CN203414070U - Fixing device for displacement sensor - Google Patents
Fixing device for displacement sensor Download PDFInfo
- Publication number
- CN203414070U CN203414070U CN201320249863.3U CN201320249863U CN203414070U CN 203414070 U CN203414070 U CN 203414070U CN 201320249863 U CN201320249863 U CN 201320249863U CN 203414070 U CN203414070 U CN 203414070U
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- China
- Prior art keywords
- adjustable
- crossbeam
- transition section
- displacement
- fixing
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- Expired - Fee Related
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Abstract
The utility model relates to a fixing device for a displacement sensor, which belongs to sensor installation and fixation technology. The fixing device for a displacement sensor comprises a vertical support unit, a transverse support unit and several adjustable displacement sensor fixing racks. The vertical support unit is a vertical support column comprising a fixing base, an adjustable transition section and a transition plate, wherein the transition plate is arranged at the top end of the adjustable transition section performing as a column, and the bottom of the adjustable transition section is arranged on the fixing base. The transverse support unit comprises a fixing corner sheet and a crossbeam, and the crossbeam is arranged on the mounting surface of the adjustable transition section through the fixing corner sheet. The adjustable displacement sensor fixing racks are arranged on the crossbeam. According to the fixing device for a displacement sensor, displacement point installation difficulty in the prior total machine displacement measurement is overcome, the space utilization rate is raised, and the measuring stability and reliability are guaranteed.
Description
Technical field
The utility model belongs to installation of sensors technique for fixing, relates to a kind of fixing device for installing of displacement transducer.
Background technology
In complete aircraft structural static/torture test, in order to measure aircaft configuration stability and displacement variable in process of the test, need carry out displacement measurement to each state of aircraft.And that solid timing problems is installed is many in the face of displacement transducer, mainly concentrate on this some: 1) displacement measurement point is many, is placed on ground unordered causing and other equipment interference of ground straggly in the past; 2) ground does not have special-purpose stationary installation, and personnel can make it be offset original installation site through situations such as collisions, and measuring accuracy is caused and had a strong impact on; 3) when survey aircraft fuselage side, conventionally utilize the on-the-spot column that loads to build simple and easy support, there is equally certain error.
Utility model content
The purpose of this utility model is: the utility model creation object is to provide a kind of in complete aircraft stryctyrak test, is that aircraft displacement state is measured, and specially designed a kind of displacement transducer stationary installation.
The technical solution of the utility model is: a kind of displacement transducer stationary installation, it comprises vertical supporter, lateral support unit, some displacement-adjustable fixing rack for sensor, wherein, vertical supporter is vertical support column, by holder, adjustable transition section, rebound, formed, rebound is arranged on the adjustable transition section top as column, and adjustable transition section bottom is arranged on holder; Described lateral support unit is comprised of fixedly gusset plate and crossbeam, and crossbeam is arranged on the installed surface of adjustable transition section by fixing gusset plate; Described displacement-adjustable fixing rack for sensor is arranged on crossbeam.
Described displacement-adjustable sensor is comprised of adjustable knob, sensor installation seat, Magnetic gauge stand, and wherein, sensor installation seat is fixed on Magnetic gauge stand by adjustable knob, and this Magnetic gauge stand is fixed on crossbeam.
Described crossbeam fixedly gusset plate is fixedly gusset plate of L-type.
Technique effect of the present utility model is: the utility model utilizes vertical support column (holder, adjustable transition section, rebound form), and displacement transducer is arranged on differing heights, by space delamination, takes full advantage of space resources; Adopt lateral support unit (displacement-adjustable fixing rack for sensor, fixedly gusset plate, crossbeam composition), displacement transducer can freely be placed within crossbeam forms plane, so most of aircraft measurement point can cover, displacement transducer is fixed on Adjustable magnetic gauge stand and utilizes electromagnet to be firmly adsorbed on crossbeam, and adjuster bar is finely tuned and made it to reach perfect condition.Thereby efficiently solving full seat in the plane shift measurement displacement point in the past installs difficulty, has improved space availability ratio, the Measurement sensibility in warranty test process and reliability.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation;
Fixedly gusset plate, the adjustable crossbeam of 3-, 4-adjustable transition section, 5-firm banking, 6-adjustable knob, 7-displacement transducer mount pad, 8-Magnetic gauge stand of 1-rebound, 2-wherein.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described further:
Refer to Fig. 1, it is the utility model structural representation.The utility model displacement transducer stationary installation comprises vertical supporter, lateral support unit, some displacement-adjustable fixing rack for sensor.
Wherein, vertical supporter is vertical support column, holder, adjustable transition section, rebound, consists of, and rebound is arranged on the adjustable transition section top as column, and adjustable transition section bottom is arranged on holder.Described lateral support unit is comprised of fixedly gusset plate and crossbeam, crossbeam by L-type fixedly gusset plate be arranged on the installed surface of adjustable transition section.Described displacement-adjustable fixing rack for sensor is arranged on crossbeam, and it is comprised of adjustable knob 6, sensor installation seat 7, Magnetic gauge stand 8, and wherein, sensor installation seat 7 is fixed on Magnetic gauge stand 8 by adjustable knob 6, and this Magnetic gauge stand 8 is fixed on crossbeam.
During the real work of the utility model displacement transducer stationary installation, first firm banking 5 is arranged on close measurement point base track, according to measuring height, select suitable adjustable transition section 4, between transition section 4 and transition section 4, adopt excessive plate 1 to be connected, gusset plate 2 is installed fixedly for secured adjusted crossbeam 3 on the face that need measure at aircraft, Magnetic gauge stand 8 correspondences are placed on and are needed on measurement point, displacement transducer is fixed on to sensor installation seat 7, by 6 pairs of measuring positions of adjustable knob, finely tunes and make it to reach perfect condition.
The utility model, by regulating the height of vertical support column and crossbeam in the position of vertical support column, can make displacement transducer be arranged on differing heights, by space delamination, thereby makes full use of space resources.And displacement transducer can freely be placed by displacement-adjustable fixing rack for sensor within crossbeam forms plane, so most of aircraft measurement point can cover, displacement transducer is fixed on Adjustable magnetic gauge stand and utilizes electromagnet to be firmly adsorbed on crossbeam, by adjustable knob 6 fine settings, make it to reach perfect condition, effectively guaranteed test figure reliability.
Claims (3)
1. a displacement transducer stationary installation, it is characterized in that: comprise vertical supporter, lateral support unit, some displacement-adjustable fixing rack for sensor, wherein, vertical supporter is vertical support column, by holder, adjustable transition section, rebound, formed, rebound is arranged on the adjustable transition section top as column, and adjustable transition section bottom is arranged on holder; Described lateral support unit is comprised of fixedly gusset plate and crossbeam, and crossbeam is arranged on the installed surface of adjustable transition section by fixing gusset plate; Described displacement-adjustable fixing rack for sensor is arranged on crossbeam.
2. displacement transducer stationary installation according to claim 1, it is characterized in that: described displacement-adjustable sensor is comprised of adjustable knob, sensor installation seat, Magnetic gauge stand, wherein, sensor installation seat is fixed on Magnetic gauge stand by adjustable knob, and this Magnetic gauge stand is fixed on crossbeam.
3. displacement transducer stationary installation according to claim 1, is characterized in that: described crossbeam fixedly gusset plate is fixedly gusset plate of L-type.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320249863.3U CN203414070U (en) | 2013-05-10 | 2013-05-10 | Fixing device for displacement sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320249863.3U CN203414070U (en) | 2013-05-10 | 2013-05-10 | Fixing device for displacement sensor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203414070U true CN203414070U (en) | 2014-01-29 |
Family
ID=49976954
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320249863.3U Expired - Fee Related CN203414070U (en) | 2013-05-10 | 2013-05-10 | Fixing device for displacement sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203414070U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106546206A (en) * | 2016-10-21 | 2017-03-29 | 奇瑞汽车股份有限公司 | Altimeter support |
| CN109470190A (en) * | 2018-11-09 | 2019-03-15 | 中国直升机设计研究所 | Rod-pulling type displacement sensor fixes device |
| CN110307449A (en) * | 2019-07-01 | 2019-10-08 | 中国人民解放军总参谋部第六十研究所 | Displacement transducer mounting bracket on a kind of cast iron test platform |
-
2013
- 2013-05-10 CN CN201320249863.3U patent/CN203414070U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106546206A (en) * | 2016-10-21 | 2017-03-29 | 奇瑞汽车股份有限公司 | Altimeter support |
| CN109470190A (en) * | 2018-11-09 | 2019-03-15 | 中国直升机设计研究所 | Rod-pulling type displacement sensor fixes device |
| CN110307449A (en) * | 2019-07-01 | 2019-10-08 | 中国人民解放军总参谋部第六十研究所 | Displacement transducer mounting bracket on a kind of cast iron test platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: Xi'an Desheng non-standard equipment manufacturing Co., Ltd. Assignor: China Plane Intensity Research Institute Contract record no.: 2015610000110 Denomination of utility model: Displacement sensor fixing device Granted publication date: 20140129 License type: Exclusive License Record date: 20151224 |
|
| LICC | Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model | ||
| EC01 | Cancellation of recordation of patent licensing contract |
Assignee: Xi'an Desheng non-standard equipment manufacturing Co., Ltd. Assignor: China Plane Intensity Research Institute Contract record no.: 2015610000110 Date of cancellation: 20160222 |
|
| LICC | Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160310 Address after: 710065, No. two, No. 3, Yanta District, Shaanxi, Xi'an Patentee after: Xi'an Desheng non-standard equipment manufacturing Co., Ltd. Address before: 710065 box 86, Xi'an, Shaanxi, Xi'an Patentee before: China Plane Intensity Research Institute |
|
| 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: 20140129 Termination date: 20200510 |