Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 1 - 50 out of 64,423

Document Document Title
WO/2019/137919A1
A flow booster for optimizing flow of fuel passing into an aircraft. The flow booster includes a fuel intake fluidly coupled to the fuel circuit, and includes a housing and a piston. The piston has a piston head slidably movable in the h...  
WO/2019/139172A1
The purpose of the present invention is to effectively use a small unmanned aircraft in all fields in which research and development are advancing. An information processing system that includes a drone 1 having a drive unit 11 for movin...  
WO/2019/140119A1
Methods, systems, and devices for wireless communications are described. A user equipment (UE) configured as a drone-coupled wireless device may be configured to transmit a message indicating information relating to the drone-coupled wir...  
WO/2019/139654A1
There is provided a dual rack and pinion rotational inerter system (500) for damping movement (694) of a flight control surface (122) of an aircraft (100). The system (500) has a flexible holding structure (506) disposed between the flig...  
WO/2019/139872A1
In some embodiments, apparatuses and methods are provided herein useful to identifying and evaluating an unidentified autonomous vehicle (AV) during a retail product delivery. In some embodiments, there is provided a system for identifyi...  
WO/2019/138466A1
In order to assist an operator of an unmanned aircraft while limiting power consumption, an operation information acquisition means (101) of this unmanned aircraft control system (S) acquires operation information pertaining to at least ...  
WO/2019/139574A1
Example moveable mounting structures and methods are described. In one implementation, an unmanned aerial vehicle (UAV) includes a body and a moveable mounting structure coupled to the body. The moveable mounting structure can move betwe...  
WO/2019/138788A1
Provided is a deployable structure which can be compact in form while being stored before or after deployment and which does not retain fold lines. The nozzle 10 of a rocket motor 1 is constituted by a fixed nozzle 11 and a distortable n...  
WO/2019/138343A1
An aerial vehicle is described herein. The aerial vehicle includes a lift mechanism that includes a rotor blade assembly coupled to a motor assembly. The rotor blade assembly includes a plurality of rotor blades that are pivotably couple...  
WO/2019/086588A3
The invention relates to an aircraft (1), in particular a commercial aircraft, and to an arrangement (20) comprising an aircraft (21). The aircraft (1) comprises at least one laser projection system (2) for projecting one or more contour...  
WO/2019/139173A1
The purpose of the present invention is to find a more meaningful method of use of an information processing system that includes a moving body such an unmanned aerial vehicle, by providing the moving body with new functions. One or more...  
WO/2019/139263A1
The present invention relates to a race system and method for an unmanned aerial vehicle. The race system for an unmanned aerial vehicle of the present invention comprises: at least one unmanned aerial vehicle which transmits data regard...  
WO/2019/139073A1
The purpose of the present invention is to improve safety of a flying device when dropped down. Provided according to a typical embodiment of the present invention is a flying device (1), comprising: an airframe unit (2); a lift force-ge...  
WO/2019/137791A1
The invention relates to a retaining assembly (10) of an electric motor (12) for driving an aircraft on an aircraft frame (14), said electric motor (12) being attachable to a support structure of the aircraft via said frame. The electric...  
WO/2019/140159A1
A satellite system operates at altitudes between 100 and 350 km relying on vehicles including a self-sustaining ion engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are...  
WO/2019/140219A1
Coatings and materials that are atomic oxygen resistant and have an atomically smooth surface that can reduce drag are disclosed. The coatings and materials can be used on at least a portion of a spacecraft intended to operate in harsh e...  
WO/2019/138660A1
This honeycomb sandwich panel is provided with: a honeycomb core 1; a first surface material 2 disposed on one surface of the honeycomb core 1 so as to be in close contact therewith; a second surface material 3 disposed on the other surf...  
WO/2019/140437A1
Compliant mounting systems, devices, and methods for mounting a vehicle engine to a vehicle structure or base include a top mount, a lower mount, a center trunnion mount, and an aft mount which are configured to react forces transmitted ...  
WO/2019/140395A1
Present aspects are directed to a system that receives digital images of parcels at various points throughout a transportation and logistics network. Based on analysis of a single digital image of a parcel, the dimensions of the parcel a...  
WO/2019/139507A1
The present invention relates to a completely new system that generally contributes to balancing the fuselage of an aircraft in general, and during landing in particular, and which is based fully on the thrust generated by the engine of ...  
WO/2019/138100A1
The disclosure relates to a wing 2 with at least two winglets 8,9,10 having a relative dihedral angle between them, and to a airplane 1 having such wings. An upstream winglet 8 broadens a region of inclined airflow, and a more downstream...  
WO/2019/137078A1
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises landing gears (40). Each landing gear (40) comprises: a driving unit (41) provided in a body (10) of the unmanned aerial vehicle, a traction mechanism (42) con...  
WO/2019/139653A1
There is provided a translational inerter assembly (500) for damping movement (606) of a flight control surface (122) of an aircraft (100). The assembly (500) has a press fit element (510) fixedly disposed within a first end (502a) of th...  
WO/2019/139559A1
The invention relates to aviation technology, more particularly to aircraft construction, and even more particularly to a cycloidal rotor that can be used to generate lift and to control an aircraft. The present cycloidal rotor comprises...  
WO/2019/140156A1
A satellite system operates at altitudes between 180 km and 350 km relying on vehicles including an engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially l...  
WO/2019/138576A1
[Problem] To provide a remote operation spray device for operating from a remote location and forcing down a spray nozzle for a spray device, that can easily generate necessary and sufficient pressing pressure for forcing down with a sim...  
WO/2019/137146A1
An upright shell extending along an axial direction, built inside with an energy storage module, a wireless communication module, and a control module in a telecommunication connection with the wireless communication module; an axially e...  
WO/2019/134385A1
A camera assembly (10) and an unmanned aerial vehicle (100). The camera assembly (10) comprises a support (12) and a camera module (14); the camera module (14) is mounted on the support (12); the support (12) comprises a mounting plane (...  
WO/2019/134912A1
The invention proposes a seat comprising a chair and a covering shell, said covering shell partially enveloping the chair. A structure of the seat shell further comprises: - at least one coating skin and at least one stiffening skin shap...  
WO/2019/134396A1
A paddle protection structure and an unmanned aerial vehicle, relating to the technical field of unmanned aerial equipment. The paddle protection structure is applied to an unmanned aerial vehicle and comprises a first frame part (1) and...  
WO/2019/096358A3
The invention relates to an autogyro having a fuselage comprising a rotor on its upper face, the rotor having rotor blades and being made to autorotate by an airflow, wherein the rotor has a rotor drive such that said rotor can be motor-...  
WO/2019/135689A1
The present aerodrome installation for recovering energy from an airplane during landing to accelerate an airplane during takeoff comprises at least two runways, each of which comprises an aerodrome unit resting upon support rails by mea...  
WO/2019/134356A1
Provided are an unmanned aerial vehicle (UAV), a power train, and a method for reducing air resistance in the UAV. A motor is arranged within a support arm or a wing such that a motor shaft is parallel to the longitudinal axis of the sup...  
WO/2019/134511A1
A ground support device for aerospace engineering, and specifically, a manipulation robot for assembly tests of a space station experiment cabinet, comprising a movable lifting platform (1), an integrated monitoring system (2), a rotatin...  
WO/2019/135802A1
A flight vehicle includes a drone (28) with a pair of shaped protrusions (22, 24) mechanically coupled to the drone. One of the shapes is a hollow lift-producing shape (22), such as being a balloon filed with a lighter-than-air gas, and ...  
WO/2019/136195A1
Systems and methods are disclosed for image capture. For example, systems may include an image capture module including an image sensor configured to capture images, a base that includes a processing apparatus and a connector, and an int...  
WO/2019/135078A1
The present invention provides a kite apparatus (100), comprising a main tether line (120a), for connection at a first end to a base station (110), a hub (130a) connected to a second end of the main tether line, a sub-tether line (145a, ...  
WO/2019/134150A1
A fault detection method and device for an unmanned aerial vehicle and a movable platform. The method comprises: detecting current flight state parameter information of an unmanned aerial vehicle (S101); and determining occurrence of a f...  
WO/2019/135271A1
An unmanned aircraft reservation system that has: an unmanned aircraft that has a battery; power supply devices that supply power to the unmanned aircraft; a flight management device that receives aircraft information about the unmanned ...  
WO/2019/135272A1
A flight control system that has: an unmanned aircraft that has a battery; a flight management device that includes a storage part at which is stored information about the past flight record of the unmanned aircraft, that receives aircra...  
WO/2019/134399A1
An unmanned aerial vehicle and a casing (1). The casing (1) is internally provided with a heating element (5) of the unmanned aerial vehicle, and the casing (1) is provided with an air inlet duct (8) thereon; the air inlet duct ( 8) is u...  
WO/2019/136304A1
In one embodiment, an apparatus is attached to a feature to be deployed on a satellite. The apparatus includes a first material having an impedance, a second material coupled to the first material configured to provide a current or volta...  
WO/2019/135058A1
The invention relates to a structure (131) for the nacelle of an aircraft propulsion unit, comprising a first skin and stiffeners (3) arranged to hold acoustic treatment modules (4) against the first skin. Each acoustic treatment module ...  
WO/2019/135912A1
Controlling an unmanned aerial vehicle to traverse a portion of an operational environment of the unmanned aerial vehicle may include obtaining an object detection type, obtaining object detection input data, obtaining relative object or...  
WO/2019/134170A1
A pan-tilt (100), a photography assembly (300), and an unmanned aerial vehicle, relating to the technical field of aircrafts. The pan-tilt (100) comprises a pitch-axis motor, a connecting arm (44), a heading-axis motor, a roll-axis motor...  
WO/2019/134406A1
Disclosed is an unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises: a frame main body (10) and a battery (20), wherein the frame main body (10) comprises a battery accommodating cavity (11) for accommodating the b...  
WO/2019/135848A1
Various embodiments include methods and aerial robotic vehicles that adjust a flight control parameter based on whether propeller guards are installed. An aerial robotic vehicle processor may determine whether a propeller guard is instal...  
WO/2019/134712A1
An unmanned aerial vehicle (UAV) (100) for a long duration flight includes a UAV body assembly(110) and a flight control system (FCS) (120) coupled to the UAV body assembly(110). The UAV(100) may further include a motor(150) coupled to t...  
WO/2019/135264A1
[Problem] To provide a flying vehicle having both a more basic structure and safety measures in place. [Solution] This flying vehicle comprises: a flying unit that is equipped with a plurality of rotary wings for producing thrust; a leg;...  
WO/2019/135786A1
The present invention related generally to acquisition, transport, and archiving of space mineral resources, including the acquisition of samples for scientific investigation on Earth or on orbiting space stations. Another use of this ap...  

Matches 1 - 50 out of 64,423