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Patent Searching and Data


Matches 1 - 50 out of 6,064

Document Document Title
WO/2020/101727A1
A panel assembly that includes inside and outside core layers, an armor layer sandwiched between the inside and outside core layers, and an armor member that includes at least an outside portion and a transverse portion. The outside core...  
WO/2020/100820A1
A flight vehicle 100 has an attachment part 25 on an upper part, the attachment part being constituted as a frame-shaped structure configured so that the vertical-direction position thereof can be adjusted, and the flight vehicle 100 has...  
WO/2020/101728A1
A door assembly configured to be positioned between a first compartment and a second compartment that includes a main door portion having a first decompression opening defined therein, at least a first panel portion positioned in a first...  
WO/2020/097042A1
This disclosure discloses a method comprising: positioning a stencil having an opening onto an aerospace part such that the aerospace part is accessible through the opening; positioning a masking medium onto the aerospace part through th...  
WO/2020/094688A1
The invention relates to an emergency opening device (1) for an aircraft door, comprising: a tubular operating member (2); and elastic compression means (3). The operating member (2) comprises a first end element (10) and a second end el...  
WO/2020/095025A1
A payload mechanism for a vehicle is provided. The payload mechanism comprises: a door (2) operable to be in a closed configuration or an open configuration within a recess of the vehicle, the recess having an aperture(10); a first beari...  
WO/2020/094042A1
Provided are a contact wire and contact net for an unmanned aerial vehicle, and a matching unmanned aerial vehicle and charging rod. The contact wire mainly consists of a surface twisted layer and a core body on which same is wrapped; Th...  
WO/2020/094695A1
The invention relates to an emergency opening device (1) for an aircraft door, comprising: a tubular operating member (2); and elastic compression means (3). The operating member (2) comprises a first end element (10) and a second end el...  
WO/2020/092313A1
An aircraft that includes a body defining a cabin interior, front and back rows of seats positioned in the passenger zone, a forward door and an aft door that are pivotable between a closed position and an open position. The cabin interi...  
WO/2020/091885A1
An aircraft that includes a body that defines a cabin interior, a divider member that divides the cabin interior into a cargo hold and a passenger cabin, front and back rows of seats positioned in the passenger cabin, a forward door that...  
WO/2020/091933A1
An aircraft that includes a body that defines a cabin interior and a side opening, a partition that divides the cabin interior into a cockpit and a passenger cabin, a front row positioned in the passenger cabin, and a first door position...  
WO/2020/091267A1
An aircraft thermoplastic reinforcement panel manufacturing apparatus according to the present invention comprises: a mold unit including a mold plate, a protective film placed on the mold plate, planar heating elements each installed on...  
WO/2020/079054A1
Aircraft door (1) comprising: an opening panel (2) provided with engagement abutments (26); a frame (3) intended to be attached to the fuselage (4) of the aircraft and comprising engagement counter-abutments (27); a hinge arm (5); a lift...  
WO/2020/079058A1
Aircraft door (1) comprising an opening (4), a frame (3), a hinge structure (5) and a circular translation guide device designed to maintain the orientation of the opening (4) during the opening or closing thereof. The hinge structure (5...  
WO/2020/074449A1
This invention concerns a door (3) of an aircraft (1) equipped with an opening/closing mechanism, the movement of which in a main horizontal plane (P) of the aircraft (1) is controlled by coupling between the door (3) and the frame (4) o...  
WO/2020/070927A1
[Problem] To elevate the containment ability of a ducted fan device at FBO time, without inhibiting a reduction in the weight thereof. [Solution] This ducted fan device has a fan shroud 52 having a torus shape in a planar view, and an el...  
WO/2020/071016A1
This method for manufacturing a structure using a composite material includes: a tapering step for forming a first tapered surface (6c) on a first stiffener (6) that is in an uncured state; a bending step for bending the stiffener such t...  
WO/2020/071417A1
This aircraft component (such as a T-shaped member (21), a protruding member (22), or a curved member (23)) has a laminated structure in which a plurality of composite material layers are laminated, and also has, as a three-dimensional s...  
WO/2020/057115A1
An arm folding assembly and an unmanned aerial vehicle are provided. The arm folding assembly comprises a connection member (1), a fixing sleeve (2), an arm receiving cylinder (3), and a limit stopper (4), wherein the connection member c...  
WO/2020/060719A1
An aircraft flooring system includes a floor beam, a seat track having a base flange, the base flange including a plurality of apertures, where the one or more of the apertures have a diamond-shaped profile, a seat track fitting coupleab...  
WO/2020/055830A1
A bi-directional egress hatch for a passenger aircraft may allow passengers to rapidly and safely exit, an overhead cabin of the aircraft onto the main deck, while allowing cabin crew to safely ascend into the overhead cabin if need be. ...  
WO/2020/045649A1
An aircraft component assembly jig (10A) is provided with: a plurality of header plates (12); receiving members (13), a plurality of which are provided on each header plate (12), and distal ends of which abut an upper surface or a lower ...  
WO/2020/045441A1
A seal structure (10) seals between a first facing surface (22) and a second facing surface (32), which face each other, by means of a seal material (40). A second part (30) has an insertion hole (31) which is open to the second facing s...  
WO/2020/047484A1
An unmanned aerial vehicle (UAV) is provided including a fuselage, a pair of wings extending outwardly from the fuselage, and a deployable surface moveable from a first undeployed position during normal flight to a second deployed positi...  
WO/2020/040671A1
Improved closed wing aircraft design and configuration with three wings on either side of the fuselage wherein at least one closed frame is established between the 1st wing (65) and the 2nd wing (67), by using at least one bracing entity...  
WO/2020/038356A1
An assembly for an aerial system (12) includes a wing support (46) foldably connected to a first and second side of a body (20) of the aerial system (12), a protection structure (42) coupled to the wing support (46) and disposed over pro...  
WO/2020/034980A1
A retractable unmanned aerial vehicle rotor protection device (100) and an unmanned aerial vehicle, the protection device being used for the protection of a rotor (200) of the unmanned aerial vehicle and comprising: an outer frame (10) u...  
WO/2020/029796A1
Provided are a propeller assembly, a power assembly and an unmanned aerial vehicle. The propeller assembly (10) comprises a propeller (12), wherein the propeller (12) comprises a first blade assembly (120); a second blade assembly (122) ...  
WO/2020/030735A1
Method for detecting a door status of an aircraft door (3), wherein the door status indicates whether the aircraft door (3) is opened or closed, the method comprising the following steps: - taking a first image (6a) of the aircraft door ...  
WO/2020/033010A2
An aircraft propulsion system with a drag reduction portion adapted to reduce skin friction on at least a portion of the external surface of an aircraft. The drag reduction portion may include an inlet to ingest airflow. The aircraft may...  
WO/2020/026533A1
Provided are a cap seal with which molding of a seal material by hand can be omitted and variation in cap seal mounting quality can be minimized, a fastening structure provided with said cap seal, and a method for mounting a cap seal. Th...  
WO/2020/020866A1
An emergency opening device for an aircraft door provided with an opening mechanism comprises: - actuation means (2, 5) for actuating the opening mechanism, comprising: a tubular operating member (2) equipped with a second locking end (4...  
WO/2020/020860A1
An emergency opening device for an aircraft door provided with an opening mechanism comprises: - actuation means (2, 5) for the opening mechanism, comprising: a tubular operating member (2); flexible compression means (5); - activation m...  
WO/2020/019629A1
A truss-type unmanned aerial vehicle frame (1) and an unmanned aerial vehicle. The vehicle frame (1) comprises a plurality of arms (11) and an intermediate connection member (12). The intermediate connection member (12) comprises a plura...  
WO/2020/020861A1
Device for opening an aircraft door in emergencies, said door being provided with an opening mechanism, comprising: - means (2, 5) for actuating the opening mechanism, comprising: a tubular manoeuvring member (2), and a second locking en...  
WO/2019/229083A3
Disclosed is an emergency exit door (2) for an aircraft cabin, said door comprising an opening assist mechanism and an opening/closing device having a control lever (7) which can selectively be actuated to either unlock the door (2) and ...  
WO/2020/015239A1
Disclosed are an unmanned aerial vehicle and an engine arm connecting structure thereof. The engine arm connecting structure (100) comprises an upper clutch member (110) and a lower clutch member (120) matched with the upper clutch membe...  
WO/2020/011013A1
A water-resistant unmanned aerial vehicle (100) comprises: a fuselage (10); an arm (20) connected to the fuselage; a motor (302) provided at the arm; and a propeller (304) connected to a rotary shaft of the motor. wherein a receptacle (2...  
WO/2020/000267A1
A motor (100), and a radar assembly, an unmanned aerial vehicle, a power device and a pan-tilt which have the motor. The motor (100) comprises a base (10), a rotor assembly (20), a first bearing (30), an elastic member (40), and a suppor...  
WO/2020/003610A1
The purpose of the present invention is to provide a composite material that is capable of suppressing decrease in the strength, which is caused by bending of fibers of a skin material during the time when the composite material is cured...  
WO/2020/000658A1
An unmanned aerial vehicle (10) and an arm (100) thereof, the arm (100) of the unmanned aerial vehicle (10) comprising: a body (110); a foot support (120) is provided at a front end of the body (110), and an inner part of the foot suppor...  
WO/2020/003609A1
The present invention addresses the problem of providing a method for molding, using a honeycomb core, a composite material structure that is high-quality, low cost, and leaves less voids. The present disclosure addresses the problem of ...  
WO/2020/000206A1
Provided is an unmanned aerial vehicle, comprising: a body (1) and a plurality of function modules (20); the body (1) comprises a plurality of support modules (10); the plurality of functional modules (20) are arranged independent of eac...  
WO/2020/000644A1
An unmanned aerial vehicle (100) and aerial vehicle frame (10) thereof. The aerial vehicle frame (10) comprises a central body, foot supports (1), and multiple aerial vehicle arms. The central body comprises a bottom housing (2), a mount...  
WO/2020/000507A1
An unmanned aerial vehicle and a body thereof and a pan-tilt-zoom camera. The unmanned aerial vehicle comprises a body (100). The body (100) comprises: a housing (110) provided with an installation groove (111), wherein the installation ...  
WO/2020/003608A1
The present invention addresses the problem of providing a composite material that can prevent a strength reduction when fibers of a skin material are bent during curing of the composite material. In a composite material (1), a filler (9...  
WO/2020/005906A1
A system and method of a modular floor assembly and installation on an aircraft is presented in embodiments herein. A floor assembly comprising an underlayment layer and a decorative layer may be assembled to provide an aircraft floor th...  
WO/2020/000628A1
An unmanned aerial vehicle, comprising a fuselage (1), front side arms (2) arranged at the front two sides of the fuselage (1), and rear side arms (3) arranged at the rear two sides of the fuselage; the front side arms (2) and the rear s...  
WO/2020/000660A1
An unmanned aerial vehicle (10) and arms (100) thereof. Each arm (100) of the unmanned aerial vehicle (10) comprises a tubular body (110); the body (110) is divided along its axial direction into a forearm portion (120) for carrying a po...  
WO/2020/000677A1
An unmanned aerial vehicle and a machine frame thereof, related to an unmanned aerial vehicle technology. The unmanned aerial vehicle (1) comprises the machine frame (100), the machine frame (100) comprising a center body (110), comprisi...  

Matches 1 - 50 out of 6,064