Solder-resistant conductive film on the surface of sensitive structure of space electrostatic accelerometer and its manufacturing process

A sensitive structure, accelerometer technology, applied in the field of precision equipment for space science loads, can solve problems such as damaged electrode pads, electrode leads are easy to break, sensor assembly is difficult, etc., to ensure stability, good matching, and small linear expansion coefficient. Effect

Active Publication Date: 2017-11-03
LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although this method can avoid the soldering resistance requirements of the film, since the sensor needs to lead out as many as twenty electrode leads, and they are not on the same surface of the same structure, high temperature curing is required after gluing. The lead wire fixing method adds multiple processes, which makes the assembly of the sensor very difficult and reduces the reliability of the sensor
At the same time, in the test stage, the sensor inevitably needs to be disassembled and assembled many times, and the electrode leads are easy to break. Faced with the problem that the electrode leads need to be fixed many times, the original glue needs to be removed before each re-gluing. It is more difficult, and there is a risk of damaging the electrode pads, so the process of using conductive silver glue to fix the electrode leads of the electrostatic accelerometer sensor has many shortcomings

Method used

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  • Solder-resistant conductive film on the surface of sensitive structure of space electrostatic accelerometer and its manufacturing process
  • Solder-resistant conductive film on the surface of sensitive structure of space electrostatic accelerometer and its manufacturing process
  • Solder-resistant conductive film on the surface of sensitive structure of space electrostatic accelerometer and its manufacturing process

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Embodiment Construction

[0034] The present invention will be described in detail below in conjunction with the embodiments. The description in this part is only exemplary and explanatory, and should not have any limiting effect on the protection scope of the present invention.

[0035] A solder-resistant conductive film on the surface of the sensitive structure of a space electrostatic accelerometer, which is a three-layer composite film system: Ti-Pt-Au, wherein the thickness of the Ti film of the adhesive layer is generally controlled at 40-60nm, and the thickness of the Pt film of the intermediate transition layer It is controlled at 600nm-1000nm, and the thickness of the conductive protective Au film is controlled at 100-200nm.

[0036] Taking the sensitive structure of the sensor of the electrostatic levitation accelerometer as an example, the fabrication process of the solder-resistant conductive film on its surface is introduced.

[0037] The sensor sensitive structural components of the elect...

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Abstract

The invention discloses a solder-resistant conductive film on the surface of a sensitive structure of a space electrostatic accelerometer, which is composed of a titanium film layer, a platinum film layer and a gold film layer, and one side of the titanium film layer is bonded to the surface of the sensitive structural part of the space electrostatic accelerometer , and the other side is sequentially connected with the platinum film layer and the gold film layer. The solder-resistant conductive film of the present invention is all made of non-magnetic materials, so it will not generate noise interference to the measurement of the space electrostatic accelerometer, and all materials have a small linear expansion coefficient, which can ensure the contact between the base glass material and each film layer. Better matching ensures the stability of the film.

Description

technical field [0001] The invention relates to the technical field of precision equipment for space science loads, in particular to a solder-resistant conductive film used on the surface of a sensitive structure of a space electrostatic accelerometer, and a manufacturing process thereof. Background technique [0002] Electrostatic accelerometer is a kind of capacitive differential inertial acceleration sensor, which has the characteristics of low measurement frequency, high resolution and large dynamic range. It is especially suitable for measuring quasi-steady state and small acceleration signals. It plays an important role in the fields of control, active vibration reduction, satellite gravity measurement and so on. [0003] The system composition and measurement principle of the electrostatic accelerometer are as follows: figure 1 As shown, the main components include an inertial sensor probe and a detection and control drive circuit. The inertial sensor probe is mainly...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C23C14/14C23C14/34C23C14/02
Inventor 王佐磊雷军刚席东学霍红庆周海佳银东东薛大同邵航
Owner LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH
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