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JPH0387098U |
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JPH0356239B2 |
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JPH0338080Y2 |
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JPH0347240B2 |
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JPH03148598A |
PURPOSE: To improve response of a body, to simultaneously steer steering blades and to improve performance by providing actuators of main wings, front wings and rear wings to be operated upon reception of signals of main wing, front wing...
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JPH03144298A |
PURPOSE: To secure the controlling property of rolling of a missile with a simple structure by a method wherein spoilers in respective stabilizing fins are engaged with one piece of ring while the spoilers are moved out of or into the su...
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JPH03144299A |
PURPOSE: To secure the controlling property of rolling of a missile by a method wherein spoilers in respective stabilizing fins are engaged with one piece of ring and the spoilers are moved out of or into the surfaces of the stabilizing ...
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JPH03129300A |
PURPOSE: To prevent the occurrence of high aerodynamical interference between a front and a rear wing by method wherein, instead of a front wing the steering angle of which is changed, a front wing axially slid by means of a drive device...
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JPH03125900A |
PURPOSE: To obtain the merits of both of fore-wing steering system and rear-wing steering system by a method wherein main wings or fore wings and rear wings are moved forward after the combustion of a rocket motor and control signals for...
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JPH03125696A |
PURPOSE: To shorten the ground run at the time of take-off and landing of an airplane by providing a wind receiving wing rotated upward at the time of take-off and landing of the airplane above a main wing, and providing an auxiliary win...
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JPH0316319B2 |
This invention relates to a tandem or multi-winged aircraft wherein a primary wing system is so designed and equipped that it is capable of being actuated in a manner to bring about a shift in the neutral point of the craft relative to i...
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JPH0338499A |
PURPOSE: To improve the operationability and stability largely by providing a drive means to change an elevation angle of a main wing based on at least one of a speed, acceleration, altitude, and weight of an aircraft detected by detecto...
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JPH035199Y2 |
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JPH034440B2 |
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JPH037696A |
PURPOSE: To provide stable sideways maneuverability even during flying with a high angle of elevation by allowing the left and right ends of the main wing to work as wing end rudder faces which their angles of elevation changeable indepe...
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JPH0254279B2 |
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JPH02242100A |
PURPOSE: To obtain a guided missile, quick in the responding property and excellent in the turning performance as well as the flying range thereof, by a method wherein main wings are attached to a cylindrical shell, connected to a fusela...
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JPH02223798A |
PURPOSE: To permit the securing of roll control property without using any space near the central part of the axle of a missile by a method wherein the missile is constituted so that respective stabilizing fins are connected through link...
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JPH02223800A |
PURPOSE: To permit the securing of merits of both of fore wing steering system or rear wing steering system by a method wherein the rear wing is moved forward after igniting a rocket motor to improve the responding property of a fuselage...
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JPH02223799A |
PURPOSE: To permit the securing of roll control property without using any space near the central axle of a missile by a method wherein respective stabilizing fins are connected through link coupling employing a ring while the steering f...
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JPH02100099U |
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JPH0234838B2 |
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JPH02166400A |
PURPOSE: To attempt to make a plurality of rear stabilizing wings take roll- hunting angle without using the space near the central shaft of a missile in which a rocket motor lies by the constitution that a drive device is controlled by ...
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JPH02161294A |
PURPOSE: To improve the response of a guided missile body, to simultaneously steer both wings and to obtain both advantages of both a front wing steering system and a rear wing steering system by moving the front wing forward after a roc...
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JPH02136399A |
PURPOSE: To improve the space efficiency and prevent the collapse of the balance of an airframe at the time of deployment/folding by providing a cylindrical storage chamber on the center-or-gravity line of the airframe inside a flying ob...
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JPH0259316U |
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JPH02114091A |
PURPOSE: To facilitate checking by forming a box beam such as a wing flap track beam for an aircraft by a single molding work into one structure body, and reducing the number of parts. CONSTITUTION: A flap track beam 32 to be attached to...
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JPH0228999U |
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JPH024199A |
PURPOSE: To achieve the remarkable reduction of an air resistance without deteriorating the maneuverability of a missile by providing steering wings, capable of being advanced and/or retreated into and/or out of a fuselage, and an actuat...
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JPH01306394A |
PURPOSE:To facilitate the enforcement of directional stability and the prevention of approach to a dangerous range when a fault is caused by providing a pentral fin as a newly added steering face in the rear of the center of gravity and ...
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JPH01300199A |
PURPOSE: To eliminate the affection of fins to rolling of a fuselage and improve the guiding accuracy of a guided missile by a method wherein a plurality of fins on the central part of the fuselage are linked and constituted so that resp...
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JPH01300198A |
PURPOSE: To operate actuators simultaneously and improve the performance of a guided missile by a method wherein one part of a rear wing is separated after the combustion of a rocket motor while a control signal from a controller is sent...
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JPH01300200A |
PURPOSE: To reduce a hinge moment upon steering by a method wherein an extendable streamer shaft is extended so as to be coupled with a streamer bearing when a missible is operated as a streamer while an extendable steering shaft is exte...
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JPH01297391A |
PURPOSE:To facilitate the advance direction control of a navigation body by accommodating a rotary body whose one part is projected from the body into the top edge of the body of the flying navigation body which is equipped with a thrust...
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JPH01289799A |
PURPOSE:To enable the twisting angle of a wing to be changed to an optimum value by providing a rudder face capable of producing an aerodynamic force in the up-and- down direction in accordance with the steering angle, at least on one si...
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JPH01285490A |
PURPOSE:To reduce weight and resistance in comparison with the addition of a new operating air control face and to attain a compact airplane by opening the wheel well door of the airplane during a flight fixing with a vertically pendent ...
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JPH01278899A |
PURPOSE:To maintain an atmospheric pressure differential between both upper and lower surfaces of a rudder plane as well as to increase the extent of steerability by installing a plate body for filling up a clearance between a rudder mou...
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JPH01157998U |
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JPH01266094A |
PURPOSE:To achieve the enhancement in an aerodynamic performance by providing horizontal canards which are provided on both right and left sides of an aircraft body and which can be operated in such a way that the fitting angles to the b...
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JPH01151096U |
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JPH01260299A |
PURPOSE: To improve response property in motion, by operating the fore wing and the rear wing of a missile independently respectively to control the missile so as not to generate the rotating motion of the body thereof. CONSTITUTION: A m...
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JPH01149892U |
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JPH01257693A |
PURPOSE:To improve the operation ability of an aircraft at takeoff and landing by operating an emergency trim system in the trim controller, of the aircraft simultaneously with a regular trim system only at takeoff and landing, so as to ...
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JPH01254490A |
PURPOSE:To compensate a steering system for a deficiency in the pitching moment generating capacity, by providing an actuator which is connected to a flight computer and is capable of driving upper and lower speed brakes. CONSTITUTION:A ...
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JPH01111998U |
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JPH01111999U |
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JPH01106798U |
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JPH01106795U |
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JPH01106797U |
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JPH01106796U |
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