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Patent Searching and Data


Matches 1 - 50 out of 5,134

Document Document Title
WO/2018/006120A1
A vehicle security system, particularly for aircraft, comprises at least one first actuator in a cockpit of the vehicle operable to control a cockpit door lock and a plurality of second actuators in a passenger section of the vehicle ope...  
WO/2018/009909A1
Protective covers (e.g., "liners") for use in protecting aircraft cargo hold floors from potentially harmful or dangerous fluids and other substances, and from physical damage, are described herein. In some embodiments, the cargo pit lin...  
WO/2018/004626A1
Disclosed herein is a water helicopter includes a fuselage, first and second fixed wings extending outwardly from left and right ends of the fuselage, first and second propellers disposed in a spaced apart configuration on a top surface ...  
WO/2018/005537A1
The present application relates to methods of manufacturing an orthotropic deck panel. One of the disclosed methods includes securing a rib member (102) in a first fixture, beveling an edge surface of the rib member (102) while the rib m...  
WO/2018/002308A2
A cabin module for a commercial aircraft comprises a set of bulkheads defining a quadrant with an inboard wall and converging side walls. The module is sub-divided by a removable partition which splits the module into two passenger compa...  
WO/2017/220931A1
The invention relates to an assembly of a fixed internal structure (54) of a turbojet engine nacelle (2) and thermal protection panels (640, 642), said fixed internal structure (54) comprising an inner face (540), on which the thermal pr...  
WO/2017/214934A1
A frame assembly (20), comprising a frame (21) and arms (22); each of the arms (22) is connected to one end of the frame (21), the frame (21) is connected to the arms (22) by means of joint portions (30, 60), the joint portions (30, 60) ...  
WO/2017/218696A1
A spacecraft is provided, which includes one or more of a centrally-oriented core, which includes a computing device. The computing device includes a processor and a memory, coupled to the processor, including computer instructions to co...  
WO/2017/215529A1
A propeller and a fuselage, comprising a forming foam (10), at least one first fiber fabric layer (20) provided on an upper surface of the forming foam (10), and at least one second fiber fabric layer (30) provided on a lower surface of ...  
WO/2017/215296A1
Disclosed is a flying robot clamping device, comprising at least two clamping jaws (1) arranged at the bottom of a flying robot body. Each clamping jaw (1) can move in an opening and closing manner. The at least two clamping jaws (1) mut...  
WO/2017/207874A1
Connector (208) suitable for integration with a functional module (201), optionally a sensor module, to be attached as payload to an aerial vehicle (101), preferably unmanned aerial vehicle (UAV), by the connector, said connector compris...  
WO/2017/207666A2
The invention relates to an air ship having a supporting structure (12) and a shell (10) that can be filled with a gas and which is tensioned by the supporting structure (12). According to the invention, said supporting structure (12) co...  
WO/2017/205997A1
Systems and methods are provided for transformation of an arm (104) of an unmanned aerial vehicle (UAV) (100) between a flight configuration and a compact configuration. The arm (104) may have multiple foldable sections (104-11, 104-12, ...  
WO/2017/208157A1
An emergency exit assembly for an aircraft, including a window frame, a window assembly having an outer surface abutting the inner surface of the window frame around its perimeter, and retaining elements spaced around the perimeter of th...  
WO/2017/203910A1
A method for designing the cross-sectional shape of the fuselage of a flying body having the fuselage extending in the roll axial direction, the section being taken on a plane perpendicular to the roll axial direction. This method is pro...  
WO/2017/198083A1
Disclosed is an aerial vehicle, comprising an aerial vehicle body. The front extremity of the aerial vehicle body is the nose, while the rear extremity is the tail. An air guiding part is upward protrudingly provided on the middle part o...  
WO/2017/201341A1
The self fixturing heater includes an outer casing having a central channel therein for selectively receiving and retaining in friction-fit relation an elastomeric fixture from a nutplate fastener assembly that axially aligns the self fi...  
WO/2017/201207A1
Systems, devices, and methods are provided that relate to aircraft with modular cabins and modular distributions. The aircraft may include a set of modules and a centralized utility bus. A module creation ecosystem may be provided that p...  
WO/2017/196568A1
An isolation mount connecting a panel to a structure includes a housing disposeable on the structure, a fastener receiver with a panel-facing surface, and a damper connecting the housing to the fastener receiver. The panel-facing surface...  
WO/2017/196171A1
The invention relates to an aircraft panel (1), in particular a cabin window. The invention also relates to an aircraft comprising at least one aircraft panel according to the invention, wherein the aircraft panel is preferably formed by...  
WO/2017/185487A1
A battery fixing and mounting structure for a battery self-dismounting unmanned aerial vehicle comprises an unmanned aerial vehicle mainly body (1) and a battery cover (2). A battery chamber (10) used for accommodating a battery (4) is f...  
WO/2017/186967A1
Unmanned aerial vehicle (UAV) (2) including a flight propulsion system (2) and a support system (4) coupled to the flight propulsion system, the support system comprising a protective outer cage configured to surround the flight propulsi...  
WO/2017/185495A1
A fastening structure for fast dismounting and replacement of an arm of a multi-shaft unmanned aerial vehicle and for uniform force bearing comprises an unmanned aerial vehicle main body (1) and a detachable arm assembly (2). The unmanne...  
WO/2017/188127A1
Provided is a component mounting system (10) in which a component (80) is mounted on a frame member (70) by using a fastener (42), the system comprising: a machine (40) that perforates the frame member and component along a machining axi...  
WO/2017/188911A1
An aircraft comprises a fuselage portion, wings, landing gear, engines, nose and tail cones, a tail fin, and a detachable cabin module, which constitutes a cabin for transporting passengers and cargo. The nose cone comprises a cockpit an...  
WO/2017/183551A1
This unmanned aerial vehicle is optimized for transport of a load and can efficiently drop a load and manage the vehicle body. The unmanned aerial vehicle, provided with multiple rotor blades, is characterized in that a frame of the unma...  
WO/2017/183004A1
An electrochromic device includes one or more flame-retardant agents.  
WO/2017/183684A1
This aircraft fuselage assembly jig is equipped with: a base provided with a plurality of frame indices for determining the positions of both ends of a plurality of aircraft fuselage frames; a plurality of header plates which project fro...  
WO/2017/183685A1
This aircraft fuselage assembly jig is equipped with: a horizontally oriented base on which an aircraft fuselage panel is placed so as to be lying down, and which is provided with a plurality of frame indices for determining the position...  
WO/2017/177458A1
Disclosed is a frame of an unmanned aerial vehicle, comprising: a centre frame (1), a dividing circuit board (2) and a flight-control installation component (3). The centre frame (1) comprises a top surface and a bottom surface opposite ...  
WO/2017/173725A1
An unmanned aerial vehicle having a linked folding structure, comprising a vehicle base (100), and a plurality of vehicle arms (200) and landing gear (300) distributed along the perimeter of the vehicle base (100), and also comprising co...  
WO/2017/177162A1
A coated transparency includes: a transparency; a base layer on the transparency, the base layer comprising at least one selected from an organic compound, an organosilicon compound, and a polysiloxane compound; a metal layer physically ...  
WO/2017/173732A1
An unmanned aerial vehicle (UAV) with a multi-arm synchronous folding mechanism, comprising: a base (1) having a flat plate shape and being provided with a plurality of rotating shafts (12) which extend parallel to the base (1); a plural...  
WO/2017/173733A1
An unmanned aerial vehicle comprising: an upper body portion (1), a middle portion (2), and a lower body portion (3). The upper body portion (1) comprises: at least one mechanical arm (11). At least one propeller (13) is arranged on each...  
WO/2017/174906A1
Polarisible interior trim window comprising a removable fixing device Interior trim window (13) able to collaborate with a support (11), the said interior trim window (13) comprising a polarisable film, a device for applying a tension to...  
WO/2017/176889A1
A truss reinforced radome crown structure shock absorbing and recoiling system that is utilized with an aircraft antenna adapter plate or other satellite communication (SAT-COM) structure to an aircraft airframe or fuselage and for allow...  
WO/2017/167945A1
The invention is based on a vehicle device, in particular an aircraft device, having at least one window unit (48a; 48b; 48c) and having at least one transparency-switching unit (54a; 54b; 54c) which is provided, in at least a first oper...  
WO/2017/172840A1
This document describes a system and method through which unmanned aerial vehicles (UAVs) can be docked, with a device that can secure the UAVs, and information can be transmitted to and from such UAVs. The UAVs are secured through the u...  
WO/2017/172906A3
Applicant discloses a two part polymer mix for use in the aircraft industry that is applied with pneumatic mix and spray gun. The two part cartridge is used in the mix and spray gun so the mix is applied immediately upon mixing, but the ...  
WO/2017/166275A1
Airframe connection components for an unmanned aerial vehicle, comprising: a support tube (110), an auxiliary member (130), and a secure member (140). An opening end of the support tube (110) is used for being fitted to a connection part...  
WO/2017/154551A1
This flying object (100) comprises: a plurality of rotor units (20) each including a propeller (21) and a motor (22) that drives the propeller (21); a plurality of balloons (30) respectively provided to the plurality of rotor units (20);...  
WO/2017/155562A1
Described are mounting assemblies for securing aircraft passenger seats, including a beam, an adaptor, and fasteners. The beam can include holes spaced along a flat upper surface. The adaptor can be supported by the beam and include a ch...  
WO/2017/148923A8
A remote-controlled unmanned foldable aircraft (1) comprises at least two motors (3) that allow the aircraft (1) to fly, and at least one support structure (2) for supporting said motors (3); the support structure (2) is flexible and inf...  
WO/2017/148923A1
A remote-controlled unmanned foldable aircraft (1) comprises at least two motors (3) that allow the aircraft (1) to fly, and at least one support structure (2) for supporting said motors (3); the support structure (2) is flexible and inf...  
WO/2017/151081A1
The utility model relates to the sphere of aviation and aircraft repair technology, namely to the Method of on-condition repair and modernization up-dating of an aircraft center wing section, in particular, of Antonov-32 (An-32) type air...  
WO/2017/143501A1
An unmanned aerial vehicle (UAV) (100) may comprise a central body (102), and a plurality of arms (104) extendable from the central body. Each arm (104) may be configured to support one or more propulsion units (108).Each arm (104) may b...  
WO/2017/146666A1
The inventions relate to aviation and to ground transport. An aircraft adapted for saving passengers in the event of an emergency consists of an upper and a lower part. The upper part is designed to be capable of controlled flight in the...  
WO/2017/143643A1
Disclosed is an unmanned aerial vehicle (100, 200), comprising a body (10, 10'), arms (20) and power assemblies (30, 30'). The arms (20) are connected to the body (10, 10') and support the power assemblies (30, 30'). The arms (20) at lea...  
WO/2017/143645A1
Disclosed is an unmanned aerial vehicle (100), comprising a body (10) and arms (22) for carrying power devices (21), the power devices (21) being used for providing power of flight. The arms (22) are movably connected to the body (10), a...  
WO/2017/141526A1
Disclosed is structure designing method for installing a composite material including a polyarylate fiber and a resin in a structure, such as a vertical tail fin, as a vibration damping member, the method comprising: a step S3 for analyz...  

Matches 1 - 50 out of 5,134