Pneumatic test device based on large-size control surface hinge moment

A technology of aerodynamic test and hinge torque, which is applied in the field of aircraft wind tunnel test, can solve the problems of large size of angle block, damage to the aerodynamic shape of rudder surface, large size of rudder surface and heavy weight

Pending Publication Date: 2021-12-24
中航通飞华南飞机工业有限公司
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Problems solved by technology

However, the realization of the large-scale rudder surface hinge moment test device does not enlarge the simple size ratio of the conventional large-scale rudder surface hinge moment test device. In the conventional large-scale rudder surface hinge moment test, the rudder surface deflection, but the weight of the large-sized rudder surface is very heavy, and it cannot be lifted by manpower. It is not feasible to realize the deflection

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  • Pneumatic test device based on large-size control surface hinge moment
  • Pneumatic test device based on large-size control surface hinge moment
  • Pneumatic test device based on large-size control surface hinge moment

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Example Embodiment

[0037] This part is an embodiment of the present invention, and is used to explain and illustrate the technical solution of the present invention.

[0038] An aerodynamic test device based on hinge moment of large-scale rudder surface, including vertical tail 1, horizontal tail connecting plate 3, horizontal tail connecting seat 4, wind tunnel connecting seat 5, horizontal tail stabilizer 6, spherical hinge 7 and elevator 8; vertical tail 1 The flat tail connecting plate 3 and the flat tail connecting seat 4 are fixedly connected with the flat tail stabilizer 6. The flat tail stabilizer 6 is connected with the elevator 8 through at least two spherical hinges 7, and the bottom of the elevator 8 is connected; the whole device is installed on the wind tunnel through the wind tunnel connection seat 5. inside the cave.

[0039] The spherical hinges 7 are arranged equidistantly along the elevator axis direction. This design and technical solution can realize the uniform loading of ...

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Abstract

The invention belongs to the technical field of airplane wind tunnel tests, and discloses a pneumatic test device based on large-size control surface hinge moment, which comprises a vertical fin, a horizontal tail connecting plate, a horizontal tail connecting seat, a wind tunnel connecting seat, a horizontal tail stabilizer, spherical hinges and an elevator. The vertical fin is fixedly connected with the horizontal tail stabilizer through the horizontal tail connecting plate and the horizontal tail connecting seat, the horizontal tail stabilizer is connected with the elevator through the at least two spherical hinges, and the bottom of the elevator is connected. The whole device is installed in a wind tunnel through the wind tunnel connecting seat. According to the pneumatic test device based on the large-size control surface hinge moment, through the design of the spherical hinges, the technical problem of connection of an elevator and a stabilizer in a large-size control surface hinge moment test is effectively solved, and meanwhile the measurement precision of a balance is guaranteed.

Description

technical field [0001] The invention belongs to the technical field of aircraft wind tunnel tests, and relates to an aircraft rudder surface device for aerodynamic tests, in particular to an aerodynamic test device for measuring large-scale rudder surface hinge moments. Background technique [0002] In the process of aircraft R&D and design, it is necessary to conduct wind tunnel hinge moment tests on various rudder surfaces such as flaps, ailerons, elevators, and rudders to obtain the variation law of the rudder surface hinge moment parameters and master the aerodynamic performance of the rudder surface. The measurement accuracy of the rudder surface hinge moment wind tunnel test results plays an important role in supporting the maneuverability of the aircraft and the design of the control system. [0003] However, in order to reduce the test cost and shorten the test period, the rudder surface hinge moment wind tunnel test usually uses a wind tunnel test device with a larg...

Claims

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Application Information

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IPC IPC(8): G01M9/06G01M9/08B64F5/60
CPCG01M9/06G01M9/08B64F5/60
Inventor 迟永一杨康智温庆程志航
Owner 中航通飞华南飞机工业有限公司
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