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A vibration and shock test fixture for ccd image sensor

An image sensor and impact test technology, which is applied in vibration test, impact test, machine/structural component test, etc., can solve the problem of uneven force, and achieve the effect of ensuring light weight and easy space inversion

Active Publication Date: 2019-03-12
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For example, the base material of the CCD image sensor and the light-transmitting material of the upper cover are made of different materials, and the glass cover of the CCD image sensor is relatively brittle, which is easy to break in the force field, so the glass cover of the CCD image sensor should be specially protected ; Another example is that the glass cover and the surrounding ceramic materials are not on the same plane, which may easily lead to uneven force; in addition, the CCD image sensor also has certain requirements for electrostatic protection

Method used

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  • A vibration and shock test fixture for ccd image sensor
  • A vibration and shock test fixture for ccd image sensor
  • A vibration and shock test fixture for ccd image sensor

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Embodiment Construction

[0029] The present invention will be described in detail below in conjunction with the accompanying drawings.

[0030] The present invention simulates the more characteristic on-site environment produced by missiles, high-speed propulsion jet aircraft and rocket engine devices through vibration tests to verify whether vibration has any effect on the ceramic body, glass body, pins or the seal between the ceramic body and the glass body. defect or damage.

[0031] The invention simulates the impact caused by sudden force or sudden change of motion state during loading and unloading, transportation or field operation through the impact test. This type of impact may destroy the working characteristics or cause damage similar to that caused by too strong vibration , if the shock pulse is repetitive, the damage is more serious.

[0032] In particular, the present invention simulates the completion of 60G-80G high-level vibration and 3000G impact tests to overcome the current diffic...

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Abstract

The present invention discloses a CCD image sensor vibration and impact test clamp which comprises a clamp body and a cover plate. The clamp body is a cubic structure, each side of the clamp body is provided with sample placement holes for placing a CCD image sensor, and the sample placement holes in each side are in axial symmetry or central symmetry. The sample placement holes are provided with pin fixed holes, and the CCD image sensor with pins can be inserted into the pin fixed holes of the clamp body. According to the invention, the clamp body is designed as the cubic structure, the thickness of the sample placement holes of each side is 0.6 cm to 1.3 cm, a hollow structure is formed by six sides, the sample placement holes are in axial symmetry or central symmetry so as to prevent resonance in a vibration process to cause sample damage. At the same time, in the condition of the certain requirement of a sample weight by equipment, 60G to 80G high order vibration and more than 3000G impact tests are completed, and the space reversal of the clamp body is easy to realize.

Description

technical field [0001] The invention relates to a fixture used for vibration and impact tests of a CCD image sensor, belonging to the field of aerospace components. Background technique [0002] Vibration and shock tests are essential and important test contents for upgrade screening tests and reliability tests of aerospace components. The test can determine the ability of the device to withstand dynamic stress, determine the impact of vibration on the device within the specified frequency range, measure the electrical noise generated by the device under vibration conditions, and determine whether the device can be used in electronic equipment that needs to withstand moderate severe shocks middle. At present, the variety and quantity of high-grade and high-reliability components used in aerospace models are increasing. In the actual quality assurance work, you will encounter various forms, various packages, various materials and expensive components, which requires the dev...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M7/02G01M7/08
CPCG01M7/02G01M7/08
Inventor 李璇张红旗唐章东王雪生刘建强范壮壮
Owner CHINA ACADEMY OF SPACE TECHNOLOGY