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US20150191243 Airframe Stabilization Mechanism for Vertical Takeoff and Landing Transport Plane  
A vertical takeoff and landing transport plane is characterized in that a structure formed in the top-bottom direction of an airframe penetrates a rear structure of the vertical takeoff and...
US20150136907 Deployable barrier arrangement for selectively blocking a passage in an aircraft cabin  
A deployable barrier arrangement for selectively blocking a passage in an aircraft cabin, wherein the barrier arrangement comprises a substantially longitudinal barrier member and a joint unit for...
US20140353428 AIRCRAFT DOOR AND AIRCRAFT COMPRISING THE SAME  
An aircraft door 18 which closes an opening of a storage space 16 for storing a RAT 13 as an accessory and which is opened in association with deployment of the RAT 13 from the storage space 16,...
US20120251092 Articulated Sensor Support Structure  
Embodiments include an assembly comprising: (a) a camera support structure comprising: a masthead disposed on the distal end of a mast wherein the masthead is configured to receive an imaging...
US20120193474 Window Mounted Raft System  
An inflatable life raft system for an aircraft includes a window coupled to a fuselage portion of the aircraft. A mechanism is used to selectively detach the window from the fuselage. An...
US20110297787 DUAL FUNCTION DOOR FOR AN AIRCRAFT ENGINE NACELLE  
The invention relates to a door (20) for an aircraft engine nacelle (6), comprising an opening leaf (22), locking means (32, 36) with which the opening leaf may be locked in the closed position,...
US20120025021 PAYLOAD DOOR AND ELEVATOR SYSTEM  
A payload door and elevator system for the translation of a payload such as a camera, from a stowed position within an aircraft fuselage to a deployed position projecting through an aperture...
US20130059518 METHOD AND SYSTEM FOR CONTROLLING AN AIRCRAFT COMPONENT DURING A WATER LANDING  
The invention relates to a system (10) for controlling a water landing of an aircraft comprising at least one detection device (12, 14, 16, 18), which is adapted to detect at least one signal...
US20120160961 System for overhead storage of cargo containers in upper lobe of aircraft  
A cargo storage and handling system for aircraft. A rack assembly mounts in an upper portion of the fuselage to form a cargo area in the upper lobe thereof. The rack includes a series of frames...
US20110290941 Attachment system of aircraft components  
An attachment system for attaching a component (11) such as a vertical tail plane to a fuselage (27) of an aircraft; the component (11) being structured as a box comprising front and rear spars...
US20130020439 SEPARATING ELEMENT FOR A PLATFORM CABIN COMPRISING A PUSH ROD MECHANISM FOR MOVING A LEAF  
The separating element (10) according to the invention for a platform cabin comprises: at least one stationary partition (12), delimiting a passage (14) defining a circulation axis (C) inside the...
US20100006701 DEVICE FOR AN AIRCRAFT POWER UNIT  
Device (3) for providing a warning signal when the fan cowl doors (8, 9) of an aircraft are not properly latched by primary locking means (6), said device (3) comprising a panel (4) the panel (4)...
US20090159748 Decompression Device With Adjustable Release Pressure  
The invention relates to a decompression element for pressure equalisation in a cabin of an aircraft, with a decompression element frame (4), a flap (2) and a hinge element or at least one bearing...
US20070278348 APPARATUS FOR OPENING AIRFRAME OF MISSILE BY PYROTECHNICAL POWER  
Disclosed is an apparatus for opening an upper and lower split-type airframe hinge-coupled to a propulsion unit of a missile and separating a payload mounted in the airframe. The apparatus for...
US20080277529 Nacelle Cowling for Turbojet and Nacelle Comprising at Least One Such Cowling  
A nacelle cowling for a turbojet, characterized in that it is provided with a fixed part and a mobile part, the mobile part being adapted to slide along the fixed part, from a closed position...
US20100096503 OUTFLOW VALVE HAVING J-SHAPED BELLMOUTH AND CABIN PRESSURE CONTROL SYSTEM EMPLOYING THE SAME  
An outflow valve is provided for use in conjunction with an actuator. In one embodiment, the outflow valve includes a frame and a first door rotatably coupled to the frame. The outflow valve is...
US20090179110 Extended Decompression Flap Arrangement  
The invention concerns an apparatus for producing a rapid air pressure equalisation between regions of an aircraft fuselage which are separated from each other by an aircraft fuselage structure...
US20090057490 Deceleration device for a cockpit door for decelerating in case of decompression  
A deceleration device for a movable component in an aircraft, the device having a deformation component, wherein the deformation component includes a deformation tool, a deformation body with a...
US20080023584 HINGE DEVICE OF A NACELLE COWLING OF AN AIRCRAFT ENGINE ON A SUPPORTING STRUCTURE  
This invention relates to a hinge device (20) of a nacelle cowling of an aircraft engine (6) on a supporting structure, including two fittings as well as a link rod (34) connected thereto and...
US20090014590 HATCH EQUIPPED WITH AT LEAST ONE LOCKING SOCKET CAPABLE OF BEING ACTUATED ON EACH SIDE OF THE HATCH  
The present invention relates to a hatch (1) provided with at least one locking socket, equipped with first actuation means (108) making it possible to urge a flexible linear pulling member (104),...
US20150108274 DECOMPRESSION PANEL ASSEMBLY AND METHOD OF EQUALIZING AIR PRESSURE DIFFERENTIAL  
Decompression panel assemblies and methods of equalizing air pressure differential are provided. The decompression panel assembly includes a panel comprising an opening defined therein, a vent...
US20090166473 Optimized aircraft manhole  
The present invention relates to an aircraft manhole comprising a skin panel (1) of the aircraft structure, an outer door (6) and an inner door (5) of the aircraft manhole being positioned on the...
US20090173823 Method and component for determining load on a latch assembly  
A cowl assembly for an engine nacelle including a first and second cowl door mounted for movement between an open position and a closed position. A latch assembly retains the first and second cowl...
US20120280081 APPARATUS FOR FACILITATING ACCESS TO A NACELLE INTERIOR  
A nacelle for housing an engine includes a fan cowl sized to cover at least a first axial portion of the engine. The engine includes an inlet end, an exhaust end, and an axis extending through the...
US20090242702 METHODS AND APPARATUS FOR OPTICAL PROPAGATION IMPROVEMENT SYSTEM  
An aircraft turret and fairing assembly for facilitating transmission of a directed energy beam from a directed energy device includes a turret section for directing an energy beam. The assembly...
US20090294591 Cover for an aircraft access opening  
The invention relates to a cover for the access opening in a composite material aircraft structure, characterized in that it comprises the following elements: an outer cover (18) arranged on the...
US20110133034 AIRCRAFT NACELLE INCORPORATING A DEVICE FOR PROTECTING AN ACCESS FLAP FOR A LOCKING SYSTEM  
An aircraft includes a part defining an aerodynamic surface against which flows an air stream, with at least one hood able to block an opening made at the aerodynamic surface, kept in the closed...
US20120280082 APPARATUS FOR FACILITATING ACCESS TO A NACELLE INTERIOR AND METHOD OF ASSEMBLING THE SAME  
A nacelle for housing an engine includes a fan cowl sized to cover at least a first axial portion of the engine. The engine includes an inlet end, an exhaust end, and an axis extending through the...
US20090121073 Aircraft having a jet engine, an adjustable aft nozzle, and an electric vertical fan  
An adjustable nozzle is mounted on the airframe downstream from the powerplant for selectively directing powerplant exhaust to exit the aircraft at an angle between about rearward and downward. An...
US20100243809 OPENING PLUG AND METHOD OF INSTALLING THE SAME  
A device is used to plug an opening in a structure having a front side and a back side. The device includes a removable plug body for plugging the opening, and a retainer that is expandable into...
US20090152397 SELECTIVE RELEASE LATCH  
A selectively released latch securing a panel in position, but which resists release in response to sudden movement of the panel, yet allowing release in response to a slow and steady movement of...
US20070145189 Opening and secure-closing system for doors  
Opening and secure-closing system for doors comprising two doors (1,2) for accessing the interior of a chamber, which open towards the outside being hinged around two hinging axes (19,20), both...
US20120267471 MISSILE NOSE FAIRING SYSTEM  
A missile nose fairing system includes sections attached at an aft end thereof to a missile body, a restraint for normally preventing aftward displacement of the plurality of sections, and a drive...
US20130056584 METHOD FOR MOUNTING AN AIRCRAFT COMPONENT AND AIRCRAFT ASSEMBLY  
A method for mounting an aircraft component, which in the mounted state is movable between a first and a second operating position and is taken up in its first operating position in a mounting...
US20120097794 AIRCRAFT PANEL COMPRISING AN OPENING EQUIPPED WITH A SURROUND  
The subject of the invention is an aircraft panel, notably a fuselage panel of the aircraft, comprising at least one opening equipped with a surround intended to accept a closing-off device that...
US20100187358 DECOMPRESSION DEVICE FOR AN AIRCRAFT  
The invention relates to a cover panel for an aircraft, comprising a decompression opening that can be closed by a decompression flap that comprises a membrane, and a ventilation opening that is...
US20100096504 STRUCTURAL ELEMENT FOR COVERING AN ELONGATE GAP ON AN AERODYNAMIC SURFACE OF AN AIRCRAFT  
A covering structural element is adapted to close an elongate gap provided on an aerodynamic surface of an aircraft. Such an element has a strip-shaped body made of metal material, including a...
US20090308976 Cover panel for an aircraft, more particularly a landing gear cover panel for a cargo plane  
The invention relates to a cover panel for a landing gear for an aircraft with at least one pivotal closable flap 6, 7. According to the invention the at least one flap 6, 7 is attached for swivel...
US20120325967 CLOSING MEMBER FOR OPENING  
An object of the invention is to provide a low-cost closing member for an opening having an excellent lightning protection capability. A door body 30, a clamp ring 40 made of a composite material,...
US20130015294 CLOSING MEMBER FOR OPENING  
An object of the invention is to provide a low-cost closing member for an opening having an excellent lightning protection capability. In a door body 30, an outer surface 31a of a plate part 31 is...
US20170183076 DOOR SYSTEM FOR AN EXHAUST GAS DUCT OF AN AUXILIARY POWER UNIT OF AN AIRCRAFT  
A door system configured to be attached to the fuselage of a tail cone of an aircraft wherein the tail cone comprises an exhaust gas duct of an auxiliary power unit of the aircraft and an opening...
US20170144744 DECOMPRESSION ASSEMBLY WITH TWO DECOMPRESSION OPENINGS  
An aircraft decompression assembly, comprising a cabin lining element, an element opening and an air channel adjacent to an element rear face and connected to the opening. A channel outlet, during...
US20170008608 SELF-ADJUSTING DOOR JAMB FOR AN AIRCRAFT DOOR  
The disclosed embodiments relate to an aircraft having an interior door with a self-adjusting door jamb. The self-adjusting door jamb includes a door jamb configured to receive the interior door...
US20160236764 MAGNETIC LATCHING SYSTEM WITH INFLATABLE SEAL  
A magnetic latching system is provided for removably latching a panel to an aircraft surface portion. The latching system includes a removable axis panel engageable to a latching land. The panel...
US20160230433 DEVICE FOR OPERATING AT LEAST ONE AIRCRAFT DOOR COMPRISING A CONTROL HANDLE  
An operating device for operating at least one door of an aircraft comprises a chassis that is fixed and secured to a fuselage of the aircraft, a control handle that is rotationally and...
US20160201371 QUICK RELEASE HINGE  
Aspects of the disclosure are directed to a system configured for installing or removing a door from an aircraft, the system comprising: a pin, a hinge comprising a slot that forms a cavity for...
US20160176496 DOOR FOR CLOSING OPENING IN STRUCTURE AND AIRCRAFT  
The present invention relates to a door for closing an opening in a structure, including: a body arranged to be capable of abutting against a first side of the opening; at least one clamping...
US20160130007 WINDOW MOUNTED RAFT SYSTEM  
An inflatable life raft system for an aircraft includes a window coupled to a fuselage portion of the aircraft. A mechanism is used to selectively detach the window from the fuselage. An...
US20160121992 SHUTTER MECHANISM FOR COVERING A WING DEPLOYMENT OPENING  
A shutter mechanism for covering a wing's spreading opening formed in an airborne body and a method for covering such opening while implementing the shutter mechanism, wherein the shutter...
US20150353203 ACOUSTICALLY DIFFUSIVE AUXILARY POWER UNIT INLET DOORS  
An inlet door for an auxiliary power unit includes a door body with opposed interior and exterior surfaces. The interior surface of the inlet door is curved to diffuse sound waves received by the...
Matches 1 - 50 out of 52 1 2 >