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Matches 1 - 50 out of 57,652

Document Document Title
WO/2017/178790A1
An aircraft (101) is provided with a single centrally located inceptor (110) for controlling pitch and roll of the aircraft. The inceptor (110) is provided with a double grip (11, 112) so that it may be comfortably operated by either a p...  
WO/2017/180840A1
A system for calculating maintenance predictions and making improvements to performance deficiencies to one or more components in an on-board inert gas generating system (OBIGGS) is described. The OBIGGS components include an ozone conve...  
WO/2017/178097A1
A profile disc (1) is proposed which is designed for mounting on an aircraft wheel rim for rotation therewith and has a plurality of air-guiding surfaces (2) which protrude from the plane of the profile disc (1) and which are capable of ...  
WO/2017/178687A1
The invention relates to a device for the detection and interdiction of drones, all in a single system. The invention comprises a passive surveillance and detection radar, a communication and synchronisation system, a system for charging...  
WO/2017/180392A1
The modular aircraft system includes a single fuselage (10) having a permanently installed empennage (12) and plural sets of wing modules (46a, 46b, 66a, 66b, 68a, 68b) and engine modules (56, 60, 64), with each wing and engine module op...  
WO/2017/180780A1
Described herein are features for a riser release flaring system for parafoils and other descent flight vehicles for controlled descent and landing of the flight vehicle. The descent flight vehicle may have a payload suspended by a canop...  
WO/2017/177406A1
A blade clamp (11) for a folding propeller, a folding propeller having the blade clamp, a power unit, and an unmanned aerial vehicle. The blade clamp (11) is used for fixing and holding blades (15) of a folding propeller. The blade clamp...  
WO/2017/179378A1
[Problem] To provide a spectral camera control device, a spectral camera control program, a spectral camera control system, an aircraft equipped with said system, and a spectral image capturing method, with which it is possible for each ...  
WO/2017/177467A1
A shock-absorbing mechanism (100), and an unmanned aerial vehicle and a movable device using the shock-absorbing mechanism (100). The shock-absorbing mechanism (100) comprises a housing (10) and a piston. One end of the piston is slidabl...  
WO/2017/178684A1
The invention relates to a modular structure formed by successive screens (1), each screen including a base (4) resting on the ground and a front partition (5). According to the invention, the front partition (5) separates an inner part ...  
WO/2017/178853A1
The air flow which this invention itself makes on its surface makes lift by the Bernoulli effect. This invention utilizes the difference of the pressure of one side of the surface on which air flows and that of the other side of the surf...  
WO/2017/178078A1
The disclosed invention considers an apparatus, system and methods that may operate to enable centralized control over a plurality of locking devices interconnected to a central control unit thus providing additional security on each sto...  
WO/2017/179160A1
Provided is an unmanned aircraft vibration-damping structure having a simple, lightweight, and small configuration which can be manufactured at low cost, and which is capable of effective vibration damping of an object to be vibration-da...  
WO/2017/179953A1
The present invention relates to a system for monitoring and suppressing forest fires using drones. By installing a plurality of vertical towers in a mountainous area and attaching drones to the vertical towers so that the drones can tak...  
WO/2017/180020A1
The present aircraft comprises a body in the form of a disc-like solid of revolution, in which an annular fan wheel is used as a propeller, said fan wheel generating a primary lift, and a counter-rotating airbreathing jet engine. The ann...  
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/2017/177301A1
A power supply module for providing power to an unregulated spacecraft electrical power bus, the power supply module comprising a solar cell, output terminals, and a power converter mounted to the solar cell, the power converter providin...  
WO/2017/178683A1
In operations that require a 3-D view and need a global view of a work area when it is advisable to have an enlarged view of a part of said area, having two pairs of cameras, one pair being stationary and the other being moveable and con...  
WO/2017/177664A1
An antenna support (11) fixed on a mounting surface (211). The antenna support (11) comprises two or more protruding arms (14) fixed at relative positions. A support platform (141) is provided on the end of each protruding arm (14) dista...  
WO/2017/180239A1
According to various embodiments, an unmanned aerial vehicle (UAV) is provided. The UAV may include a motor controller (202). The UAV may further include a motor (105) connected to the motor controller (202). The UAV may further include ...  
WO/2017/175139A1
This disclosure includes armrests having one or more laminates and methods and kits for making the same. Some armrests include an elongated beam extending between a first end and a second end, the elongated beam having one or more lamina...  
WO/2017/176080A1
The present invention relates to a dispersing device for dispersing contents in the form of a liquid formulation, a granular formulation or a mixture and, particularly, provides a dispersing device comprising: a tank for storing the cont...  
WO/2017/176310A1
A satellite (10) has thrusters (18) that are integral parts of its frame (12). The frame defines cavities therein where thrusters are located. The thrusters may include an electrically-operated propellant and electrodes to activate combu...  
WO/2017/177038A1
An aerial device is provided. The aerial device includes a processor and a memory that includes instructions configured to cause the processor to perform certain operations when the processor executes the instructions. The operations may...  
WO/2017/175217A1
To eliminate stability issues in forward flight due to oncoming flow interfering with the flows produced inside the rotor, rotor shielding or enclosure are used giving it the ability to operate steadily at various forward speeds. Further...  
WO/2017/174942A1
The invention relates to a device (10) for propelling a passenger (1), comprising a body (10a) arranged to receive the passenger (1) and cooperating with a fuel-fed thrust unit (12). The arrangement of such a device can be used to obtain...  
WO/2017/174939A1
The invention relates to an electrical connector (18) suitable for electrically connecting a device (14) arranged on the outer surface of the fairing (6) of an aircraft (10). The connector (18) is characterised in that it comprises a tub...  
WO/2017/176004A1
The present invention relates to: a device for connecting, to a drone, a line to be used in the installation of a transmission line and a communication line and then separating the line at a target point, in order to install the line on ...  
WO/2017/174944A1
The invention relates to a device (10) for propelling a passenger (1), comprising a body (10a) arranged to receive the passenger (1) and cooperating with a fuel-fed thrust unit (12). The arrangement of such a device can be used to obtain...  
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/2017/173734A1
A method and a device for adjusting a photographic angle and an unmanned aerial vehicle. The method for adjusting a photographic angle comprises: acquiring position information of a photographic target and an unmanned aerial vehicle (101...  
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/2017/175195A1
A rotor (3, 3') for a hover-capable aircraft (1) is described that comprises: a drive mast (6); a hub (5) operatively connected to the drive mast (6) and rotatable about a first axis (A); and at least two blades (9) hinged to the hub (5)...  
WO/2017/174911A1
The invention pertains to a luminous display device (14) designed to be fixed on the fairing of an aircraft, the device comprising: -an electroluminescent film (140); -an electrically conducting protection film (142), designed to be inse...  
WO/2017/174288A1
The invention relates to a device for controlling the collective pitch and the cyclic pitch of the rotor blades of a rotorcraft, of the direct turbine driven type with counter-rotating coaxial rotors (REDT), said device comprising means ...  
WO/2017/175804A1
[Problem] To provide a method for controlling the flight of a drone that performs accurate chemical spraying on agricultural land having a narrow and complex topography. [Solution] At least one reference point pole is installed at a boun...  
WO/2017/175696A1
A low earth orbit (LEO) satellite system in which a constellation is configured from a large number of satellites circling along a low-altitude orbit so as to construct a global monitoring infrastructure for many terminal devices, each o...  
WO/2017/176824A1
Systems, apparatuses, and methods are provided herein for receiving aerial vehicle delivery. An apparatus for receiving aerial vehicle delivery comprises a receiving pad configured to receive a package released by an aerial vehicle; one ...  
WO/2017/176154A1
The invention relates to on-board emergency and safety equipment and concerns covers containing airbags for chairs installed in aircraft. The device comprises a cover on an aircraft chair, in which the following, equipped with pyrotechni...  
WO/2017/176490A1
Liquid storage systems for space vehicles include at least one storage tank including a tank inlet, a tank outlet, and a plurality of liquid storage compartments coupled to each other in series between the tank inlet and the tank outlet....  
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/2017/176811A1
In an illustrative embodiment, a stowage compartment system for an aircraft passenger suite articulates from a lowered position wherein the top of the compartment is disposed at a height that is approximately even with a footrest or otto...  
WO/2017/175199A1
An aerial vehicle, configured to transport cargo, and including a propulsion system and a foldable cage (204) is described. The foldable cage is substantially linear while in a folded configuration, and substantially circular while in a ...  
WO/2017/176298A1
A contoured class divider (10) for dividing an aircraft cabin according to a predetermined class arrangement and including a divider panel (12) having a contour closely matching a contour of a forward-positioned seatback (S), and adapted...  
WO/2017/176754A1
In an illustrative embodiment, an apparatus for treating air discharged to a passenger suite of an aircraft includes an enclosure that houses components for treating air passing through the enclosure and a detachable cover connected to t...  
WO/2017/175410A1
The present invention configures a variable pitch mechanism for helicopters, which has a simple configuration having a reduced number of components, and which is capable of precisely controlling the pitch angle of blades even without an ...  
WO/2017/176650A1
In a preferred embodiment, an aircraft monument is adapted for being mounted against an aft-facing bulkhead of the aircraft. The monument may have an aisle-accessible compartment that includes comestible item dispensers and lower footwel...  
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/2017/176748A1
In an illustrative embodiment, a crew information system is coupled to sensors in passenger seats, seatbelts, tray tables and overhead bins. If the vehicle seat sensor subsystem senses a passenger on a seat and senses the corresponding p...  
WO/2017/176953A1
A vehicle includes a propulsion system using one or more impellers as opposed to propellers. The impellers impart circumferential and radial velocity components to the working fluid, which may be air or water. The air is deflected by cou...  

Matches 1 - 50 out of 57,652