Matches 1 - 30 out of 30


Match Document Document Title
US20130009004 INTERNAL GAS TURBINE PROPULSION THRUST REVERSER  
A thrust reverser for a gas turbine engine includes a hinge, a propulsion system duct, and a kicker blocker. Bypass air and gas path air travel through the propulsion system duct and the...
US20130206902 POWER SUPPLY CIRCUIT FOR AN AIRCRAFT DE-ICING SYSTEM  
An aircraft electrical supply circuit including: a power distribution network, onboard the aircraft, for electrical devices located in an engine of the aircraft or near the engine; and a power...
US20110101159 NESTED FAIRING THRUST REVERSER  
A thrust reverser nozzle for a gas turbine engine nacelle includes opposite and asymmetrically pivoting first and second doors defining a nacelle aft section, first and second trailing edges of...
US20120256051 STUB FRAME FOR A CASCADE THRUST REVERSER STRUCTURE  
The invention relates to a stub frame (121) for a cascade thrust reverser structure of a nacelle (101) of an aircraft, said stub frame (121) being intended for being fastened to one or more...
US20050001095 Self-aligning thrust reverser system lock assembly  
A lock assembly for a thrust reverser system that prevents thrust reverser movement, in either the deploy or stow directions, includes a lock bar and a lock that are configured to be self-aligning...
US20120181388 Unmanned Aerial Vehicle Drag Augmentation by Reverse Propeller Rotation  
An air vehicle configured to augment effective drag to change the rate of descent of the air vehicle in flight via propeller shaft rotation direction reversal, i.e., thrust reversal.
US20110108665 METHOD AND DEVICE FOR IMPLEMENTING THE THRUST REVERSERS OF AN AIRCRAFT  
Method and device for implementing the thrust reversers of an aircraft. According to the invention, the following successive steps are carried out automatically: deployment (E3) of the previously...
US20090313969 Thrust Reverser for a Turbofan Gas Turbine Engine  
The thrust reverser comprises sections, such as arms and skins, which may be connected along joints to provide a thrust reverser body. A plurality of fittings may be integrally formed on a surface...
US20090314887 THRUST REVERSER CASCADE ASSEMBLY AND AFT CASCADE RING WITH FLOW DEFLECTOR PORTION  
An aircraft engine thrust reverser cascade assembly includes a plurality of circumferentially spaced cascade segments, each cascade segment including a plurality of spaced vanes including an...
US20140252167 REVERSE CORE ENGINE THRUST REVERSER FOR UNDER WING  
A gas turbine engine for mounting under a wing of an aircraft has a propulsor that rotates on a first axis, and an engine core including a compressor section, a combustor section, and a turbine...
US20100270428 THRUST REVERSER ASSEMBLY WITH SHAPED DRAG LINKS  
A thrust reverser blocker door assembly for use in turbofan engines includes an engine nacelle with an aft translating cowl that is movable from a stowed position to a deployed position. An engine...
US20090321561 NACELLE FOR AIRCRAFT COMPRISING MEANS OF REVERSING THRUST AND AIRCRAFT COMPRISING AT LEAST ONE SUCH NACELLE  
Aircraft nacelle comprising a cowling and an engine, the cowling comprising a fixed portion and a mobile portion able to slide in order to define a radial opening with the mobile portion, a thrust...
US20130009005 REVERSE THRUST DEVICE  
The invention relates to a reverse thrust device including a stationary upstream structure including a front frame (30) and a cowl (40). Said cowl (40) is extended by a nozzle (41) with a variable...
US20140131515 AIRCRAFT TURBOJET ENGINE THRUST REVERSER WITH A REDUCED NUMBER OF LATCHES  
A thrust reverser with grids includes a jet engine pylon, a one piece cowl either directly or indirectly slidably mounted on the jet engine pylon between a direct jet position and a reverse jet...
US20100107599 THRUST REVERSER FOR A JET ENGINE  
The invention relates to a thrust reverser (9) for an aircraft nacelle (1), including: a front frame (11), a cowl (21) which can move between an operating position and an intermediate maintenance...
US20090121078 AIRCRAFT POD AND AIRCRAFT EQUIPPED WITH AT LEAST ONE SUCH POD  
A pod for an aircraft including a cowling, an engine housed in the inner volume of the cowling, an annular channel circulating a secondary thrust flow arranged between the engine and the cowling,...
US20060145001 Fan cowl door elimination  
A nacelle for housing an aircraft jet engine. The jet engine has a fan case and a portion disposed downstream of the fan case relative to a direction of airflow through the jet engine. The nacelle...
US20110101158 Thrust Reversers Including Monolithic Components  
Aircraft systems including thrust reversers with monolithic components are described herein. An aircraft system in accordance with one embodiment includes a thrust reverser having a fan duct inner...
US20090127391 Pivoting Fairings for a Thrust Reverser  
The thrust reverser is used with a gas turbine engine and includes first and second doors pivotable between a stowed position and a deployed position. When deployed, pivoting fairings on the first...
US20080105074 Bi-directional locking ring assembly for aircraft thrust reverser manual drive unit  
A bi-directional locking ring assembly is provided comprising a housing and a gear having a plurality of teeth. The gear is coupled to the housing to rotate in opposite directions about a...
US20080041184 Method For Fixing A Flexible Drive Shaft In A Thrust Reverser And A Thrust Reverser Of This Type  
The embodiments relate to a method for fixing a flexible drive shaft in a front frame of a thrust reverser, this front frame being realized with the aid of two partially open semicircular...
US20100193632 INTEGRAL COMPOSITE SLIDER FOR AIRCRAFTS  
A slider apparatus integral with a slidable member and a method for integrating the slider apparatus with the slidable member. The slider apparatus integrated with the slidable member may be...
US20110062279 HYBRID BEAM FOR A THRUST REVERSER UNIT  
Latch beams and hinge beams of an aircraft thrust reverser and a method for manufacturing the beams. The latch and hinge beams may comprise a plurality of hollow composite tubes joined with a...
US20130146708 CASE ASSEMBLIES WITH COMMON CONTROLS  
A case assembly for an aircraft is provided. The assembly includes a thrust reverser actuation system (TRAS) configured to provide braking assistance to the aircraft; a variable area fan nozzle...
US20120056038 Mechanism for Changing the Shape of a Control Surface  
An apparatus comprises a structure having a first side, a second side substantially opposite to the first side, a flexible skin, and a plurality of deformable assemblies. The flexible skin is...
US20170101962 VIBRATION DAMPING DRAG LINK FITTING FOR A THRUST REVERSER  
A nacelle drag-link assembly for a thrust reverser of a propulsion system includes a drag-link fitting, a drag link, a coupling assembly, and a vibration damping assembly. The drag-link fitting...
US20150298814 CLOCKED THRUST REVERSERS  
An aircraft includes a fuselage including a propulsion system supported within an aft portion. A thrust reverser is mounted proximate to the propulsion system for directing thrust in a direction...
US20150298794 AIRCRAFT WITH FORWARD SWEEPING T-TAIL  
An aircraft includes a propulsor supported within an aft portion of the fuselage. A thrust reverser is supported proximate the propulsor for redirecting thrust forward to slow the aircraft upon...
US20150291289 ASYMMETRIC THRUST REVERSERS  
An aircraft includes a propulsion supported within an aft portion of a fuselage A thrust reverser is mounted in the aft portion of the fuselage proximate the propulsion system for directing thrust...
US20150275821 Engine Thrust Reverser Lock  
In some aspects, an aircraft engine thrust reverser lock system includes a pin-capturing member. The pin-capturing member includes a body that is rotatable about an axis defined by a pivot...

Matches 1 - 30 out of 30