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JPH01168596A |
PURPOSE:To enhance the extent of maneuvering performance in vertical, cross and diagonal directions of aircraft by attaching a stabilizer and a rudder 4 to a cylinder whose roll angle is free of alteration. CONSTITUTION:A rudder 4 is mad...
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JPH01168595A |
PURPOSE:To enhance the extent of maneuvering performance in vertical, cross and diagonal directions of aircraft as well as to lighten the load added to a fuselage of the aircraft by installing a wing, whose elevation angle is free of alt...
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JPH01137198A |
PURPOSE: To achieve a speedy response and a high trim angle by developing a front wing after rocket motor combustion, sending the control signal of one control device to the actuator of two kinds of steering wings, namely front and rear ...
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JPH01137197A |
PURPOSE: To reduce a hinge moment on steering, by extending an extension streamer shaft and connecting it to a streamer bearing on streaming and extending the extension steering shaft, and connecting it to a steering bearing on steering ...
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JPH01137196A |
PURPOSE: To prevent guiding accuracy from deteriorating, by allowing each stable steering to perform similar steering in a link and hence eliminating a roll moment as the entire stable wing. CONSTITUTION: One portion of a ring 5 becomes ...
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JPH01137194A |
PURPOSE: To obtain improved lift characteristics, by loading a steering wing inside and outside an airframe body partially or entirely for steering due to the rotation of one portion or entire portion of the steering wing within an axle ...
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JPH0174499U |
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JPS6483494A |
PURPOSE: To achieve shortening of a landing run distance by composing a flap of an aircraft to be operated upward automatically or manually after grounding at the time of landing for generating negative lift downward to improve braking e...
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JPS6467598A |
PURPOSE: To enhance motion performance and aerodynamic stability while preventing mechanical interference with a mother machine by incorporating stabilizer fins in the body of a guided projectile and developing the fins by a torsional to...
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JPS6467495A |
PURPOSE: To improve reliability of a structure by composing an actuation means for a flap member contained and supported in a trailing edge part of an aircraft wing through a specific link means of a lever arm connected to a rotation act...
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JPS6457098A |
PURPOSE: To provide a device which lightens the hinge moment at steering of a steering wing, by providing a steering gear with a steering shaft, which has an extensive steering shaft, and an extensive drifting shaft within a guiding cont...
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JPS6457100A |
PURPOSE: To get large lift, enough motion performance, and aerodynamic stability, by providing a guided air frame with a developed stabilizing wing with enough wing area, a development steering wing, a tensile spring to develop these, it...
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JPS647920B2 |
A trailing edge flap moveable from a stowed position behind a wing to a downwardly and rearwardly extending position to deflect jet exhaust from an upper surface blowing jet engine downwardly and rearwardly to augment lift. The actuating...
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JPS63315899A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63312299A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS6363424B2 |
A compensator is disclosed for centering a frame supported steerable member comprising part of the steering system for a vehicle. The compensator is connected between the frame and the steering system and comprises a cylinder containing ...
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JPS63287694A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63251397A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63240495A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63145797U |
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JPS63142600U |
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JPS63215498A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63119200U |
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JPS63177000A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63176995A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS6335480B2 |
A carrying wing having a movable flap, an outer skin of plastics formed continuously without gap from the carrying wing surface to the flap surface, the skin being designed as a thin flexible membrane spanning the transition zone between...
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JPS63108897U |
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JPS63163799A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63163798A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63154497A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63132000A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS6325999B2 |
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JPS63121599A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS6324879B2 |
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JPS63501239A |
A coupling mechanism for quick attach/disconnect of a control fin to a missile which does not require the use of a separate tool to make the attachment. A first coupling member 24 is mounted on the control fin actuator rod 16. A force re...
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JPS6361699U |
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JPS6368494A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS635319B2 |
A hinge arrangement between a lifting foil and a flap. The flap comprises a plurality of sections. Each section is mounted by one coupling restraining hinge device to the foil, the hinge device has a hinge pin that extends into a socket ...
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JPS632795A |
This invention relates to a system for controlling an aerodynamic surface mounted mobile on an aircraft so as to be able to pivot freely about a fixed axis and provided with a tab itself articulated on the trailing edge of the aerodynami...
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JPS62201202U |
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JPS62199402U |
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JPS6249239B2 |
A helicopter stabilator having naturally high response to the main rotor wake excitation frequency in roll and yaw stabilator vibratory modes is selectively mounted so as to be detuned therefrom in antisymmetric stabilator vibratory mode...
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JPS6243918B2 |
PCT No. PCT/JP82/00459 Sec. 371 Date Aug. 3, 1983 Sec. 102(e) Date Aug. 3, 1983 PCT Filed Dec. 2, 1982 PCT Pub. No. WO83/01933 PCT Pub. Date Jun. 9, 1983.An expansion type life-saving raft, in which the life saving raft is folded with th...
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JPS62145900U |
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JPS62182599A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS62173398A |
An aircraft wing with a trailing edge flap and a flap-supporting system toward each end of the flap. The flap-supporting systems are completely housed within the wing of the aircraft when the flap is in its stowed or retracted position. ...
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JPS62119000U |
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JPS62118999U |
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JPS62157895A |
An aircraft leading edge slat (11) is biased when at an extended location toward a first position wherein the trailing edge (19) of the slat is a predetermined distance from the wing upper surface. The slat is pivotable to a second posit...
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JPS62157896A |
A leading edge wing slat having a movable nose portion (11) wherein the nose portion leading edge moves relative to the slat frame (12) in a downward and rearward direction when the slat is extended. This causes an intermediate flexible ...
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