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JPS62155198A |
A system for coupling together two flaps of an aircraft wing, which flaps are adjacent and are situated at least substantially in the extension of each other. Each flap has its own pivoting and drive means. The system includes a mechanic...
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JPS6224640Y2 |
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JPS62128873A |
PURPOSE:To make it possible to deflect the propelling air flow broadly, and to improve the turning property, by furnishing an auxiliary rudder plate to a main rudder plate. CONSTITUTION:The steering gear 10 consists of a main rudder plat...
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JPS62999U |
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JPS621000U |
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JPS61125899U |
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JPS61161400A |
(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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JPS61110459U |
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JPS61149798A |
(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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JPS61101078U |
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JPS61101300U |
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JPS61122499A |
A pivot or bearing arrangement for the pivotable control surface of a guidable missile, especially a projectile which can be fired through the intermediary of the gas pressure generated by a propellant charge. The pivot bearing includes ...
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JPS6184099U |
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JPS61105332A |
A plurality of substantially axially aligned gear trains (10 - 12) each has an input sun gear (13) and two output ring gears (15 and 16 or 17), the output ring gears being relatively rotatable in response to rotation of the sun gear (13)...
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JPS6154396A |
PURPOSE:To obtain sufficient efficiency of a rudder when a large rudder angle is taken in high speed sailing by making one of a pair of rudeers which is on the outside of turning take a rudder angle smaller than set rudder angle. CONSTIT...
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JPS6113198U |
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JPS618800U |
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JPS6050636B2 |
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JPS60157400U |
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JPS6047156B2 |
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JPS60193794A |
(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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JPS60111898U |
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JPS6078300A |
(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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JPS6013756Y2 |
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JPS6012799Y2 |
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JPS6012280B2 |
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JPS606400Y2 |
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JPS6022597A |
(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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JPS6015295A |
(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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JPS5945558B2 |
Tailoring the contour and chord length of a variable camber leading edge flap for the tapered wing of an aircraft is aimed at improving the aircraft's low speed performance particularly for takeoff and landing. Each segment of a spanwise...
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JPS59102659A |
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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JPS5984696A |
To reduce buffeting caused by separation on the wings of an aircraft, a parameter representing the buffeting in amplitude, frequency and phase is measured. The measuring signal is subjected to filtering intended to establish the characte...
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JPS5973396A |
(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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JPS5953299A |
(57)【要約】 本公報は電子出願前の出願データであるため
要約のデータは記録されません。
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JPS599399B2 |
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JPS58209699A |
(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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JPS5853639B2 |
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JPS5849599A |
(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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JPS5813398B2 |
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JPS5813397B2 |
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JPS5836795A |
A leading edge flap is provided for an airfoil. The leading edge (24) is rotatably mounted to the airfoil (74). A first flap segment is (48) attached to the leading edge (24) and has an external aerodynamic surface (50a) adapted to form ...
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JPS5811360B2 |
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JPS5833591A |
A reversible aerofoil comprises a central panel (10) with lateral panels (12A,12B) hinged to opposite edges. The lateral panels can be hinged so that either one overlies the central panel while the other is extended, thereby producing al...
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JPS5810277B2 |
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JPS5759439Y2 |
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JPS5750717B1 |
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JPS5748230B2 |
A system for attaching fins to a tubular body of a model rocket employs a base with a horizontal upper surface and upstanding fin guide plates mounted on the base. In the preferred form, the base has a central aperture that receives an e...
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JPS57144196A |
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JPS57501443A |
PCT No. PCT/SE81/00281 Sec. 371 Date May 20, 1982 Sec. 102(e) Date May 20, 1982 PCT Filed Sep. 29, 1981 PCT Pub. No. WO82/01230 PCT Pub. Date Apr. 15, 1982.The invention relates to an angle setting device of hinge type, especially for us...
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JPS5755298A |
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