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WO/2013/006210 |
Data recording systems (100) and methods (400) for synchronizing data of a plurality of different data types on a single packet (300). The methods involve: receiving the data and an audio frame containing voice data and timing data commu...
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WO/2013/006072 |
The present invention is an improvement to waterborne platforms that are used to anchor aerial and airborne systems deployed over water. The system basically consists of a fully submerged main body (1), which is immersed in a body of wat...
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WO/2013/003540 |
Described are retractable armrest systems (100) including a receptacle (102), a support bar (104) comprising a first end (114) and a second end (116), wherein the first end is coupled to the receptacle, and an armrest (106) coupled to th...
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WO/2013/000577 |
The invention pertains to an airfoil (10) with a main wing (12), with at least one high-lift body (14) that is arranged on the leading edge of the main wing (10) such that it can be moved between an initial adjusting position and a maxim...
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WO/2013/002784 |
A rotor hub has a yoke with radial arms allowing flapping of connected blades about a flap axis. A grip is rigidly attached to each blade, and a lead-lag bearing connects each grip to one of the arms, the bearing defining a lead-lag axis...
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WO/2013/002862 |
. A submerged ram air turbine generating system (10) adapted for use in a pod (12) mounted to the wing of an aircraft comprises a sub¬ merged inlet (26) extending substantially entirely around the outer surface of the pod housing (14), ...
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WO/2013/000447 |
The invention relates to a connection arrangement (30b) for connecting two profiled elements (32, 34) in a seamless and aerodynamically smooth manner in order to form a profiled surface around which a laminar flow is possible. A first pr...
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WO/2013/002862 |
A submerged ram air turbine generating system adapted for use in a pod mounted to the wing of an aircraft comprises a submerged inlet extending substantially entirely around the outer surface of the pod housing, a stator in the form of a...
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WO/2013/003099 |
Vibration - damping blankets (36) are attached to the back surfaces of fairing panels (12) of a flight vehicle (e.g., an aircraft or spacecraft) to reduce vibration, fatigue, structure and airborne transmitted energy, and cabin noise. In...
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WO/2013/002874 |
An actuator assembly (10) may comprise a housing (12), a shaft (62), a shape memory alloy (SMA) torque tube (18), and first and second unidirectional bearings (32,36). The SMA torque tube (18) may rotate the shaft (62). The first unidire...
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WO/2013/000035 |
A method of controlling operation of an unmanned aerial vehicle having a flight control system (110) comprising: a flight controller (300) for implementing a flight control strategy; and an engine control unit (117) interfaced with said ...
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WO/2013/001224 |
The invention is aimed at effecting rapid, simple protective dome opening, allowing accessibility to the device to be protected (radar and other communication systems, etc.). Accordingly, the invention makes provision for a unique kinema...
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WO/2013/003537 |
Described are multipurpose tray table systems including a passenger seat back (102), at least one tray table arm (104) pivotally coupled to the passenger seat back, and a tray table (106) pivotally coupled to the at least one tray table ...
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WO/2013/002383 |
A vertical takeoff and landing aircraft having: a propeller (2) having a fan (21) for generating lift and thrust; a motor (3) for supplying power to the propeller (2); a frame (4) for coupling the propeller (2) and the motor (3); a seat ...
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WO/2013/000036 |
An air cooling system for an unmanned aerial vehicle including a propeller (14) driven by an engine (12) has at least one cooling air duct (22) to direct cooling air to cool a vehicle component e.g. a cylinder head. The duct has at least...
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WO/2013/002673 |
The invention relates to engine systems for spacecraft with a solar sail and can be used when maneuvering the spacecraft with the solar sail for improved control of the thrust of said spacecraft. The result consists in the possibility of...
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WO/2012/175863 |
According to the invention, the blade (11), intended to be mounted on the hub (12, 13) of a turbomachine propeller so that an empty space (18, 18A, 18B) is defined between the base (14A) of the blade (14) and the face of the hub (12, 13)...
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WO/2012/175928 |
An aircraft wing assembly comprising a wing (2) having a wing box structure including an upper wing cover (7) and a lower wing cover (8), and a wing tip device (1) attached to the outboard end of the wing, the wing tip device including a...
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WO/2012/176132 |
The invention relates to a fluid supply bench (1), for example for an aircraft undergoing maintenance, said bench including: a fluid circuit (10) comprising a variable-displacement, constant-pressure pump (12), said circuit (10) being in...
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WO/2012/175843 |
The invention relates to a structure for mounting a power train having non-ducted propellers onto the fuselage of an aircraft, said mounting structure being connected via first and second means for attaching onto so-called front and rear...
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WO/2012/177785 |
An airdrop package (400) for fuel and water is disclosed. A plurality of hollow cylinders (408) are made of combustible firelog material. Closed water container nested within at least some of the plurality of hollow cylinders. The airdro...
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WO/2012/176223 |
A hooking member (1) for favouring landing of an aircraft on a access surface (G) comprising a support group (2) which protrudes from the support pads (P) of the aircraft to which is firmly coupled, a grip assembly (3), coupled to the su...
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WO/2012/176738 |
Provided is an armrest that can be produced at a low cost and with a lightweight structure, and is able to prevent pinching of clothes or fingers by means of a simple structure. A core plate (20) and a cover member (30) are integrally fo...
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WO/2012/175756 |
The device comprises at least one folding, inflatable chamber (3), at least one runner (4) for landing on water, which is coupled to the aircraft (2) by means of the chamber (3), and at least one air intake (6) connected to the chamber. ...
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WO/2012/177334 |
A rigid coupler (300) for use in electrically isolating an electrically conductive fluid conveyance system is described. The rigid coupler (300) includes a nonconductive liner (306) having a first end configured to couple to a first adjo...
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WO/2012/175619 |
The invention relates to a combined rescue beacon and flight recorder device (1) for an airplane, which is ejectable, buoyant and/or provided with flotation devices, which comprises a frame provided with at least one outer side surface h...
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WO/2012/178012 |
Disclosed is a restraint system for a vehicle, such as a wheeled vehicle, boat, or fixed or rotary winged aircraft. The system includes a control system integrated into the harness and strap of the restraint. This permits crewmembers to ...
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WO/2012/177258 |
A method and apparatus comprising a structure (330) and an extended portion (332) in the structure (330). The structure (330) is configured for connection to a hinge (328) for a door (308) in an aircraft (200). The extended portion (332)...
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WO/2012/174988 |
A vertical take-off and landing aircraft with tiltrotor power for use on land and in the air comprising: a body (3) equipped with a driving device, controlled wheels (8) for allowing the body to move on the ground, a front thruster (1) a...
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WO/2012/175187 |
The present invention relates to a rotary-wing drone (1) comprising a frame in which are located: - a set of sensors (13) designed for performing tasks of surveillance and/or intelligence gathering and/or assisting with the guidance of t...
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WO/2012/175953 |
Apparatus and a method performed by the apparatus, the apparatus being mounted on an unmanned vehicle (2) (e.g. an aircraft) and arranged to act upon a payload (18) (e.g. a weapon), the payload (18) being mounted on the unmanned vehicle ...
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WO/2012/175863 |
According to the invention, the blade (11), intended to be mounted on the hub (12, 13) of a turbomachine propeller so that an empty space (18, 18A, 18B) is defined between the base (14A) of the blade (14) and the face of the hub (12, 13)...
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WO/2012/178181 |
Apparatus and methods for eliminating back drive in a push pull type control system, are provided. An exemplary apparatus includes a control rod (31)including a pair of spaced apart piston displacement members (67,69) each configured to ...
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WO/2012/177352 |
Described herein is a novel method and apparatus for preventing spark propagation from a hydraulic joint (110) to a surrounding medium, such as a fuel source. The hydraulic joint (110) includes a fitting (112) and a tube (114, 116). A ti...
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WO/2012/173632 |
The self-sustaining drone aircraft freight and observation system (5) comprises a fleet of jet-powered drone aircraft (10) designed to carry freight (12) only. The drones (10) operate from a separate airfield in outlying areas to decreas...
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WO/2012/171589 |
A drive unit (16) for an aircraft running gear (2) having at least a first wheel (4) and a second wheel (6) on a common wheel axis (A), wherein the drive unit (16) is drivingly coupleable to at least one of the first and second wheels (4...
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WO/2012/172208 |
The invention relates to a method for mounting an aircraft engine (40) on a pylon (43), characterized in that it comprises the following steps: positioning at least a first shear pin (53) either in a first opening (51) provided in a fron...
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WO/2012/172238 |
The invention relates to the field of cryogenic propulsion and, in particular, to a cryogenic propulsion assembly (1), comprising at least: a reignitable main propulsion unit (6); a first cryogenic tank (2), connected to the main propuls...
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WO/2012/173542 |
The present invention regards a cover for covering a gap (2) between a first structural portion (3, 3 ') and a second structural portion (5, 5') of an aerial vehicle (29, 41 ), the cover (1, 25) comprises a first attachment section (9), ...
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WO/2012/173836 |
A flexible-usage travel suite (10) that includes an enclosure having a floor (12), surrounding walls (14) defining a predetermined area and an egress/ingress opening (16). A seat (20) is positioned adjacent a first side of the enclosure ...
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WO/2012/173651 |
An aircraft engine fuel system 900 is disclosed having a gas turbine engine 101, a turbocharger 910, a compressor bleed air system 930 for providing compressor air (A) from the gas turbine engine 101 to the turbocharger 910, and a fuel d...
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WO/2012/172320 |
The invention provides a computer-implemented method and corresponding system for conducting an inspection of an aircraft component, such as an aircraft engine. Reference data relating to the component is stored electronically in a datab...
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WO/2012/171520 |
The invention relates to a drive device for an aircraft (100), at least comprising a battery (101) for storing electrical energy, an electric motor (103) for driving a propeller (104), a conducting means (102) for transferring the electr...
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WO/2012/171105 |
The test cell comprises a test cell chamber comprising an air intake opening for allowing air to be fed into the test cell chamber. An aircraft engine test stand is mounted within the test cell chamber with the aircraft engine to be test...
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WO/2012/173594 |
A system and method to mitigate the effect of hydrodynamic ram. The system including a chamber adapted to receive fluid and a core disposed within the chamber. A plurality of columns extend through the core and a plurality of orifices ex...
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WO/2012/173593 |
A system and method to amplify displacement includes a housing forming a cylindrical chamber having an elastomeric material disposed therein. The chamber being sealed with a first membrane and a second membrane. The first membrane being ...
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WO/2012/174572 |
A method for improving airport and ramp throughput is provided. The method minimizes the time interval between an aircraft's landing and takeoff by independently moving the aircraft with an onboard electric driver that drives at least on...
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WO/2012/168518 |
The object of the invention is to achieve a universal module that can be fitted to any type of hose, and specifically to the various installations currently used, without making modifications thereto, and which is applicable not only to ...
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WO/2012/171023 |
A split winglet is disclosed having a first generally upward projecting wing end, and a second generally downward projecting wing end. The second generally downward projecting wing end may be integrally formed with the first generally up...
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WO/2012/168429 |
The present invention provides a method for starting up electric or electronic devices, in particular devices in or for an aircraft or spacecraft, comprising the following steps : supplying at least one location identification which cont...
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