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Patent Searching and Data


Matches 651 - 700 out of 3,501

Document Document Title
WO/2015/158894A1
The invention relates to a landing gear (1) of an aircraft (5), comprising: a strut assembly (10) including a first end (10a) designed to be mounted on the aircraft (5) and a second end (10b) opposite the first end (10a); a rod (14) slid...  
WO/2015/130360A3
A system for enhancing vision inside an aircraft cockpit (10) includes a primary display system (34) configured to receive the signals related to flight data (33) and display visual representations based on the flight data (33). The syst...  
WO/2015/149263A1
A damping device (10) and aircraft (100) using the damping device (10); the damping device (10) comprises a base (1) and a mounting base (2) being spaced a certain distance from the base (1). The damping device (10) also comprises at lea...  
WO/2015/149370A1
A tripod head driving device (100) and a tripod head assembly using same. The tripod head driving device (100) comprises a holding arm (10), a first motor (20), a connecting frame (30) used for fixing an imaging device (60), a connecting...  
WO/2015/144040A1
Disclosed is a mounting structure of an electronic speed governor in a holder, comprising a base (1) for fixing a carrying body, a first support (2) rotatablely connected with the base (1) and rotating in the Z-axis direction, a second s...  
WO/2015/136307A1
A lighting system for an aircraft cabin includes an electrical light source and a photoluminescent light source. The electrical light source is provided at or near a ceiling of the aircraft cabin and the photoluminescent light source is ...  
WO/2015/128533A1
The invention relates to a device consisting of a base (19) having a turbine (1) that is protected and partially concealed by a cover (15), and also includes an image-recording element (16), which is a camera in the present preferred emb...  
WO/2015/123669A1
An aerial camera system includes an aerial device disposed onboard a non-aerial vehicle as the non-aerial vehicle moves along a route. The aerial device also can be configured to fly above the route during movement of the vehicle along t...  
WO/2015/115927A1
´╗┐The claimed group of inventions relates to power engineering and can be used for locating faults in overhead power transmission lines. A method for locating faults in overhead power transmission lines comprises installing, on a lightn...  
WO/2015/076886A3
Embodiments described herein may help to provide medical support via a fleet of unmanned aerial vehicles (UAVs). An illustrative UAV may include a housmg, a payload, a line-deployment mechanism coupled to the housing and a line, and a pa...  
WO/2015/105886A1
An unmanned aircraft structure evaluation system includes a computer system with an input unit, a display unit, one or more processors, and one or more non-transitory computer readable medium. Image display and analysis software causes t...  
WO/2013/131072A3
A low power method for determining whether a cargo destined for air transport is in a flying state having the steps of: providing a housing for attachment to a cargo the housing having: an accelerometer for detecting a linear acceleratio...  
WO/2015/089637A1
A system and a method are disclosed for managing a plurality of critical functions in an aircraft, the system comprising at least one data providing unit for providing digital signals, wherein at least one digital signal is associated wi...  
WO/2015/085499A1
Provided is a carrier (200) for use on a moving body, the carrier being used for achieving coupling of the moving body and a carried object (209), and the carrier comprising at least two rotational axes (202, 204, 206), wherein a superim...  
WO/2015/086923A1
The invention relates to a method for processing images captured by a lens (OPT) on board an aircraft (1), said aircraft (1) including at least one engine (M) each of which includes at least one propeller (11), said method including: a s...  
WO/2015/085155A1
An airborne vehicle includes a positioning system to acquire information relating to a position of the airborne vehicle, and a measurement system to transmit signals to and receive signals from survey sensors of a survey arrangement used...  
WO/2015/079155A1
The invention relates to a system (2) for generating non-propulsive energy in an aircraft, including: an auxiliary power unit (20) including a gas turbine (21) and a fuel cell (22); a pathway (23) for the intake of outside air into the a...  
WO/2015/076886A2
Embodiments described herein may help to provide medical support via a fleet of unmanned aerial vehicles (UAVs). An illustrative UAV may include a housmg, a payload, a line-deployment mechanism coupled to the housing and a line, and a pa...  
WO/2015/073540A1
Lighting systems and methods for landing in a degraded visual environment are disclosed. The lighting systems comprise one or more lighting units mounted to an aircraft operable to hover near a landing zone. Each lighting unit is operabl...  
WO/2015/053901A1
A modular truss assembly for mechanically and electrically mounting system components of a modular equipment center (MEC 44, 46, 48). A plurality of MECs is spatially distributed throughout the vehicle (10) to service equipment loads. Th...  
WO/2015/014116A1
A remote control method and apparatus for controlling the state of a movable object and/or a load carried thereon are provided. The remote control method comprises: receiving, via an apparatus, a state signal that corresponds to a user's...  
WO/2014/175934A3
An auxiliary power unit bracket, according to an exemplary aspect of the present disclosure includes, among other things, a gearbox mounting face and a compartment mounting face, the gearbox mounting face configured to attach to an auxil...  
WO/2014/174340A1
An aircraft flight data monitoring and reporting system is provided. The system comprises: an onboard flight data recording and reporting unit; a zero-configuration service discoverer; a remote base station; a remote flight data monitori...  
WO/2014/174211A1
The invention relates to a device (14) for displaying an LED message on the fairing (16) of an aircraft, characterized in that said device comprises: at least one light-emitting sheet (26) urged against the fairing (16); a means (28) for...  
WO/2014/170060A1
The invention concerns a method for measuring the volume of a cluster of materials, comprising: - defining (20) a flight plan of a drone (10) for flying over a cluster (2) of materials; - acquiring (22), by the drone, when flying over th...  
WO/2014/167038A1
The aim of the present invention is to produce a display of the environment of the aircraft by combining live shooting by replacing a window with a camera lens and an illumination of this environment in suitable radiation ranges, connect...  
WO/2014/161428A1
Systems, devices, and methods are provided relating to improved mounting platforms for supporting a payload (1) on a movable object. In one aspect, an apparatus for supporting a payload (1) comprises: a first support member (6) coupled t...  
WO/2014/161945A1
Method for aerial image capturing by means of an unmanned and controllable aircraft comprising a camera, more particularly a drone, during a flight manoeuvre of said aircraft, comprising continual determining of a camera position and ali...  
WO/2014/150063A1
A swing down mount system (10) for mounting a camera gimbal (16) or other viewing/recording device to a helicopter is disclosed. The system comprises a frame (11), an axle (12) mounted on the frame, a first arm (14) attached to the axle,...  
WO/2014/143389A1
A coating composition including a hydrophobic first aliphatic polyisocyanate, a second aliphatic polyisocyanate including a hydrophilic portion, a polyester polyol, a hydrophilic polyol, and a fluorinated polyol compound is disclosed. A ...  
WO/2014/140981A1
The present technology provides a system and method for tracking payload drops from aircraft. The method includes initiating a payload drop, accurately determining the start of the drop and the end of a drop, determining a drop vector, a...  
WO/2014/134713A1
A proximity sensor for detecting non-contact detection of a target using a fibre optic strain sensor and a system for operating multiple such proximity sensors is disclosed. The proximity sensor includes an optic fibre that has an optic ...  
WO/2014/136068A1
A method provides alert information, regarding an aircraft wheel braking system, to an operator of an aircraft during an aircraft landing. An input of a target deceleration rate for the landing aircraft is received prior to the aircraft ...  
WO/2014/117248A1
A switch assembly is disclosed having a switch with an actuator moveable from an armed position to a disarmed position. A housing is attached to the switch and contains a cam that holds the switch actuator in the armed position. A trigge...  
WO/2014/106712A1
A method for managing an electric power network (1) of an aircraft, the power network (1) comprising at least one distribution bus arranged to supply electrical loads, at least one generator (G1, G2) of a propulsion engine of the aircraf...  
WO/2014/081614A1
A viewing device for an aircraft includes an image receiver adapted to receive an image of a predetermined spatial area of an exterior of an aircraft, an image projector adapted to display the image of the predetermined spatial area, and...  
WO/2013/074177A3
A turret assembly for attachment on the undersurface of an aircraft that reduces performance limitations due to gimbal lock and reduces the cross section profile of the assembly. The assembly includes a roll actuator including a drive sh...  
WO/2014/057037A1
An aircraft (10) is provided with at least one multifunctional light unit (16) comprising at least one light source (18) for outboard light emission, which unit is provided on sideway facing areas (20) of the aircraft. The multifunctiona...  
WO/2014/028091A3
A helicopter collision-avoidance system is disclosed. An exemplary system includes at least one lamp, such as a light emitting diode (LED) lamp, an incandescent lamp, a halogen lamp, an infrared lamp, or the like; a radar emitter configu...  
WO/2013/181402A3
A lighting arrangement for an aircraft includes a navigational lighting group (42) disposed at a leading edge (36) of a wing (38) of the aircraft. The navigational lighting group includes at least one right of way light (50, 52). The lig...  
WO/2013/142413A3
Anti-icing solid state aircraft lamps are disclosed. The anti-icing solid state aircraft lamp includes at least one solid state light source, a substantially optically transparent cover optically coupled to the at least one solid state l...  
WO/2013/190109A3
The invention relates to an electrical circuit adapted for cutting off an electrical supply to an electrical equipment, said electrical circuit receiving as input at least two discrete electrical signals xi, i=1, N, the electrical circui...  
WO/2014/022316A1
A power stabilizing device in a system includes as a portion of a power converter section, a second PWM converter provided between a second primary AC bus and a second DC bus in an electric system and configured to perform mutual convers...  
WO/2014/018163A1
A modular light emitting diode (LED), remote phosphor, and other lighting technologies lighting assembly includes a plurality of lighting subassemblies and a power supply electrically coupled with the plurality of lighting subassemblies ...  
WO/2007/021013A3
[PROBLEMS] An aircraft in which a payload box can be easily replaced according to purpose of use. [MEANS FOR SOLVING PROBLEMS] An aircraft in which a payload box (400) having various kinds of equipment including a camera loaded in it is ...  
WO/2014/011806A2
Aircraft washlight systems having an asymmetric lens are disclosed. An example vehicle cabin illumination system includes a light source located one side of a surface of a vehicle cabin, and an asymmetric lens through which the light pas...  
WO/2013/190044A1
The invention relates to an electric circuit suitable for cutting off an electric power supply of an electric device, the circuit including an electrical device and a supply voltage source of the electrical device, also having as inputs ...  
WO/2013/186536A1
A method of providing apparatus comprising: providing a first store and a first payload on or in the first store, the first store being for mounting to the outside of an aircraft (4); acquiring aerodynamic properties, moments of inertia,...  
WO/2013/004991A3
Casings (100) and housings for use in high speed airflow (for example for mounting on a high speed vehicle) are described. In one embodiment, a housing for imaging equipment is described. The housing has a tapering form with symmetrical ...  
WO/2013/181402A2
A lighting arrangement for an aircraft includes a navigational lighting group disposed at a leading edge of a wing of the aircraft. The navigational lighting group includes at least one right of way light. The lighting arrangement also i...  

Matches 651 - 700 out of 3,501