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Matches 951 - 1,000 out of 1,466

Document Document Title
JP5728688B2  
JP5711252B2  
JP5676824B2  
JP5666431B2  
JP2015006875A
To provide a method that enables precise positioning of a vertical takeoff and landing (VTOL) aircraft before the gimbal can even be used when the line of sight has a tunnel effect, such as a view through trees into a window.A method com...  
JP2015000716A
To provide a vehicle capable of flying in vertical and lateral directions in air without causing generation of wind at its surroundings and having less possibility of accidents.Overlapped wings 3 are attached to inside of a bottomed cyli...  
JP2014240242A
To enable attitude control to be performed easily and quickly in a flight vehicle (multicopter) with plural multiblade rotors (propellers).A vertical take-off and landing flight vehicle comprises: a plurality of inner rotor units (RU11-R...  
JP2014231253A
To provide a QTW craft that solves the problem of a stable flight by obtaining a total integration of technologies including the constitution of a flight control system and the loading of a flight control rule that cope with an item with...  
JP2014223846A
To provide a vertical take-off and landing aircraft capable of gliding even when losing thrust power while suppressing increase in size of an airframe.A vertical take-off and landing aircraft comprises: propellers 2 generating lifting po...  
JP5633799B2  
JP2014531362A
The present invention catches a crew member (1) and relates to a propulsive engine (10) provided with a main part (11) designed to connect with a promotion unit (12a, 12b, 13a, 13b) to which pressurized fluid was supplied from a pressuri...  
JP2014218105A
To provide an aircraft which enables low-speed flight by using wings that gain sufficient lift and is not affected by cross wind even in low-speed flight.Sub-fuselages 12 are arranged in parallel on both sides of a main fuselage 1. A fro...  
JP2014213846A
To reduce a defect of causing wind blast damage to the periphery or generating remarkable noise upon takeoff and landing, such as of a helicopter as a vertical takeoff and landing vehicle based on a new fluid dynamic principle, and achie...  
JP2014169064A
To provide "a vertical take-off and landing plane based on new fluid mechanics principles" that achieves "improving defects such as causing wind pressure damage in the periphery and generating remarkable noise in the takeoff and landing ...  
JP5580552B2  
JP2014520726A
It is safe, quietness and control are easy, and efficient and compact airplane composition is enabled by the combination of a plurality of perpendicular lift rotors, tandem wings, and a front thrust propeller. A perpendicular lift rotor ...  
JP2014144702A
To provide a vertical takeoff/landing aircraft improved in controllability while restraining addition of a control mechanism.A vertical takeoff/landing aircraft incudes: a propeller 2 which generates lift force and thrust force; a main f...  
JP2014142828A
To secure safety for a third party by making a tracking movement so as not to move outside a movable space.Position of a mobile object and self position are estimated, a plurality of movement candidate positions are set in surrounding po...  
JP5549020B2  
JP5549019B2  
JP5550930B2  
JP5538409B2  
JP3191468U
[Subject] A flown type body using a principle of reaction flight promotion which difficult flight training cannot be needed, either, but anyone can control easily, and can carry out lifesaving and fire fighting also to emergencies, such ...  
JP5524970B2  
JP5510843B2  
JP5512612B2  
JP5510872B2  
JP5504403B2  
JP5506369B2  
JP5485975B2  
JP5480533B2  
JP2014065321A
To provide an apparatus that includes improvement means for a variety of pieces of existing equipment for performing vertical short-distance takeoff/landing of a fixed-wing and fixed-engine ship-based aircraft and a variety of V/STOL air...  
JP5421503B2  
JP5378065B2
Electronic equipment frequently requires cooling to maintain the integrity and reliability of the equipment, and to elongate the life expectancy of the equipment. When in operation, the fan (5,6) of a UAV creates airflow comprising outsi...  
JP2013248968A
To widely provide reusable-type space coming-and-going aircraft applying vertical takeoff and landing aircraft, which do not require a special high-performance (high-cost) engine and the like, and a part of a vertical flight system of a ...  
JP5335618B2
A strut support system for a ducted fan unmanned aerial vehicle (12) to suppress noise comprising: a ducted fan fuselage (14) that defines an opening (42); an engine that extends longitudinally through the opening in the fuselage; a driv...  
JP2013203334A
To easily estimate a magnitude of an available torque from limited engine performance parameters in real time regardless of a rapid change in engine performance.In a torque estimation apparatus 12 for a helicopter 10, a measuring point t...  
JP2013193510A
To provide a holonomic floating mobile body, the total thrust vector of which can be controlled with high precision.A floating moving body A operated in gravity includes a machine body M, and six or more thrusters Si (in Fig.1, i=1, 2 to...  
JP2013189104A
To provide a vertical takeoff/landing aircraft capable of performing thrust control with a simple structure and of achieving safe taking off and landing in a narrow space where an obstacle is present.A vertical takeoff/landing aircraft i...  
JP2013189036A
To provide a lightweight flying object for measuring having superior flying stability in which a fuselage or various kinds of devices mounted to the fuselage are hardly damaged even if an flying object crashes on the ground, especially w...  
JP2013533823A
An existing bottom-adjustable propeller-type flying object requires a device having a complex structure constructed through the combination of various components such as a servo, a control plate, and a hinge to control the rotor pitch at...  
JP5277342B1
[Subject] In the vertical take-off and landing aircraft which turns the surface of revolution of a rotor under the wing, makes take-off and landing perpendicularly, turns the surface of revolution of a rotor behind a wing, and moves forw...  
JP2013532601A
A safe, quiet, easy to control, efficient, and compact aircraft configuration is enabled through the combination of multiple vertical lift rotors, tandem wings, and forward thrust propellers. The vertical lift rotors, in combination with...  
JP5252973B2  
JP2013530096A
An aircraft hover system for enabling an aircraft to hover at a target spatial location represented by GPS location coordinates. The hover system includes a display screen rendering a display including live video feed of the terrain belo...  
JP2013129301A
To solve a problem in a conventional small unmanned aircraft, wherein a flight operation for long hours is difficult, although having superior flight performance peculiar to a rotor craft.In a small unmanned aircraft V, drive parts 1 gen...  
JP5224823B2  
JP2013527364A
It is a system for increasing a thrust of Hwang with a duct, and this system is provided with a circumference ejector which has an inner side Cowl member (107) and an outside Cowl member (101). With addition of an actuator (111) attached...  
JP5211381B2  
JP2013107626A
To provide a method and apparatus for controlling an unmanned air vehicle (UAV) that includes a plurality of independently controllable control vanes.Control vane position commands are supplied that will move each of the control vanes to...  

Matches 951 - 1,000 out of 1,466