Apparatus for load testing

专利摘要:
Load test apparatus according to the present invention, the driving unit for providing a driving force; An equivalent inertia unit for a test object driven by a driving force transmitted from the driving unit; A disk coupling assembly connecting the drive unit and the equivalent inertia unit and transmitting a driving force; A housing for supporting the equivalent inertia portion to be rotated; A leaf spring connected to the equivalent inertial part and transmitting torque generated from the equivalent inertial part; Torque sensor unit for measuring the torque transmitted through the leaf spring; And a base supporting the drive unit, the housing, and the torque sensor unit. It includes. According to the present invention, there is an advantage that can be measured without the actual wind tunnel test, by using a spring and torque sensor connected to the moving object, the torque generated by aerodynamics for the movement of the object.
公开号:KR20030043090A
申请号:KR1020010074076
申请日:2001-11-27
公开日:2003-06-02
发明作者:전관수
申请人:엘지이노텍 주식회사；
IPC主号:

专利说明:

Load testing device {Apparatus for load testing}
[7] The present invention relates to a load test apparatus, and more particularly to a load test apparatus that can measure the torque generated by the aerodynamic force against the movement of the object, without the actual wind tunnel test.
[8] In general, a traveling object or a flying object is subject to aerodynamic drag and lift for its movement. In addition, torque generated by aerodynamic force is generated on the wing and the like formed on the flying object. The drag, lift, torque, etc. are an important factor in designing a car or an airplane, and use a wind tunnel device to experiment.
[9] Here, the wind tunnel device refers to a device in which air is artificially flowed to investigate a phenomenon in which air flows, a force of air flow on an object, or movement of an object in the flow.
[10] In this case, when measuring the influence of aerodynamic forces on an aircraft object, experimentally measure the aerodynamic forces, moments, etc. received by the flying object using a real model or real object. In general wind tunnel system, the air flow is circulated to create a continuous flow, which is classified into a closed loop type and an open road type according to how the air flow is circulated, and closed according to the measuring method of the measuring unit. Divide into expression and open.
[11] On the other hand, the wind tunnel test has a merit that it is possible to easily and safely experiment with low cost since it is possible to analyze the measurement result by systematically changing the model when using a small model, compared to the direct measurement using the real object.
[12] However, since the difference in the various measured quantities such as the difference in size and speed between the model and the real object has a great influence on the measurement result, the experimental result is sometimes different from the actual test result. It is necessary to consider.
[13] As a result, the pressure in the wind tunnel device may be increased, or a wind tunnel facility may be constructed that is large enough to use a dense gas or to contain a real object. Therefore, in order to perform the wind tunnel test, there is a disadvantage in that the burden of installation cost is greatly generated along with the space limitation.
[14] The present invention was created in view of the above-described conditions, and the load generated by aerodynamic forces on an object's movement can be measured without a real wind tunnel test by using a spring and a torque sensor connected to a moving object. It relates to a test apparatus.
[1] 1 is a view schematically showing the configuration of a load test apparatus according to the present invention.
[2] <Explanation of symbols for the main parts of the drawings>
[3] 11 ... drive section 12 ... disc coupling assembly
[4] 13 ... Housing 14 ... Equivalent inertia
[5] 15 ... Leaf spring 16 ... Torque sensor
[6] 17 ... Bass
[15] Load test apparatus according to the present invention to achieve the above object,
[16] A driving unit providing a driving force;
[17] An equivalent inertia unit for a test object driven by a driving force transmitted from the driving unit;
[18] A disk coupling assembly connecting the drive unit and the equivalent inertia unit and transmitting a driving force;
[19] A housing for supporting the equivalent inertia portion to be rotated;
[20] A leaf spring connected to the equivalent inertial part and transmitting torque generated from the equivalent inertial part;
[21] Torque sensor unit for measuring the torque transmitted through the leaf spring; And
[22] A base supporting the drive unit, the housing, and the torque sensor unit; Its features are to include.
[23] According to the present invention, there is an advantage that can be measured without the actual wind tunnel test, by using a spring and torque sensor connected to the moving object, the torque generated by aerodynamics for the movement of the object.
[24] Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to the accompanying drawings.
[25] 1 is a view schematically showing the configuration of a load test apparatus according to the present invention.
[26] Referring to Figure 1, the load test apparatus according to the present invention includes a drive unit 11 for providing a driving force; An equivalent inertia part 14 for a test object, driven by a driving force transmitted from the drive part 11; A disk coupling assembly (12) connecting the drive unit (11) and the equivalent inertia unit (14) and transmitting a driving force; A housing (13) for supporting the equivalent inertial portion (14) to be rotated; A leaf spring 15 connected to the equivalent inertial portion 14 to which torque generated by the equivalent inertial portion 14 is transmitted; Torque sensor unit 16 for measuring the torque transmitted through the leaf spring (15); And a base 17 supporting the drive unit 11, the housing 13, and the torque sensor unit 16. It includes.
[27] Then, the operation of the load test apparatus having such a configuration will be described. First, the equivalent inertia 14 is simulated to reflect the moment of inertia of the test object. That is, when the torque generated by the aerodynamic force is to be detected in the wing of the vehicle, the equivalent inertial portion 14 simulates the moment of inertia of the wing. Therefore, the shape of the equivalent inertial portion 14 should be formed to simulate the same moment of inertia in view of the shape of the body of the aircraft and the wings coupled to the body.
[28] In addition, the equivalent inertial portion 14 is supported to be rotated by the housing 13, and the equivalent inertial portion 14 is fastened to the drive portion 11 via the disc coupling assembly 12. At this time, the equivalent inertial portion 14 is fastened to the driving unit 11 through the disk coupling assembly 12, such that the rotation axis of the driving unit 11 and the rotation axis of the equivalent inertia unit 14 are within a predetermined range. Even in the case of misalignment, the driving force can be transmitted effectively.
[29] Through such fastening, the equivalent inertial portion 14 is driven by the driving force of the driving unit 11. Accordingly, the equivalent inertia portion 14 generates torque in accordance with the rotational movement, the generated torque component is transmitted through the leaf spring (15). Here, the leaf spring 15 is to simulate the torque generated by the equivalent inertial portion 14 by the aerodynamic force.
[30] The torque transmitted through the leaf spring 15 is measured by the torque sensor unit 16. That is, by referring to the torque component measured by the torque sensor unit 16, it is possible to detect the torque component generated by the aerodynamic force at the equivalent inertia unit 14, for example, the wing portion of the vehicle.
[31] According to the load test apparatus according to the present invention as described above, by using a spring and a torque sensor connected to the moving object, the torque generated by the aerodynamic force can be measured without the actual wind tunnel test There is an advantage.

权利要求:
Claims (1)
[1" claim-type="Currently amended] A driving unit providing a driving force;
An equivalent inertia unit for a test object driven by a driving force transmitted from the driving unit;
A disk coupling assembly connecting the drive unit and the equivalent inertia unit and transmitting a driving force;
A housing for supporting the equivalent inertia portion to be rotated;
A leaf spring connected to the equivalent inertial part and transmitting torque generated from the equivalent inertial part;
Torque sensor unit for measuring the torque transmitted through the leaf spring; And
A base supporting the drive unit, the housing, and the torque sensor unit; Load test apparatus comprising a.

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同族专利:

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引用文献:

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公开号 | 申请日 | 公开日 | 申请人 | 专利标题

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法律状态:
2001-11-27|Application filed by 엘지이노텍 주식회사

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2001-11-27|Priority to KR1020010074076A

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2003-06-02|Publication of KR20030043090A

优先权:

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申请号 | 申请日 | 专利标题

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KR1020010074076A|KR20030043090A|2001-11-27|2001-11-27|Apparatus for load testing|