CN201476797U - High-precision optical gyroscope-temperature box-stationary base device - Google Patents

High-precision optical gyroscope-temperature box-stationary base device Download PDF

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Publication number
CN201476797U
CN201476797U CN2009201674063U CN200920167406U CN201476797U CN 201476797 U CN201476797 U CN 201476797U CN 2009201674063 U CN2009201674063 U CN 2009201674063U CN 200920167406 U CN200920167406 U CN 200920167406U CN 201476797 U CN201476797 U CN 201476797U
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CN
China
Prior art keywords
base
incubator
temperature box
precision optical
clamp
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN2009201674063U
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Chinese (zh)
Inventor
李县洛
赵小宁
雷建军
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No 618 Research Institute of China Aviation Industry
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No 618 Research Institute of China Aviation Industry
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Priority to CN2009201674063U priority Critical patent/CN201476797U/en
Application granted granted Critical
Publication of CN201476797U publication Critical patent/CN201476797U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to a high-precision optical gyroscope-temperature box-stationary base device which comprises a stationary base 1, a temperature box 2, a base clamp 3 and a rotating disc 4, wherein the base clamp 3 is cylindrical, one end of the base clamp 3 is arranged in the temperature box 2, the stationary base 1 is arranged at the top end, and the other end penetrates a temperature box base platform 5 and is connected with the rotating disc 4; thermal insulation material 6 is arranged between the base clamp 3 and the temperature box base platform 5, the thermal insulation material 6 is flexible thermal insulation material which surrounds the base clamp 3 and is in tight contact with the inner surface of a central hole of the temperature box base platform 5, and a thermal insulation column 7 is arranged in the middle of the base clamp 3 in the temperature box base platform 5. The high-precision optical gyroscope temperature box stationary base device can effectively reduce the impacts of environmental disturbance and vibration of a temperature box compressor on a high-precision optical gyroscope while realizing the thermal insulation of the temperature box with outside, thereby having higher test precision and reliability. Meanwhile, the combination of the device can realize the measurement of a gyroscope scale factor, thereby having greater practical application value.

Description

The quiet base unit of a kind of high-precision optical gyro incubator
Technical field
The utility model relates to the quiet base unit of a kind of high-precision optical gyro incubator.
Background technology
High-precision optical gyro subtle disruption to external world is very responsive, as small vibration or temperature variation, all might exert an influence to the optical gyroscope precision.Therefore in the real work, provide the experiment porch of an absolute rest and temperature constant to the high-precision optical gyro as far as possible.
When particularly in the high-low temperature test chamber of high-precision optical gyro, carrying out humid test, how when maintenance is temperature-resistant, to guarantee the test fixed pedestal of an absolute rest again, particularly reduce various vibration interference, the interference that comprises extraneous disturbance and incubator vibration of compressor is an important problem always.
When prior art high-precision optical gyro carried out humid test in high-low temperature test chamber, gyro was placed directly on the incubator base station table top, is subjected to the influence of incubator compressor disturbance easily, therefore influenced the measuring accuracy of gyro.And owing to gyro is placed directly on the incubator base station table top, and prior art incubator base station generally maintains static, therefore the high-precision optical gyro holding position when carrying out humid test that is placed in the incubator is constant, makes that the pilot project that can carry out is limited.
The utility model content
In order to solve prior art high-precision optical gyro is difficult to reduce vibration interference in the maintenance temperature in incubator influence and the limited problem of pilot project, isolate external interference and can realize the quiet base unit of high-precision optical gyro incubator that multinomial performance is tested when the utility model provides a kind of energy to keep temperature-resistant.
In order to solve the problems of the technologies described above, the utility model provides following technical scheme: the quiet base unit of a kind of high-precision optical gyro incubator, it comprises quiet pedestal 1, incubator 2, base clamp 3, rotating disk 4, wherein, base clamp 3 is cylindrical, these base clamp 3 one ends are in incubator 2, and its top is quiet pedestal 1, and the other end passes incubator base station 5 and links to each other with rotating disk 4; And be provided with heat-barrier material 6 between described base clamp 3 and the incubator base station 5, described heat-barrier material 6 is a flexible insulant material, it closely contacts around base clamp 3 and with incubator base station 5 inside surfaces, and the described in addition centre that is positioned at the base clamp 3 of incubator base station 5 is provided with heat insulation post 7.
Described heat-barrier material 6 is a heat insulation foam.
Described base clamp 3 realizes that by the some screws that are arranged in the screw channel 8 locking of the two is connected with heat insulation post 7.
Described rotating disk 4 is arranged on the end pier 9.
The quiet base unit of the utility model high-precision optical gyro incubator reduces external disturbance and incubator vibration of compressor to being placed on the influence of the high-precision optical gyro on the quiet pedestal by being arranged on flexible insulant material between base clamp and the incubator base station.The described heat-barrier material heat insulation post middle with being located at the cylindrical base anchor clamps completely cuts off incubator together by base clamp and extraneous heat transmission simultaneously, make the high-precision optical gyro in the incubator can keep the environment of a constant temperature, thereby realize zero inclined to one side accurate measurement.In addition, by base clamp is arranged on the rotating disk, the rotation by rotating disk and the metering of gyro umber of pulse can realize the measurement to gyro constant multiplier, constant multiplier repeatability and gyro constant multiplier temperature control, therefore have bigger actual application value.
Description of drawings
Fig. 1 is the structural representation of quiet base unit one better embodiment of the utility model high-precision optical gyro incubator,
Wherein, the quiet pedestal of 1-, 2-incubator, 3-base clamp, 4-rotating disk, 5-incubator base station, 6-heat-barrier material, the heat insulation post of 7-, 8-screw channel, pier at the bottom of the 9-.
Embodiment
The utility model is described in further detail below by embodiment:
See also Fig. 1, this figure is the structural representation of quiet base unit one better embodiment of the utility model high-precision optical gyro incubator.In the present embodiment, the quiet base unit of described high-precision optical gyro incubator, it comprises quiet pedestal 1, incubator 2, base clamp 3 and rotating disk 4.Wherein, base clamp 3 is cylindrical, and these base clamp 3 one ends are in incubator 2, and its top is quiet pedestal 1, and the other end passes incubator base station 5 and links to each other with rotating disk 4, and this rotating disk 4 is arranged on the end pier 9, and this end pier 9 is the Dali stone pier.Be provided with heat-barrier material 6 between base clamp 3 and the incubator base station 5 in addition, this heat-barrier material 6 is flexible heat insulation foam, and it closely contacts around base clamp 3 and with the inside surface of incubator base station 5 center pits.The described in addition base clamp 3 that is positioned at incubator base station 5 is divided into two parts, be folded with heat insulation post 7 between two parts base clamp, this heat insulation post 7 is made by the entity heat-barrier material, and it is fastenedly connected by the some screw locking realizations in base clamp 3 screw channels 8 and two parts base clamp 3.
In the present embodiment, heat-barrier material 6 and heat insulation post 7 that the quiet base unit of described high-precision optical gyro incubator is arranged between base clamp 3 and incubator 2 inside surfaces can be isolated incubator effectively by the heat transferred between the base clamp 3 and the external world.Because heat insulation foam is a flexible material, and it fits tightly between base clamp 3 and incubator 2, therefore have vibration isolating effect simultaneously, can reduce the influence of external disturbance and incubator 2 vibration of compressor gyro.Therefore the quiet base unit of the utility model high-precision optical gyro incubator can be realized vibration isolation in heat insulation, disturb thereby help eliminating, realization is to gyro zero inclined to one side accurate measurement, comprise zero measurement of average partially, and zero stability, zero measurement of laying particular stress on indexs such as renaturation and random walk coefficient partially.
In addition, because the gyro of the quiet base unit of the utility model high-precision optical gyro incubator is arranged on the quiet pedestal 1, and quiet pedestal 1 links to each other with rotating disk 4 by base clamp 3.Therefore, the rotation of rotating disk 4 can be rotated by the gyro that base clamp 3 drives on the quiet pedestal 1.Therefore in rotating disk 4 rotation processes, its rotational angle can directly be read by rotating disk 4, and the gyro circuit can write down the umber of pulse of rotation process gyro output simultaneously.Utilize the umber of pulse write down and the relation of rotational angle then: N=K θ, wherein, K is the optical gyroscope constant multiplier, and N is the accumulative total umber of pulse of rotation process gyro output, θ is a rotational angle, for this reason by measuring the constant multiplier K that umber of pulse N and rotational angle θ just can calculate gyro.And can realize measurement, and can investigate the susceptibility of constant multiplier by repeatedly measuring the angle that rotating disk 4 rotates and the accumulative total umber of pulse of gyro output to temperature by changing the incubator temperature to laser gyro constant multiplier repeatability.And constant multiplier K is one of an optical gyroscope very important index parameter, so the quiet base unit of the utility model high-precision optical gyro incubator has bigger actual application value.
The heat-barrier material of the quiet base unit of the utility model high-precision optical gyro incubator is not limited to heat insulation foam in addition, as long as it is a flexible material when having heat-proof quality, as heat insulation polymkeric substance etc.
The quiet base unit of the utility model high-precision optical gyro incubator is by being arranged on being arranged on realization and heat insulation the time, can reducing the influence to the high-precision optical gyro of environmental perturbation and incubator vibration of compressor to gyro of flexible insulant material between base clamp and the incubator base station and heat insulation post in sum.In addition because the quiet pedestal in the incubator fixedly provides an absolute rest for gyro, and the enough big experiment stationary platform of opposing torque, so can improve the reliability that gyro is tested greatly under high and low temperature.Therefore this device can effectively improve the measuring accuracy and the reliability of high-precision optical gyro, thereby realizes that average, zero stability partially, the zero accurate measurement of laying particular stress on indexs such as renaturation, random walk coefficient are measured partially to zero.Link to each other with rotating disk by base clamp owing to gyro simultaneously, therefore the metering of rotation by rotating disk and gyro umber of pulse can realize the experimental study to gyro constant multiplier, constant multiplier repeatability and constant multiplier temperature control, therefore has bigger actual application value.

Claims (4)

1. quiet base unit of high-precision optical gyro incubator, it is characterized in that: comprise quiet pedestal [1], incubator [2], base clamp [3], rotating disk [4], wherein, base clamp [3] is cylindrical, these base clamp [3] one ends are in incubator [2], its top is quiet pedestal [1], and the other end passes incubator base station [5] and links to each other with rotating disk [4]; And be provided with heat-barrier material [6] between described base clamp [3] and the incubator base station [5], described heat-barrier material [6] is a flexible insulant material, it closely contacts around base clamp [3] and with incubator base station [5] inside surface, in addition, be provided with heat insulation post [7] between the described base clamp [3] that is positioned at incubator base station [5].
2. the quiet base unit of high-precision optical gyro incubator according to claim 1 is characterized in that: described heat-barrier material [6] is a heat insulation foam.
3. the quiet base unit of high-precision optical gyro incubator according to claim 2 is characterized in that: described base clamp [3] realizes that by the some screws that are arranged in the screw channel [8] locking of the two is connected with heat insulation post [7].
4. the quiet base unit of high-precision optical gyro incubator according to claim 2, it is characterized in that: described rotating disk [4] is arranged on the end pier [9].
CN2009201674063U 2009-07-23 2009-07-23 High-precision optical gyroscope-temperature box-stationary base device Expired - Fee Related CN201476797U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009201674063U CN201476797U (en) 2009-07-23 2009-07-23 High-precision optical gyroscope-temperature box-stationary base device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009201674063U CN201476797U (en) 2009-07-23 2009-07-23 High-precision optical gyroscope-temperature box-stationary base device

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CN201476797U true CN201476797U (en) 2010-05-19

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105952905A (en) * 2016-06-27 2016-09-21 九江精密测试技术研究所 Thermostat rotating table shaft system seal design
CN112484748A (en) * 2019-09-11 2021-03-12 九江精密测试技术研究所 Sealing structure of incubator turntable refrigeration conveying system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105952905A (en) * 2016-06-27 2016-09-21 九江精密测试技术研究所 Thermostat rotating table shaft system seal design
CN112484748A (en) * 2019-09-11 2021-03-12 九江精密测试技术研究所 Sealing structure of incubator turntable refrigeration conveying system

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100519

Termination date: 20160723