|
Match
|
Document |
Document Title |
|
|
7618007 |
Force balancing actuator
There is provided a force balancing actuator for mounting a pressure vessel, containing an engine, to aircraft structure. The force balancing actuator includes a cylinder and piston that is...
|
|
|
7607609 |
Mounting device for an aircraft engine comprising two thrust recovery rods with a double rear mechanical connection
A mounting device for an aircraft engine includes a rigid structure and a device for mounting the engine on the rigid structure, the mounting device including a thrust load recovery device with two...
|
|
|
7594623 |
Torsionally de-coupled engine mount system
A torsionally de-coupled engine mount system ( 13 ) for use in tilt rotor aircraft ( 11 ) applications is disclosed, in which an engine is mounted at its forward end to a prop rotor gear box by...
|
|
|
7581694 |
Vertical tail unit for aircraft and aircraft equipped with same
A vertical tail unit for an aircraft and an aircraft equipped with the vertical tail unit. The vertical tail unit is provided with an engine. The engine extends cantilevered beyond a fin of the...
|
|
|
7566029 |
Suspension for suspending a jet engine on an aircraft strut
A suspension for suspending a jet engine on an aircraft strut includes a beam having a platform provided with fasteners for fastening the beam to the aircraft strut and arranged transversely with...
|
|
|
7549604 |
Fuel efficient fixed wing aircraft
A fixed wing aircraft having a fuselage having a forward end and a rearward end, the fuselage's forward end forming a nose section; the aircraft further having a primary thrust turbo-prop engine...
|
|
|
7540450 |
Aircraft propulsion system
An aircraft propulsion system comprises a power plant driving a number of outboard propulsion units to propel a fixed wing aircraft.
|
|
|
7527220 |
Aircraft engine mount
A mount for an aircraft engine arranged to be attached firstly by a beam to the aircraft, and secondly by lateral and a median load transmission elements to the engine, the mount having an...
|
|
|
7526921 |
Auxiliary power unit with integral firebox
An auxiliary power unit (APU) with integral firebox provides an integral unit for aircraft to utilize an APU without the use of a separate firebox. The present invention comprises a turbomachine...
|
|
|
7510147 |
Vibration damping pylon
The pylon of the present invention provides damping of vibrations transferred in both directions between the aircraft and the payload. That is, the pylon of the present invention damps the effects...
|
|
|
7496433 |
Method and apparatus for minimizing the noise emitted by a rotorcraft during take-off and landing
The method includes a preliminary period in which a reference rotorcraft is used that corresponds to a rotorcraft of a particular type, with a series of noise measurements being performed on said...
|
|
|
7461815 |
Suspension system for a rotary wing aircraft engine
The invention relates to a system for suspending an engine of a rotary wing aircraft. The technical field of the invention is that of manufacturing suspension devices for helicopter engines. The...
|
|
|
7451947 |
Engine mounting structure under an aircraft wing
This invention relates to a mounting structure ( 1 ) for mounting an engine ( 2 ) under an aircraft wing ( 4 ), the structure comprising a rigid structure ( 8 ) and means ( 10 ) of fastening this...
|
|
|
7448573 |
Engine suspension pylon for aircraft
The invention refers to a suspension pylon ( 4 ) for an aircraft engine ( 2 ), the pylon including a rigid structure ( 10 ) forming a box provided with a lower spar ( 28 ) and an upper spar ( 26 ),...
|
|
|
7445179 |
Engine assembly for aircraft
The invention relates to an engine suspension pylon for an aircraft including a rigid structure provided with a box ( 24 ), this pylon also including an engine aft attachment ( 8 ) provided with an...
|
|
|
7438262 |
Redundant gas turbine engine mounting arrangement
A gas turbine engine mounting arrangement for attaching a gas turbine engine to a support structure, such as a pylon of an aircraft, comprises a main mounting member adapted to interconnect the...
|
|
|
7431126 |
Support means for an acoustic liner used in an auxiliary power unit exhaust muffler
The present invention provides support means for an acoustic liner in an APU exhaust system, where the acoustic liner has a tubular sidewall with an outer surface, a first longitudinal edge, a...
|
|
|
7419121 |
Integrated mount duct for use with airborne auxiliary power units and other turbomachines
An integrated mount duct includes a load ring for mounting a turbomachine to a flight vehicle, wherein the load ring has a cylindrical shape with a flange edge and a stepped edge, and comprises one...
|
|
|
7398945 |
Cast unitized primary truss structure and method
A truss structure well suited for use as an engine strut on a commercial aircraft. The truss structure is cast as a single piece integrally formed component from a titanium alloy or another...
|
|
|
7341225 |
Aircraft wing and aeroengine arrangement for attenuating engine noise
An aircraft comprising an aeroengine and a noise reflective surface, the aeroengine capable of generating a hot exhaust jet and noise characterized in that the reflective surface is profiled to...
|
|
|
7325770 |
Mounting of engine onto an aircraft structure
The invention pertains to an engine mount onto an aircraft structure comprising at least one connection means between a first and a second element such as an engine case and said structure,...
|
|
|
7318565 |
Electric motor assisted takeoff device for an air vehicle
A takeoff assist device for an air vehicle, such as an unmanned air vehicle is provided. The device features an electric motor and is much less complex and lighter than takeoff assist devices...
|
|
|
RE39972 |
Detachable integral aircraft tailcone and power assembly
The present invention provides a tailcone and power assembly mountable to the body of an aircraft using a height adjustable dolly. The tailcone assembly comprises a longitudinal support member, a...
|
|
|
7296768 |
Structure for mounting a turboprop under an aircraft wing
A structure for mounting a turboprop under an aircraft wing includes a rigid structure and a device for fastening the turboprop on the rigid structure. The rigid structure is composed of a box, and...
|
|
|
7267301 |
Aircraft engine with means of suspension from the structure of an aircraft
An aircraft engine includes a mounting attached to an aircraft structure and transmitting forces between an engine casing and the aircraft structure. The mounting includes a fail safe assembly with...
|
|
|
7240877 |
Multi-engined aircraft with lowering shaft
A multi-engine aircraft having one engine positioned at the tail of the fuselage may include rear tail units in a vertical longitudinal plane-of-symmetry of the fuselage. The tail engine is...
|
|
|
7232091 |
Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft
This invention relates to a mounting system ( 100 ) inserted between an aircraft engine ( 2 ) and a rigid structure ( 4 ) of an attachment strut ( 6 ) fixed under a wing ( 8 ) of this aircraft, the...
|
|
|
7198224 |
Energy absorbing airframe for a vertical lift vehicle
An airframe includes an energy absorbing structure with a frame, a beam mounted to the frame at a rotational joint and a collapsible member. In response to reaching a predetermined threshold load...
|
|
|
7165743 |
Front fastening device for aircraft engine
A front attachment device for attaching an aircraft engine to an aircraft pylon includes an upper brace fitted with elements rigidly fastened to the pylon and first and a second connecting rods,...
|
|
|
7159819 |
Mounting structure for mounting a turboprop under an aircraft wing
A mounting structure for mounting a turboprop under an aircraft wing includes a rigid structure provided with an aft underwing box, and at least one forward rigid section. Each forward rigid...
|
|
|
7150432 |
Horizontal augmented thrust system and method for creating augmented thrust
A horizontal augmented thrust system includes at least one wing. The wing includes a wing outer envelope, a trailing edge and a flap. At least one pulse jet engine is positioned entirely within the...
|
|
|
7121512 |
Drain particularly for engine support strut
A drain, for example for an aircraft engine support strut, arranged on the trailing edge of the rear secondary structure of the strut. The drain includes a conduit with a substantially horizontal...
|
|
|
7121504 |
Hanging device to connect an engine to an aircraft wing
The invention relates to a hanging device ( 1 ) connecting an engine ( 2 ) to a wing ( 4 ) of an aircraft, with the device being made up of a rigid structure ( 8 ) and hanging equipment ( 10 )...
|
|
|
7108224 |
Aircraft engine rear suspension with thrust recovery
A suspension of the turbo fan engine to an aircraft pylon, includes a fitting arranged to be attached to a pylon, a lever fastened in its central portion to the fitting via a linking device with a...
|
|
|
7104306 |
Cast unitized primary truss structure and method
A truss structure well suited for use as an engine strut on a commercial aircraft. The truss structure is cast as a single piece integrally formed component from a titanium alloy or another...
|
|
|
7103952 |
Engine loader and transporter apparatus and methods
Engine loader and transporter apparatus and methods are disclosed. In one embodiment, an engine handling assembly includes a motorized drive assembly engageable with a floor surface, and an...
|
|
|
7100869 |
Turboprop carrier structure and an assembly including such a carrier structure
The carrier structure of the invention is used for carrying a turboprop and it is designed to be mounted beneath and/or in front of an airplane wing. In characteristic manner, the carrier structure...
|
|
|
7093794 |
Aircraft and detonative engine incorporating pulse detonation engines
An aircraft includes at least one airfoil having a leading edge and a trailing edge. A number of pulse detonation engines are distributed along one of the leading and trailing edges of the airfoil...
|
|
|
7090165 |
Aeroengine nacelle
A nacelle ( 55 ) for a gas turbine engine ( 10 ), the engine ( 10 ) comprising accessories ( 34 ) mounted to a fan casing ( 28 ) and a core engine ( 9 ), the nacelle ( 55 ) substantially surrounds...
|
|
|
7083144 |
Apparatus and methods for support of propulsion systems interconnect members
An apparatus for supporting an aircraft system interconnect member between a strut and an engine of the aircraft. The apparatus includes a disconnect panel near the engine through which the...
|
|
|
7083143 |
Apparatuses and methods for attaching engines and other structures to aircraft wings
Apparatuses and methods for attaching jet engines and other external structures to aircraft wings are disclosed herein. In one embodiment, an aircraft system includes a wing and a unitary fitting...
|
|
|
7073750 |
Propulsion system for model airplane
An improved structure and method for powering the flight of a model airplane by positioning the motors and propellers on the back side of the top wings of an airplane using a single or double-deck...
|
|
|
7021585 |
Aircraft engine rear mount with thrust links and boomerang-shaped lever
A turbine engine mount to a pylon of an aircraft includes a bracket arranged to be attached to the pylon, and a lever attached in its central part to the bracket via a first connection and two...
|
|
|
7017858 |
Two-tone isolator assembly
The invention proposes to address the vibration transfer function transmitted by a turbo-fan engine or equivalent to the aircraft structure, with two types of isolators mounted on a unique assembly...
|
|
|
7011275 |
Internal spur gear drive
An internal spur gear drive has a mounting base including one or more sets of motor mounting lugs extending therefrom, for attaching a corresponding number of drive motors thereto. A drive shaft...
|
|
|
7007890 |
Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position
The turbojet according to the invention is designed to be fixed onto the upper part of the aft section of the fuselage of an aircraft using at least one coat hanger, the turbojet comprising a fan,...
|
|
|
6988692 |
Rear fastening device for aircraft engine
A rear attachment suspension or device of a turbo engine to an aircraft pylon includes an upper brace fitted with a pylon fastening device and hinged by second ball joint connections, first and...
|
|
|
6986482 |
Suspension part of a turbojet engine
A suspension part for mounting a turbojet engine includes two ends equipped with two elements, juxtaposed in a widthwise direction of the suspension part, for fixing the suspension part to the...
|
|
|
6983912 |
Hybrid exhaust heat shield for pylon mounted gas turbine engines
The present invention is a hybrid engine exhaust heat shield assembly that includes a plurality of sections. The plurality of sections include one or more sections formed of titanium (or other high...
|
|
|
6976655 |
Mounting arrangement
A mounting arrangement ( 26 ) is provided for mounting an engine ( 10 ), typically a gas turbine engine, to a vehicle. The mounting arrangement ( 26 ) includes connecting means ( 28, 30 )...
|