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WO/2015/153845A1 |
A method of drive system diagnostics of an aircraft includes capturing high load drivetrain component vibration data at select steady-state and/or high-load transient operating conditions of the aircraft and processing the captured vibra...
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WO/2015/146528A1 |
A cap (9) is applied to a securing structure part (1) for securing structure elements (3, 3) using a fastener (5) passed through through-holes (3a) formed in the structure elements (3, 3), and a collar (7) fastened to the tip part (5a) o...
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WO/2015/145359A1 |
Assemblies, apparatus, devices and methods useful in providing lightning protection of avionic components associated with aircraft antennas are disclosed. Aspects of the present disclosure may be used on aircraft comprising structural el...
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WO/2015/145121A1 |
A container (1) comprises a receptacle (2) with an opening (3). In one embodiment, the container (1) is suitable for use on a commercial passenger aircraft as a life vest stowage device. A Radio-Frequency Identification (RFID) tag (24) i...
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WO/2015/142481A1 |
A method can include determining that an aircraft is on approach to a runway. The method can include determining a flight path vector (FPV) location of the aircraft based at least in part on a projected landing location with respect to t...
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WO/2015/138318A1 |
A system and method for displaying standby instrument information is disclosed. The touch-screen instrument panel system for a vehicle has a touch-screen information panel display configured to display vehicle operation information recei...
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WO/2015/138327A1 |
Systems, methods and computer-storage media are provided for a touch-screen interface panel (TSIP) of an aircraft. The TSIP may communicate with one or more aircraft systems. In other words, the TSIP is configured to display information ...
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WO/2015/127856A1 |
An active type bird collision prevention method and device for aircraft; the method comprises: activating a radar detection device (1) to detect whether a flying creature such as a bird approaches a preset danger area of the aircraft, an...
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WO/2015/127630A1 |
An impact protection apparatus (100, 200, 300) is provided, comprising a gas container (110, 210, 310) configured to hold compressed gas and an inflatable member (130, 230, 330) configured to be inflated by the gas and function as an air...
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WO/2015/121624A1 |
The present invention proposes a cap (100) having a collar portion (14) with three or more contact regions arranged to contact the end of a fastener (2, 3, 4) around which the collar portion is provided, the collar portion having a lobed...
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WO/2015/108586A2 |
Provided herein are systems and methods for providing reliable control of an unmanned aerial vehicle (UAV). A system for providing reliable control of the UAV can include a computing device that can execute reliable and unreliable progra...
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WO/2015/108588A2 |
Provided herein are systems and method for autonomously or semi-autonomously landing an unmanned aerial vehicle (UAV) on a landing pad. The landing pad can include features configured to correct misalignment of the UAV on the landing pad...
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WO/2015/097708A1 |
An aircraft part, such as a cockpit or cabin, comprising a support structure and a robot arm (7). The robot arm has a proximal end (10) attached to the support structure and a distal end adapted to hold a electronic device (8). An actuat...
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WO/2015/091390A1 |
There is provided apparatus and a method for assessing the integrity of a bonded joint and a bonded joint assembly. The assembly has a bonded joint monitored for bond integrity and comprises first (1) and second (2) components each defin...
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WO/2015/090525A1 |
A flight data memory module (1) has a data memory device (2) for storing data, a data receiver device (3, 4) for receiving the data and a sheath (8) enclosing the data memory device (2). The sheath (8) has a spherical, ellipsoid, ovoid a...
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WO/2015/090959A1 |
The invention relates to a passenger aircraft (10) comprising a pressurized cabin which has a crown volume (13) and a passenger deck (12), the passenger deck (12) having at least one passenger compartment (14) which is separated from the...
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WO/2015/091794A1 |
A composite structure (10) comprising one or more electrically conductive pathways (12) and one or more isolators for isolating the pathways (12) from the bulk of the structure (10).
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WO/2015/078724A1 |
The present invention relates to an apparatus for determining a mechanical force of an actuator on a movable aircraft component. The apparatus according to the invention comprises a shaft, in particular a solid or hollow shaft, for trans...
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WO/2015/081198A1 |
A propeller blade assembly including a propeller blade having a leading edge, and a trailing edge extending between a tip and a hub, and an electrically conductive band extending longitudinally on either or both of the leading edge and t...
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WO/2015/051057A1 |
A system for active vibration control includes an actuator configured to reduce the impact of a vibratory load imposed on an airframe of a rotorcraft to an amount that is less than a threshold; and a controller configured to determine th...
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WO/2015/037375A1 |
The purpose of the present invention is to provide a landing decision assistance system, a landing decision assistance method, and a landing decision assistance program with which even a general user who is not a specialist can easily an...
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WO/2015/038206A1 |
Systems and methods for reducing the number of runway excursions (i.e., airplanes going off the end of a runway). An alerting system is provided which alerts pilots when computer calculations indicate that current airplane braking is ins...
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WO/2015/034513A1 |
An aircraft including a jet engine including a core having a compressor and combustion chamber, and a particulate sensor located within the core and a particulate detection method for an aircraft having a jet engine where the method incl...
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WO/2015/033742A1 |
An objective of the present invention is to provide an aircraft flight information generation device, an aircraft flight information generation method, and an aircraft flight information generation program, whereby information is generat...
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WO/2015/025130A1 |
A cap for forming a sealed cavity (130) around an end of a fastener (120) protruding from a structure (110). The cap has: a cap body with an annular base (210) terminating at a rim (211) which surrounds an opening into a central cavity (...
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WO/2015/023451A1 |
A conductive insert which provides a low resistance bond between low conductive materials. The insert includes a first surface and an oppositely facing second surface. A plurality of openings extends between the first surface and the sec...
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WO/2015/015153A1 |
The invention proposes a joint (100) comprising a structure (110), a fastener passing through the structure (110) with an end (120) of the fastener protruding from the structure (110), and a cap (140) installed on the end (120) of the fa...
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WO/2015/007957A1 |
The invention concerns a metal attachment for providing an electrically conductive surface through the entire thickness of structural elements to be assembled. The attachment therefore comprises a head (12) and a smooth barrel (12) exten...
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WO/2015/007919A1 |
The invention concerns a metal attachment (10) for providing an electrically conductive surface through the entire thickness of structural elements to be assembled. The attachment therefore comprises a head (12) and a smooth barrel (14) ...
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WO/2015/005125A1 |
This method for producing a reinforcing structure comprises: a step for preparing a stringer that has a fiber exposed surface; a step for arranging a conductive protective material so as to cover at least a part of the fiber exposed surf...
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WO/2015/006171A1 |
A standby flight display system for use on an aircraft is disclosed herein. The aircraft has a primary flight display system that is configured to display a first image on a primary flight display screen. The standby flight display syste...
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WO/2015/005126A1 |
This method for producing a reinforcing structure comprises: a step for preparing a stringer that has a fiber exposed surface; a step for arranging an insulating protective material so as to cover at least a part of the fiber exposed sur...
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WO/2014/207353A1 |
The present disclosure concerns a remote connection system capable of being incorporated into an aircraft (1A, 1B, 1C) comprising at least one motor propeller (50A, 50B, 50C) having a plurality of blades (52A, 52B, 52C) capable of rotati...
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WO/2014/204348A1 |
The utility model relates to protective anti-missile equipment for aircraft. The field of the present invention is the protection of aircraft (passenger, cargo and business planes, and helicopters) from man-portable guided missiles with ...
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WO/2014/195942A1 |
A system for determining a region of interest for an imaging device based on instrument landing system (ILS) is provided herein. The system may include an imaging device attached to an aircraft; an ILS detector; a computer processor conf...
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WO/2014/184722A1 |
The present invention proposes a method of installing a cap (100) to form a sealed cavity (20) around one end of a fastener (300) to thereby contain out-gassing and sparking events in the event of a lightning strike to the fastener (300)...
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WO/2014/171228A1 |
[Problem] To provide a vehicle posture display device capable of displaying the posture and variation in up-down positions of a vehicle in a three-dimensional, easy-to-understand manner. [Solution] A plotter device includes a highway scr...
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WO/2014/172305A1 |
The present disclosure provides methods and articles useful in sealing fasteners, including seal caps and methods of their use, and in particular light weight seal caps having higher dielectric breakdown strength, lower weight, and/or lo...
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WO/2014/172302A1 |
The present disclosure provides methods and articles useful in sealing fasteners, including seal caps and in particular translucent or transparent seals or seal caps. In some embodiments, a seal cap which is optically translucent and opt...
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WO/2014/170672A1 |
The present invention proposes a cap (100) for forming a sealed cavity (12) around one end of a fastener (2-4) to thereby contain out-gassing and sparking events in the event of a lightning strike to the fastener (2-4). The invention als...
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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...
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WO/2014/162032A1 |
The invention relates to a system for indicating the parked state of an aircraft using means belonging to the aircraft, such that personnel can safely approach the aircraft. The system comprises two types of indicator lights disposed on ...
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WO/2014/156369A1 |
The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in a manufacturing process to be reduced, and weight increase...
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WO/2014/156274A1 |
The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in quality management to be reduced, and weight increases to ...
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WO/2014/148963A1 |
The invention relates to a method for joining a first composite structure (la, lb) to at least a second structure (1a, 1b) comprising the steps of: providing a hole in the first composite structure (S100, S200), providing a hole in the a...
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WO/2014/143451A1 |
A multi-member assembly including a first structural member (18), a second structural member (16) opposed from the first structural member, a crossover seal (28) positioned between the first and second structural members, wherein the cro...
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WO/2014/143545A1 |
A method and apparatus for sealing a fastener element. A structure may be positioned over a seal cap that has been adhered and sealed to the fastener element. A number of projections associated with the structure may be moved along an in...
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WO/2014/138574A2 |
Active noise and vibration control (ANVC) systems and methods are provided. The systems and methods include providing sensors configured to detect vibration of a structure and a controller in electrical communication with the sensors. Th...
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WO/2014/131671A1 |
The invention relates to a hand cart (1) for tablet computers (2), wherein the hand cart (1) has a plurality of insert compartments (3) for receiving tablet computers (2). The hand cart (1) comprises at least one network part (4) which i...
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WO/2014/127607A1 |
The present invention provides a visual perception-based airplane landing assisting device. The device acquires a series of runway images, performs tilt angle (γ) correction on the original runway images, and calculates airplane height ...
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