| Document |
Document Title |
|
JPH11348894A |
To provide a full wing aircraft which can make a wing surface integrally-formed with an airframe serves as a steering surface controlling the attitude of an aircraft. This full wing aircraft consists of a central part 2 which is disposed...
|
|
JP2963382B2 |
To prevent a load from being applied to a structure as moment when braking force is applied to a brake disk by providing a bracket extended in the advancing direction of a moving body from part of a hinge member supporting the brake disk...
|
|
JPH11509804A |
PCT No. PCT/GB97/00979 Sec. 371 Date Dec. 2, 1997 Sec. 102(e) Date Dec. 2, 1997 PCT Filed Apr. 9, 1997 PCT Pub. No. WO97/38900 PCT Pub. Date Oct. 23, 1997The present invention relates to a variable camber wing mechanism. The mechanism in...
|
|
JP2889501B2 |
|
|
JPH1170898A |
To realize high efficiency, and simplify the constitution by eliminating a tail rotor out of a single rotor helicopter. In this tail rotorless, single rotor helicopter, a variable flow straightening wing 1 is provided underneath a main r...
|
|
JPH10324299A |
To prevent both wings from causing left-right-unbalanced operation, by connecting the outer end of a link arm with two matched mobile wing surfaces of both wings, interconnecting their inner ends, and operating the matched mobile wing su...
|
|
JP2719674B2 |
PURPOSE: To enhance a hitting accuracy by coping with demands for reductions in the size, weight and cost, and controlling (roughly) damping (convergence degree) of a body in lateral directions while correcting a time delay, an error, et...
|
|
JP2709559B2 |
PURPOSE: To enhance a steering accuracy and to improve a space efficiency as an entire missile by providing a torque motor in the direction perpendicular to an axial direction of the airframe, and coaxially coupling a steering shaft of a...
|
|
JPH1016890A |
To provide an expansion aerodynamic surface for forming a lifting surface by expanding a plate-like small wing from both gunwales of the body of an airplane and using this also as a steering wing or a brake. An expansion aerodynamic surf...
|
|
JP2669783B2 |
PURPOSE: To improve a flight characteristic by using a flexible band wing in a vehicle such as a missile, and prevent the flexible band wing from negatively affecting control ability. CONSTITUTION: A vehicle includes a streamlined missil...
|
|
JPH09267799A |
To provide an articulated aerodynamic steering surface for providing a plurality of machine functions by one articulated aerodynamic steering surface. An articulated aerodynamic steering surface is composed of a first steering surface 21...
|
|
JPH09257398A |
To reduce air resistance upon straight flying by providing a shape memory alloy so as to partly cover a head surface of a flying structure, the shape memory alloy being changed so as to protrude to the outside of the flying structure wit...
|
|
JP2646239B2 |
|
|
JP2622670B2 |
PURPOSE: To provide vortex drag reduction effect which is equal to that obtained when a wing end is extended, reduce induced drag, and increase lift/ drag ratio without extending an end of a wing which is thin and long vertically and uni...
|
|
JP2605696B2 |
|
|
JP2605698B2 |
|
|
JPH0986498A |
To provide a control device for an aircraft to effectively perform control of a yawing moment and control of a speed. A control device for an air craft comprises wings 10 and 11 for two speed brakes integrally rotatable around a common h...
|
|
JP2588739B2 |
|
|
JP2580317B2 |
|
|
JP2524831Y2 |
|
|
JPH0924897A |
To provide a roll control device for an aircraft unrestricted in a position of providing a flap as in case of using an aileron and prevented from the lowering of lift of main wings as in case of using a spoiler. Lift plates 1 movable bet...
|
|
JPH0914376A |
To provide mechanism that can change a radial angle and can change its radius by extending and-contracting motion. Regarding radial angle changeable mechanism, the radial angles of other components are changed by the change of the rotati...
|
|
JPH0911991A |
To generate a high dynamic lift needed for takeoff and landing in jetting a jet stream in the circumferential direction of an outer peripheral sur face of a cylindrical body by providing a shift mechanism to shift the cylindrical body fr...
|
|
JPH092394A |
PURPOSE: To provide roll control of an aircraft which is free from reduction of the lift or reversal of effect without using the air force. CONSTITUTION: A balancing weight 1 is installed between wing spars of right and left main wings 1...
|
|
JPH08276897A |
PURPOSE: To restrain an increase in resistance by retracting a strake in a fuselage when it is not necessary and protrude the strake to operate only when it is necessary. CONSTITUTION: This strake comprises a strake body 3 which is dispo...
|
|
JPH08253197A |
PURPOSE: To rotate the tail unit around an engine exhaust port and control an attitude by combining thrust deflection in an attitude control device of an aircraft. CONSTITUTION: A movable part 1 rotatable around an exhaust nozzle 2 of an...
|
|
JPH08239098A |
PURPOSE: To shorten the gliding distance, and increase the lift force of main wings, and increase loading capacity by equipping an airplane with turnable, tiltable, fixable, and extensible garnered wings, and installing an interlocking d...
|
|
JPH08230793A |
PURPOSE: To provide an aircraft which does not lose the directional steerability even in a large angle of attack by providing a movable outer plate of a body rear part provided openable in the right-to-left direction by a front end hinge...
|
|
JP2505098Y2 |
|
|
JP2501651B2 |
|
|
JPH08504142A |
A rudder device for water-going craft or aircraft, where there is provided in the vessel a cavity (21) which is open to the outside of the vessel. In the cavity there is provided a body (2) which can rotate about an axis (3), which exten...
|
|
JPH0826192A |
PURPOSE: To control the posture of an air frame by regulating a rudder face area for changing the aerodynamic effect of a rudder face if the rudder face of an airplane has any abnormality such as fixation and malfunction in it. CONSTITUT...
|
|
JPH07291192A |
PURPOSE: To delay the stalling of a main wing in case of the large angle of incidence and reduce the flight resistance in the navigation state with the supersonic speed and the transonic speed, by controlling the intensity of a swirl gen...
|
|
JPH07267191A |
PURPOSE: To perform remarkable acceleration of a slot flow, prevent the occurrence of peel of a flow over the upper surface of a flap wing element, and sharply increase the lift of the whole of a main wing. CONSTITUTION: A gap between a ...
|
|
JPH07267190A |
PURPOSE: To supplement a deficiency of direction stabilization in the high angle elevation region of an aircraft having a conventional fixed type ventral fin, increase lateral slide capacity in a region where the capacity is demanded and...
|
|
JPH07251797A |
PURPOSE: To keep the position of an airframe by providing at the nose of the aircraft a movable control board which is longitudinally movable and which when in a forwardly projected position generates pitching moments in a direction for ...
|
|
JPH07223593A |
PURPOSE: To provide a vortex flap for generating a high lift by reducing the stream which is directed to the upper surface from the undersurface of a wing, passing through a gap formed at the upstream side flap rear end and the downstrea...
|
|
JPH0733999Y2 |
|
|
JPH0733998Y2 |
|
|
JPH0762466B2 |
An aircraft speedbrake is integrated into a jet engine exhaust nozzle. A first set of nozzle flaps which are normally out of the airstream, are extended into the airstream to create drag on the airframe and thereby act as speedbrakes. A ...
|
|
JPH07132891A |
PURPOSE: To facilitate a change between a cruising condition and a high-lift condition by providing either of a frontal line slat or a leading-edge Krueger flap formed on the front of a wing leading-edge part made into an adhesive stream...
|
|
JPH0711359Y2 |
|
|
JPH0710088A |
PURPOSE: To provide an aircraft which can fly with high lift during the taking- off and landing on the ground (or water). CONSTITUTION: An aircraft is provided with main wings 22, a vertical tail 23, and horizontal ailerons 24 provided f...
|
|
JPH06321189A |
PURPOSE: To provide a lift variable device which solves a trouble such that airframe strength must be designed in a speed area where respective lift bearing ratios of the main wing, tail plane and body bearing the lift of an aircraft are...
|
|
JPH0690000B2 |
|
|
JPH06257999A |
PURPOSE: To improve a steering accuracy and fluttering resistance by eliminating looseness of rotation of steering wings in a guided missile in which the wings are operated to be mounted and removed in a short time. CONSTITUTION: A guide...
|
|
JPH06255589A |
PURPOSE: To secure the directional stability and safety of an aircraft by forming the side face shape of a vertical tail approximately into L-shape, and protruding the longitudinal side of the L-shape onto the airframe during normal flig...
|
|
JPH06213598A |
PURPOSE: To eliminate a looseness in rotation of a steering wing and improve an accuracy of the steering wing and anti-flattering characteristic in a guided missile in which the steering wing is fixed or removed within a short period of ...
|
|
JPH06171597A |
PURPOSE: To provide an aircraft to perform vertical taking-off and landing, reduce an airport facility cost, and perform high-efficient air transportation. CONSTITUTION: A vertical type vertical engine 6 is arranged in a fuselage 5, a tu...
|
|
JPH0619999Y2 |
|
