Small-size self-balancing type weather vane

A self-balancing and self-balancing technology, applied in measuring devices, instruments, aircraft parts, etc., can solve the problems of small measuring angle range and large weight of blade wind vane, and achieve the effect of increasing the angle of attack

Active Publication Date: 2014-04-02
TAIYUAN AERO INSTR
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The present invention solves the problem that the wind vane of the existing blade-type vane angle of attack and side-slip angle sensor is close to the surface of the aircraft or product, and is greatly affected by the profile of the aircraft or product. In addition, the blade-type weather vane has a large weight and can measure the angle For smaller range problems, a small self-balancing wind vane is provided

Method used

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  • Small-size self-balancing type weather vane

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Embodiment Construction

[0013] A small self-balancing weather vane includes a rotating shaft 1, a weather vane pole 2 and a weather vane 3 made of aluminum alloy. The weathervane 3 and the weathervane pole 2 are combined with rivets. The front half of the weathervane pole 2 is made of stainless steel and has an equal-diameter structure; the second half is made of aluminum alloy and has a streamlined contraction design. The front half is equal in diameter; the wind vane 3 is made of aluminum alloy and has a symmetrical plate structure on both sides. The weather vane 2 is a high-strength rotating shaft 1 and the present invention is connected to an angular displacement sensor to realize angle transmission. The rotating shaft 1 is a load-bearing structure made of high-strength metal materials.

[0014] For aircraft cruising at supersonic speed, the head of weathervane 2 is generally pointed, and for aircraft cruising at subsonic speed, the head of weathervane 2 is generally hemispherical.

[0015] The...

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Abstract

The invention belongs to the technical field of measurement for attack angles and sideslip angles in an aircraft air data system and specifically relates to a small-size self-balancing type weather vane. The problems of a large influence on aircraft or product profiles and a smaller measurable angle scope of the present blade type weather vane are solved. The small-size self-balancing type weather vane comprises a rotating shaft, a weather vane rod and a weather vane made of aluminum alloy material, wherein the weather vane rod comprises a front half part made of stainless steel material and a rear half part made of aluminum alloy material; the front half part has an equal-diameter structure; the rear half part has a streamline contracting type structure; the diameter of the front end of the rear half part connected with the front half part is the same as the diameter of the front half part; the weather vane has a two-side symmetrical platy structure. The small-size self-balancing type weather vane can be used for effectively eliminating the influence on the aircraft or product surface and accurately outputting the attack angle and sideslip angle data; the measurement scope of an attack angle/sideslip angle sensor is greatly increased; the highest use mach number can reach 2.5 and the 340-degree measuring scope can be achieved.

Description

technical field [0001] The invention belongs to the technical field of angle of attack and sideslip angle measurement in an aircraft air data system, and in particular relates to a small self-balancing wind vane. Background technique [0002] Existing angle-of-attack and side-slip angle vanes are generally blade-type, and the weather vane itself is very heavy, and counterweights need to be installed inside the housing for balance, resulting in excessive weight of the entire product. In addition, due to the limitation of the internal counterweight structure, the measurement range of the angle of attack and sideslip angle is very small, generally not exceeding 30°. The angle of attack and sideslip angle sensor developed by the blade wind vane is close to the surface of the aircraft or the product, and the measurement of the angle of attack and side slip angle will be affected by the airflow on the surface of the aircraft, so it must be compensated by a program; the blade wind ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00G01B21/22
Inventor 杜振宇石岩张丽
Owner TAIYUAN AERO INSTR
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