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Matches 1 - 50 out of 54,896

Document Document Title
WO/2017/007710A1
Embodiments of the present invention provide systems and methods for disposal of liquid and food into a sink basin (12). The disclosed system cooperates with and delivers the received waste material to the main waste system on-board the ...  
WO/2017/005607A1
A flow body (2) for a vehicle comprises at least one planar skin section (4) with an outer side (8), an inner side (16) and at least one opening (10) that penetrates the skin section, as well as at least one active flow control device (1...  
WO/2017/007915A1
An aircraft is provided that is convertible in flight between a rotary wing configuration and a fixed wing configuration. In its fixed wing configuration the aircraft resembles a Blended Wing Body (BWB) having a swept wing angle β. Conv...  
WO/2017/005997A2
The invention relates to a reduction gear (11) having an epicyclic gear train for a turbine engine (1), in particular of an aircraft, comprising: a planetary shaft (15) having an axis of rotation A; a ring gear (19) having an axis A exte...  
WO/2017/006421A1
In the present invention, a drone 1 carrying baggage takes off from a takeoff device 11, and travels to a user's home 20, which is the delivery destination of the baggage, using a GPS system. When the drone 1 approaches the user's home w...  
WO/2017/005259A1
The invention relates to a decentralized seat control system (1) for seats (2), comprising multiple seat elements which can be moved linearly or angularly relative to one another and which can be adjusted by intelligent devices (4 to 9),...  
WO/2017/006655A1
Many types of tailless airplanes which are triangular in planar view have been disclosed, but all of these are exclusively suited to high-speed flight; in contrast, the purpose of the present invention is to provide a tailless airplane w...  
WO/2017/004826A1
An anti-fall and anti-drift unmanned aerial vehicle comprises an unmanned aerial vehicle body (1). At least one rotor (10) is disposed on the unmanned aerial vehicle body (1). Wings (3) are respectively disposed on the left side and the ...  
WO/2017/005737A1
The invention relates to a system for dual management of anti-icing and boundary layer suction for an aerofoil (4) of an aircraft, including: at least one anti-icing channel (44) and at least one suction channel (46); a device (26) for m...  
WO/2017/008015A1
An aircraft passenger restraint and protection system including an aircraft seat (22) mounted at an oblique angle to a direction of forward travel, a multi-point seat belt (36) associated with the aircraft seat (22), and a structural mou...  
WO/2017/007345A1
A joining member having a first portion with a first base, a first base wall, a plurality of first extensions, a first locking tip at a distal end of each of the plurality of first extensions, and at least one stop member. A second porti...  
WO/2017/006738A1
Provided is a mounting jig for positioning a plate-like structural member (200) having a pair of positioning holes (220) formed at the opposite ends thereof. The mounting jig is provided with: a support section (110) for supporting the l...  
WO/2017/006064A1
The invention relates to a device for electrical connection (2) intended to connect a superinsulating blanket to a structural panel of a spacecraft, said connection device (2) comprising: - a conducting sleeve (12) having an axis (A‑A)...  
WO/2017/007077A1
In an embodiment of the present invention, disclosed is a monitoring method. A monitoring method according to one embodiment of the present invention comprises: an event generation area detection step for detecting an event generation ar...  
WO/2017/007524A1
A pneumatic artificial muscle (PAM) actuator (100) includes first and second end caps (102-104), an elastic bladder (106) connected to the end caps, and a covering (108) around the elastic bladder and connected to the end caps. At least ...  
WO/2017/007045A1
The present invention relates to a drone capable of wirelessly communicating with a mobile terminal, the mobile terminal, and a control method for the drone and the mobile terminal. The drone according to one embodiment of the present in...  
WO/2017/007456A1
A monitoring system may include a semi-autonomous mobile monitoring device capable of determining whether it has a sufficient power level to perform a monitoring task based on the distance between the position of the mobile monitoring de...  
WO/2017/007304A1
The present invention relates to a variable gap cover for an aircraft, mould assembly for forming such a cover and a method for manufacturing a variable gap cover. The gap is present between a first vehicle part and a second vehicle part...  
WO/2017/007549A1
A latch assembly (110) can include a latch rail (314), a latch body (312), and a biasing mechanism (322). The latch rail can include a first end (318) and a second end. The first end can couple to a back portion of a seat that includes a...  
WO/2017/001977A1
The present invention belongs to the fields of sound-proofing structures for aircraft, typically provided in airports or other infrastructures for aircraft. In order to test and service an aircraft, it must be placed in outdoors conditio...  
WO/2017/004328A1
The present disclosure includes a hardened tablet for use within an aircraft cabin, the hardened tablet including a processor, a touch screen, a memory, a tablet and a protective layer applied to the touch screen of the tablet, the prote...  
WO/2017/003391A1
The present invention is a passenger seat (13) seating group (14) having seat cushion foam (2) and carrier pipes (1 ), to which said seat cushion foam (2) is fixed, and a chassis (15), wherein it further comprises a carrier profile (8) w...  
WO/2017/000299A1
Disclosed are a limit device (10) and an unmanned aerial vehicle (100) having the limit device (10). The limit device (10) is used to connect a gimbal platform (23) and comprises: a fixed assembly (11) and a rotating member (12), wherein...  
WO/2017/002055A2  
WO/2017/002298A1
The screen device of the present disclosure is provided with: a screen that has a plurality of photoelectric conversion elements and that receives video light from a video projection device; a power supply unit that supplies electric pow...  
WO/2017/000156A1
A double-blade tandem helicopter comprises a helicopter body (10), a power system, a control system, and two groups of rotors (30, 50). The two groups of rotors are vertically disposed relative to the helicopter body. Each group of rotor...  
WO/2017/003542A2
The present invention is directed to a solar-powered aircraft comprising a fixed wing panel, a motor driven propeller, a plurality of secondary wing panels, and a tail assembly having a first tail panel and a second tail panel. Each seco...  
WO/2017/001158A1
The invention relates to an inset light having a closure assembly, comprising a housing, which has a supporting surface, and comprising a lighting module, which can be inserted into the housing and has at least one light source and a lig...  
WO/2017/000528A1
A driving device assembly including multiple driving devices (05) and an aircraft. The driving devices (05) are triangularly arranged to form a triangular driving device module (01). The combination method is that the spatial distances b...  
WO/2017/004542A1
Passageway including a section that is extendable and retractable, the section including a frame, slide track assemblies, and scissor bar assembly. The frame has upright members. The slide track assemblies are disposed proximately to res...  
WO/2017/000876A1
Provided are a geo-location or navigation camera, and an aircraft and a navigation method therefor. The geo-location or navigation camera comprises an image capturing apparatus (15), a capturing direction of the image capturing apparatus...  
WO/2017/001411A1
A method and system (60) for generating emergency power includes a hydrogen storage system (62) configured to supply hydrogen gas, an air delivery system (64) configured to supply air at a predetermined temperature, and a fuel cell syste...  
WO/2017/001400A1
The invention relates mainly to an aircraft seat attachment (10) which comprises: a body (11) fastened to an aircraft seat leg (12); at least one stud (13) secured to said body (11); and a plunger (16) mounted so as to be translatably mo...  
WO/2017/003671A1
A latching mechanism is provided for engaging an aircraft surface panel to a support member. The aircraft panel is provided with a post extending from the lower surface, which extends through a panel support member into a post engagement...  
WO/2017/001160A1
A flush-type light comprising at least two light-exit channels arranged oriented along a common main emission direction, comprising a plurality of lighting modules, assigned to the light-exit channels, comprising at least one light sourc...  
WO/2017/001792A1
The invention relates to: laminated glazing (1) including a first structural ply (4) attached to a first sheet of glass (2) of 0.5 to 1.5 mm in thickness by means of a first adhesive interlayer (3), said first sheet of glass (2) making u...  
WO/2017/001845A1
An aircraft passenger seat comprises a seat back and a seat pan, the seat pan being pivotally connected at or around a forward end thereof to a seat frame at a first pivot point, and at or around a rearward end thereof to a lower end of ...  
WO/2017/003814A1
An aircraft overhead stowage system for a cross-aisle galley complex. The aircraft overhead stowage system includes a stowage compartment housing disposed above a ceiling of the galley complex that is supported above the ceiling by a sto...  
WO/2017/001984A1
An aircraft comprises an aircraft structure, a flight control surface attached to the aircraft structure, and a local hydraulic power pack disposed proximal to the flight control surface. The local hydraulic power pack is configured to p...  
WO/2017/002054A1
The present invention provides a stiff in-plane and/or soft in-plane rotor head for a rotorcraft. The invention includes a vertically extending rotor shaft, a center hub disposed on the rotor shaft for conjoint rotation therewith, and a ...  
WO/2017/000304A1
An unmanned aerial vehicle (100), a control system for an unmanned aerial vehicle, a control method for an unmanned aerial vehicle, and a landing control method for an unmanned aerial vehicle. The unmanned aerial vehicle (100) comprises ...  
WO/2017/003447A1
A catalytic thruster includes a reaction chamber that extends between first and second opposed chamber ends. The first chamber end includes a thermal standoff cup. There is a catalyst bed in the reaction chamber, and a feed tube extends ...  
WO/2017/001898A1
The present invention relates to a mission grip system (1) which enables the pilot/copilot to control the critical mission equipment in aircrafts simultaneously, and basically comprises a pilot mission grip (2); a copilot left hand missi...  
WO/2016/209334A2
A multirotor flying vehicle including at least one rotor support frame organized on a geometric grid, with a plurality of rotor assemblies coupled to the at least one rotor support frame. At least one power supply is coupled to and power...  
WO/2016/205932A1
An auxiliary power unit for an aircraft, having a compressor, an intercooler including first conduit(s) having an inlet in fluid communication with the compressor outlet and second conduit(s) configured for circulation of a coolant there...  
WO/2016/210265A1
An adaptive landing gear assembly for a rotary wing aircraft, the adaptive landing gear assembly including a controller; a first landing gear support having a first ground contact element; and a second landing gear support having a secon...  
WO/2016/207622A1
A system comprising: a low observable aircraft (2) having its external surfaces oriented at a limited number of directions; a device (12) mounted to the aircraft (2) outside the external surfaces of the aircraft (2); and a fairing (10) l...  
WO/2016/210355A1
A mounting arm assembly movable between stowed and deployed configurations, includes a pivot arm pivotally engaging an armrest of a seat; a tilt arm engaging the pivot arm; and a mount engaging the tilt arm for supporting a personal elec...  
WO/2016/210432A1
The present disclosure is directed to robotic systems, unmanned aerial vehicles in particular, and various systems and improvements within the field of robotics. Specifically, the present disclosure includes advancements in unmanned vehi...  
WO/2016/205931A1
A compound engine assembly for use as an auxiliary power unit for an aircraft and including an engine core with internal combustion engine(s), a compressor having an outlet in fluid communication with an engine core inlet, a bleed condui...  

Matches 1 - 50 out of 54,896