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JP2023082181A |
To provide a telescoping expansible wing system.A telescoping expansible wing system comprises: a first wing section comprising a hollow interior; a second wing section which is attached to a fuselage of an aircraft and configured to be ...
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JP7289954B2 |
A telescoping wing system for a UAV, comprising:a first wing section comprising a substantially hollow interior; anda second wing section configured to be stowed within the interior of the first wing section such that an external surface...
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JP7284828B2 |
A roadable vehicle includes main wings, a fuselage, a sliding door on a lateral side surface of the fuselage, and hinge mechanisms. The hinge mechanisms connect the main wings to the fuselage. The hinge mechanisms allow the main wings to...
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JP7280609B2 |
A control device of this embodiment comprises: an acquisition unit that acquires information indicating the strain of a vane of a structure, and information indicating a control amount of a movable vane of the structure; a first determin...
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JP7280137B2 |
An aircraft (10) includes an aircraft body (30) including a longitudinal axis (31) and a wing box (40) extending through the aircraft body. The aircraft also includes an attachment assembly (100) coupled to the aircraft body and to the w...
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JP2023070092A |
To provide support systems suitable for transfer of large structures.A support system (100) includes a support beam (110) elongated along a longitudinal axis (L). The support beam includes a first end portion (112) longitudinally opposed...
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JP2023070095A |
To provide a method for transporting a workpiece from an initial work cell to a subsequent work cell in a manufacturing environment having a plurality of work cells.The invention relates to a method for transporting a workpiece (50) from...
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JP7274679B2 |
The present disclosure relates to the technical field of air vehicles, and in particular, an air vehicle with a double-layer rotor wing structure, including a cabin in which a power device is arranged, the power device includes a drive a...
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JP7271797B2 |
Systems, devices, and methods including a wing panel; a spar disposed in the wing panel, where the spar comprises: an upper cap; a lower cap; a honeycomb core connected between at least a portion of the upper cap and the lower cap; an in...
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JP7269057B2 |
A wing flap (100) includes a flap body (164) movably couplable to the wing body (258) of an aircraft wing (214), and a torque member (108) couplable to a flap actuator (260) of the aircraft. The torque member (108) is integrally formed w...
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JP7269032B2 |
Described herein is an auxiliary support system for a flap coupled to a wing of an aircraft. The auxiliary support system comprises a base fixable relative to the wing. The auxiliary support system also comprises a first track engagement...
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JP7268112B2 |
A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The...
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JP2023054770A |
To provide a method for reinforcing a junction of fiber-composite aircraft components forming an elongate conduit.The junction-reinforcing method comprises (a) abrading a junction 534, and (b) applying a sealant 558 along the junction 53...
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JP7254347B2 |
A morphing wing includes a pantograph mechanism capable of being extended and contracted in a predetermined direction, a plurality of flight feathers attached to the pantograph mechanism, connection members configured to connect flight f...
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JP2023514546A |
Systems, devices and methods including one or more rib mounting flanges (200a, 200b, 200c, 200d, 200e). Each rib mounting flange has a spar opening (202a) configured to receive the main spar (110) of the wing panel (100) and one or more ...
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JP2023513127A |
The systems, devices and methods include a leading edge tubular member (114), an upper tubular member (110), a lower tubular member (112), and between the leading edge tubular member (114) and the upper tubular member (110). one or more ...
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JP7242197B2 |
A center wing box assembly for an aircraft which includes: a composite lower wing skin, a composite upper wing skin and a composite spar which extends between the composite lower wing skin and the composite upper wing skin. The center wi...
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JP2023035827A |
To provide composite structures used in aircraft, and more specifically, a lightweight control surface exhibiting high residual strength, improved fracture toughness properties, and damage tolerance.A thin, lightweight control surface is...
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JP2023030450A |
To provide a skin member and a vane structure having secured strength while being lightweight.A skin member 100 forming an outer plate of a vane structure includes a framework material 110 having a grid shape and forming a shape of the o...
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JP7232630B2 |
A methodology for designing spoilers or droop panels and aerodynamic systems including the designed spoilers or the designed droop panels are described. In one embodiment, the spoilers and the droop panels can be deployed on a wing with ...
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JP2023028026A |
To provide a drone that is less likely to be subjected to impacts of winds due to a fixed wing at the time of take-off and landing.A drone includes: rotors; a fixed wing capable of being stored; and control means for controlling deployme...
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JP7230100B2 |
A telescoping wing system for a UAV, comprising:a first wing section comprising a substantially hollow interior; anda second wing section configured to be stowed within the interior of the first wing section such that an external surface...
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JP2023026401A |
To provide fuel dams, an aircraft main wing box, an aircraft, and a method for assembling an aircraft main wing.A method for assembling an aircraft main wing 12 includes: fastening fuel dams 100 to stringers 18; and fastening the fuel da...
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JP2023020868A |
To provide hat-stringer assemblies for an aircraft and methods of forming the hat-stringer assemblies.A hat-stringer assembly 100 for an aircraft comprises a hat stringer 110 with a first hat-stringer leg 140, a second hat-stringer leg 1...
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JP2023504967A |
The present invention involves self-adaptive wing systems and aircraft. This is a variable wing for an aircraft and includes a fixed section that forms a lifting wing from the skin, plus vertically offset upper and lower movable sections...
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JP2023504739A |
Systems, apparatus and methods include an unmanned aerial vehicle (UAV) (101), one or more inner wing panels (107) of the UAV, one or more outer wing panels (109) of the UAV, and one or more inner at least one inboard propeller (140) mou...
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JP7214599B2 |
A braking force generation device has: a first mode in which a deflector and a blocker door are retracted with respect to a wing; a third mode in which, while the leading edge and the trailing edge of the deflector are separated from the...
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JP7210526B2 |
There is provided a flight vehicle including: a wing unit; a battery that is arranged in the wing unit; an air intake unit that is formed at a position corresponding to the battery on a front side of the wing unit; a heat sink unit that ...
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JP2023009836A |
To provide a structure of a morphing wing with high flight performance.A morphing wing 140 comprises: a link structure capable of expanding in a first direction and retracting in a second direction, which is opposite to the first directi...
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JP2023009892A |
To provide a flight apparatus that has an excellent flight performance and eliminates the need of high operation skill that requires a user for a long time to become skilled in operation.A flight apparatus 100 includes: a thrust device 1...
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JP7202771B2 |
A composite structure (100) includes a base structure (101), a core (102) disposed on the base structure, the core having a non-uniform contour relative to the base structure, and a layered cover material (104) disposed on the base struc...
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JP7202194B2 |
The construction of a stringer transition through a common base (66) eliminates the need for plate fittings and their associated fasteners to connect opposing ends of a first stringer (84) having a large cross-sectional area to a second ...
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JP2022191765A |
To suppress power consumption of a battery for a flying body while continuing flight of the flying body.A flight control device comprises: a pair of pressure sensors 31 and 31 disposed in a vertical direction on a surface of a flying bod...
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JP7197177B2 |
A multirotor aircraft that includes a chassis, three or more vertical rotors, one or more free wings and on ore more fixed horizontal rotor. The free wing is attached to the chassis by an axial connection so that the angle of the free wi...
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JP7197178B2 |
A multirotor aircraft that includes a chassis, vertical rotors, foldable wings, and a means for deploying and folding the foldable wing. The foldable wing is attached to the chassis and the means for deploying and folding the foldable wi...
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JP7178099B2 |
To provide a flying body that can efficiently and safely transition to level flight from hovering.A flying body 1 includes: lift generation parts 10B, 10T such as a main wing; thrust generating parts 30B, 30T allowing for flight and hove...
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JP7177746B2 |
Provided is a control device that controls a flying body including a double-sided light-receiving solar battery panel provided on a main wing, the control device comprising: a positional relationship acquisition unit that acquires the po...
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JP7177747B2 |
Provided is a control device for controlling an aerial vehicle having a double-sided light receiving type solar cell panel disposed on a main wing, the control device comprising: a positional relationship acquisition unit that acquires t...
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JP7177586B2 |
An end effector (50) provides one up assembly drilling through mated components, including a panel, by preloading the components to assure interface integrity, thus avoiding subsequent separation for cleaning and deburring. The end effec...
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JP7173665B2 |
A vertical take-off and landing aircraft which uses fixed rotors for both VTOL and forward flight operations. The rotors form a synthetic wing and are positioned to achieve a high span efficiency. The rotors are positioned to even out th...
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JP7169753B2 |
An aircraft (10) includes a fuselage (12) having a longitudinal axis (20), a wing assembly(24), and a fuselage positioning mechanism (50) operatively connecting the fuselage to the wing assembly. The fuselage positioning mechanism is ope...
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JP7166777B2 |
A closed-angle composite airfoil spar (210) is provided for an airfoil assembly (200). The composite airfoil spar comprises a web portion (320) having a thickness. The composite airfoil spar (210) also comprises a flange portion (322) ha...
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JP2022544076A |
The present invention relates to a method of field spraying with an unmanned aerial vehicle (UAV). The method includes flying a UAV over crops in a field and spraying the crops with a liquid spray, the UAV having wings extending in a dir...
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JP7153351B2 |
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JP2022152518A |
To provide a jet airplane operation property simulation system in a single-engine propeller airplane that can suppress tendencies of turning that are generated during power operation in a single-engine propeller airplane and gradually ca...
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JP2022151899A |
To provide an aircraft which changes a wing with a large wing width to a small wing width in view of convenience of road transportation or road travel in order to improve flight efficiency.An aircraft comprises a telescopic wing which ca...
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JP2022150610A |
To optimize a lamination order of an anisotropic composite laminate structure while utilizing characteristics of an anisotropic material.A designing method of an anisotropic composite laminate structure, which structures a predetermined ...
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JP7149116B2 |
The purpose of the present invention is to provide an aircraft which comprises a left and right pair of rotors, a rotor disposed on the airframe centerline, and a fixed wing and exhibits excellent airframe stability during vertical takeo...
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JP2022145626A |
To provide a system and method for routing power feeder wires passing through, e.g., an area outboard of a surge fuel tank in an aircraft wing.An electrical pass-through assembly includes a sleeve 32. The sleeve 32 has a connected end 34...
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JP2022142803A |
To provide a wing with no flap and with passively variable camber, and an aircraft having this wing.A wing comprises: a box structure constituting a front edge of the wing; a top face outer plate which is attached to a rear end of a top ...
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