraft having an engine pylon, an engine fan case and an engine fan cowl. The fan cowl support includes a support having a forward end connected to the engine fan case...
US20120018577 ENGINE MOUNTING WITH AN ADAPTED LOAD/DEFORMATION CURVE  
The invention relates to a mounting for attaching an engine to an aircraft structure, said mounting including a metal spring and being adapted for fulfilling the following conditions: the...
US20150144733 Motor Pylons for a Kite and Airborne Power Generation System Using Same  
A motor pylon system adapted for use with an airborne power generations system is disclosed. The pylons may support turbine driven generators for wind based electrical power generation which also...
US20130221154 Motor Pylons For A Kite And Aiborne Power Generation System Using Same  
A motor pylon system adapted for use with an airborne power generations system is disclosed. The pylons may support turbine driven generators for wind based electrical power generation which also...
US20140312167 Ram Air Fan Mounting Bracket  
A bracket has an axial rear wall to be secured to a housing for a ram air fan and a base floor defined between lateral sidewalls. The base floor has a slot extending for an axial length and for a...
US20110127369 FAN COWL SUPPORT CRADLE MOUNTED ON THE ATTACHMENT PYLON AND ON THE AIR INLET OF THE NACELLE  
An engine unit for an aircraft including an engine, a device for hooking the engine, and a nacelle surrounding the engine and provided with fan cowls, the device for hooking including a rigid...
US20140117152 Twin Tip Turbine Propulsors Powered by a Single Gas Turbine Generator  
A gas turbine engine has a core engine incorporating a turbine, and a manifold positioned downstream of the turbine. The manifold delivers gas downstream of the turbine into at least two nacelles,...
US20110108662 ATTACHMENT PYLON FOR AN AIRCRAFT TURBO-SHAFT ENGINE WITH CONCENTRIC HOT AIR CHANNELS  
The invention relates to a pylon (14) for attaching a turbo-shaft aircraft engine designed to be laterally offset on a rear part of the aircraft structure, where the pylon possesses an aerodynamic...
US20150251768 ENGINE PYLON STRUCTURE  
A pylon structure for mounting an aircraft engine to a wing. The pylon structure comprises a torque box having a wing mount on the aft portion, a first engine mount on the fore portion and second...
US20130320134 AUXILIARY FIRE RESISTANT MOUNT SYSTEM FOR AN AUXILIARY POWER UNIT  
An auxiliary power unit is composed of a gas turbine engine, a gearbox, and a gearbox driven generator. A mount bracket is mechanically attached to the gearbox. The bracket is for connecting to an...
US20130161446 HINGING CRADLE FOR FAN COWLS SUPPORTED BY SAID COWLS IN CLOSED POSITION  
The invention relates to an engine assembly for aircraft in which the coupling device comprises a fore aerodynamic structure having a cradle equipped with an aerodynamic cowling, the cradle being...
US20110259998 CONFIGURATION OF A REAR FUSELAGE TAIL CONE OF AN AIRCRAFT WITH AN AUXILIARY POWER UNIT  
Configuration of a rear fuselage tail cone of an aircraft with an auxiliary power unit, whereby a fire compartment of the rear fuselage tail cone defines a housing for the auxiliary power unit in...
US20130227963 ASSEMBLY FOR ATTACHING THE HANGERS FROM WHICH AN AIRCRAFT PROPULSION UNIT IS SUSPENDED  
An assembly is designed to attach hangers from which an aircraft propulsion unit is suspended. The propulsion unit is intended to be suspended from a structural element of the aircraft. The...
US20120080554 AIRCRAFT ENGINE ATTACHMENT PYLON COMPRISING TWO FRONT WING SYSTEM ATTACHMENTS WITH ORTHOGONAL SHEARING PINS  
The present invention relates to an aircraft assembly (200) comprising a wing (2) and an engine attachment pylon (4) fixed to the wing by means of attachment means comprising a first and a second...
US20140151497 ENGINE PYLON FOR AN AIRCRAFT  
An engine pylon for attaching an engine to an aircraft, where the engine pylon includes a monolithic support structure having a body that includes multiple spaced bulkheads, multiple longerons...
US20100314491 AIRCRAFT ENGINE PYLON ATTACHMENT  
An aircraft engine mounting structure comprising a pylon box having an upper surface and at least one attachment element configured to be attached to a front spar of an aircraft wing box, the...
US20140252159 ENGINE INSTALLATION  
A fuselage mounted gas turbine engine installation the installation includes at least one propeller stage and a gas turbine core arranged in use to drive the propeller stage. The core is external...
US20150175272 REINFORCED PRIMARY STRUCTURE FOR AN ATTACHMENT PYLON  
The disclosure herein relates to a structural element for an aircraft comprising a portion of an attachment pylon primary structure. According to the disclosure herein, the attachment pylon...
US20150184544 Fan cowl locking system  
A locking system comprising a handle mounted such that it can rotate about an operating spindle, wherein the handle can move between a locked position and an unlocked position, a hook mounted on...
US20150184543 Fan cowl locking system  
A locking system comprising a handle mounted such that it can rotate about an operating spindle, wherein the handle can move between a locked position and an unlocked position, a hook mounted on...
US20120138736 AIRPLANE WITH A TAILCOAT TAIL ASSEMBLY AND REAR ENGINE  
An airplane, including a fuselage having an elongate shape along a longitudinal axis of the airplane, and at least one wing attached to the fuselage between front and back ends of the fuselage and...
US20140369810 ASSEMBLY FOR MOUNTING A TURBINE ENGINE TO A PYLON  
An assembly is provided for mounting a turbofan engine to a pylon. The turbofan engine includes a fan section and an engine core. The mounting assembly includes a fan case, a first mount and a...
US20110168836 AIRCRAFT ENGINE SUPPORTING PYLON  
Pylon (19) attached to an aircraft fuselage part (17) having a close transversal section of a curved shape comprising a skin (31) and a plurality of frames (33); its structural configuration...
US20110174919 STRUT DESIGNED TO SUPPORT AN AIRCRAFT TURBOJET ENGINE, AND NACELLE COMPRISING SUCH A STRUT  
This strut (9), designed to support an aircraft turbojet engine, has, on the one hand, a connecting part (11) for connection between the casing (1) of the fan (3) or the casing of the gas...
US20130092789 HYBRID DRIVE FOR HELICOPTERS  
The rotors of a helicopter are powered by electric motors. The electrical energy required for this purpose is produced by a motor-generator unit, which comprises one or more internal combustion...
US20110309188 RIGID AIRCRAFT PYLON STRUCTURE IN CONTACT WITH A FUSELAGE LATERAL EXTENSION FOR ATTACHMENT  
An aft part of an aircraft, including at least one engine assembly including a turbine engine and a turbine engine mounting pylon. A rigid structure of the mounting pylon includes a longitudinal...
US20120006936 ENGINE ASSEMBLY FOR AIRCRAFT INCLUDING A MODULAR RIGID STRUCTURE FOR MOUNTING PYLONS  
An aircraft engine assembly including a mounting pylon including a rigid structure fitted with a central box, together with a forward extension and a rear extension each including an attached...
US20120234970 AIRCRAFT ENGINE ATTACHMENT PYLON  
The invention relates to an aircraft engine attachment pylon, comprising a box formed by the assembly of a first spar (18), a second spar (20) and two lateral panels (22), the pylon also...
US20150259074 AIRCRAFT ASSEMBLY COMPRISING A MOUNTING STRUT BUILT INTO THE NACELLE AND ARRANGED AT THE REAR SECTION OF THE FUSELAGE  
In order to reduce engine deformation, the subject matter disclosed herein provides an assembly for an aircraft, comprising an aircraft rear section, an engine, a nacelle, and a mounting strut for...
US20110036942 ENGINE ATTACHMENT PYLON COMPRISING MEANS OF FASTENING SPARS AND PANELS LOCATED OUTSIDE THE INNER SPACE IN THE BOX  
An engine attachment pylon for an aircraft including a rigid structure including a box including an upper spar and a lower spar, connected to each other through two lateral panels. At least one of...
US20120241555 SUPPORT BLOCK FOR A MOTOR OF A ROTARY WING DRONE  
The support block (130) of each motor of the drone comprises: a support part (131) onto which are fastened an electric motor (120) for driving a propulsion group (100) of the drone, and at least...
US20140339357 SYSTEM AND METHOD FOR COOLING AN AIRCRAFT WING  
An aircraft comprises a turbine engine suspended from a wing by means of a pylon. Compressed hot air is bled off from the turbine engine. A bleed air duct in the wing conveys the compressed hot...
US20150144732 AERODYNAMIC FAIRING DIVIDED INTO SUB-PORTIONS  
An aerodynamic fairing including at least one sub-assembly, each sub-assembly having a frame which is orientated transversely relative to the longitudinal axis of the fairing and a floor portion...
US20130320135 AFT AERODYNAMIC FAIRING WITH IMPROVED THERMAL RESISTANCE FOR A PYLON FOR ATTACHING AN AIRCRAFT PROPELLING ASSEMBLY  
An aft aerodynamic fairing for a pylon for attaching an aircraft propelling assembly, including a caisson structure, a heat-shield floor, as well as a support structure for this floor comprising...
US20120111996 ASSEMBLY FOR AN AIRCRAFT COMPRISING A TURBOMACHINE ATTACHMENT STRUT OF WHICH THE MEANS FOR ATTACHMENT TO THE WING ARE ARRANGED IN A T SHAPE  
An assembly for an aircraft including: a mechanism attaching a primary structure of an attachment strut to a wing, forming an isostatic system; an attachment housed in a leading edge of the wing...
US20120273610 ENGINE PYLON COMPRISING A VORTEX GENERATOR, AND METHOD FOR THE PRODUCTION THEREOF  
The invention relates to a method for manufacturing an engine pylon (7) to be mounted between an engine (1) and an aircraft wing (6), said method comprising: mounting a pylon box (8) around a main...
US20150166188 FRONT INSTALLATION NODE INTEGRATED WITH AIRCRAFT PYLON  
A front installation node is suitable for integral forming with a front end frame of an aircraft pylon and includes a first lug and a second lug, each respectively protruding outwardly from one of...
US20110168837 AIRCRAFT PROPULSION SYSTEM  
An aircraft propulsion system including a bypass turbojet engine surrounded by a nacelle together with a mechanism attaching the engine to a pylon of an aircraft. The nacelle includes an inner...
US20120012694 FAIL-SAFE AIRCRAFT ENGINE MOUNTING APPARATUS  
A mounting apparatus for an aircraft engine that provides load path redundancy includes a forward mount that attaches the aircraft engine to a pylon at a forward position of the aircraft engine,...
US20110315814 ASSEMBLY COMPRISING A GAS TURBINE ENGINE AND A SUPPORTING PYLON  
A gas turbine engine 2 is supported on an aircraft fuselage by a pylon 10 which carries a mounting ring 6. The mounting ring 6 is releasably coupled to an engine ring 8 on the casing of the engine...
US20120056033 PYLON FOR ATTACHING AN AIRCRAFT TURBINE ENGINE COMPRISING ALIGNED FRONT WING TIES  
The invention relates to a pylon for attaching a turbine engine for an aircraft, having a rigid structure (10) and means for attaching the pylon on a wing of the aircraft, said means for attaching...
US20150197341 ASSEMBLY FOR AN AIRCRAFT, COMPRISING AN ENGINE ATTACHMENT BODY EQUIPPED WITH AT LEAST ONE SHACKLE SUPPORT FITTING THAT PASSES INTO THE BOX SECTION OF THE ATTACHMENT PYLON  
In order to allow better introduction of forces into the box section of an aircraft engine attachment pylon, the subject matter herein discloses a pylon including a primary structure forming a box...
US20140054413 AIRPLANE HAVING A REAR PROPULSION SYSTEM  
An aeroplane comprising a fuselage elongated in a longitudinal direction of the aeroplane is provided. The aeroplane includes a wing attached to the fuselage in a midsection of said fuselage in...

Matches 1 - 50 out of 345 1 2 3 4 5 6 7 >