CN103913187A - Integrated test instrument heavy load component integration box - Google Patents
Integrated test instrument heavy load component integration box Download PDFInfo
- Publication number
- CN103913187A CN103913187A CN201410170883.0A CN201410170883A CN103913187A CN 103913187 A CN103913187 A CN 103913187A CN 201410170883 A CN201410170883 A CN 201410170883A CN 103913187 A CN103913187 A CN 103913187A
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- China
- Prior art keywords
- side box
- guide rail
- beams
- guiding rail
- base plate
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Abstract
The invention discloses an integrated test instrument heavy load component integration box which comprises a front frame, a rear frame, side box plates, a base plate, a cover plate and an internally-installed frame. The internally-installed frame is provided with side connecting plates, wherein the upper edges and the lower edges of the side connecting plates are matched with upper grooves and lower grooves of the two side box plates respectively. The four opposite corners of the two side connecting plates are connected through beams. The lower faces of the upper beams and the upper faces of the lower beams are provided with positioning holes in an arrayed mode. An upper guiding rail strip and a lower guiding rail strip are opposite and are connected between the two upper beams. An upper guiding rail strip and a lower guiding rail strip are opposite and are connected between the two lower beams. Each guiding rail strip is composed of a guiding rail and two-side connectors. The opposite faces of the upper guiding rail strips and the lower guiding rail strips are provided with strip-shaped grooves. The connectors are connected with the guiding rails through tenons inserted into hollow portions of the guiding rails. The connectors are provided with positioning columns matched with the positioning holes. Clamping buckles buckled with the beams are arranged on the connectors. The beams are fixedly connected with the side box plates, the base plate and the cover plate through connecting pieces. Modules are even in stress when impacted, and configuration is convenient and flexible.
Description
Technical field
The present invention relates to a kind of instrument integration case, particularly relate to a kind of integrated test test instrument heavy duty component integration case.
Background technology
Along with scientific and technological progress, various Portable Measurement Instrument have been come into all trades and professions, as medical treatment, commercial production and exploration all conglomeraties such as speedily carry out rescue work, for people's productive life provides reliable Data support.Portable Measurement Instrument has conveniently moving advantage flexibly, but its person's character moving also makes it construct usually among jerk, these situations generally occur in transhipment and test process, because built-in feature module connected mode generally adopts bolt fixing several on crossbeam, crossbeam is used in bolt fixing machine cabinet frame again, supporting point concentrates on pilot hole, on several fixed hole positions of crossbeam and framework, for portable instrument equipment, in the time having elliptical gear, built-in feature module can be subject to inertia and acceleration gravity effect, destroy the fixed connection structure between self and casing, be easy to cause the internal functional unit module of certain mass to become flexible and displacement, point type link is subject to force unbalance, syndeton is destroyed the distortion that also can cause parts self, the performance of surveying instrument is affected or disabler, especially the built-in feature module that quality is larger is influenced even more serious, also have the interior mounting hole site layout of instrument box relatively fixing, when installing and keeping in repair, can not move and take out, narrow space is not easy to operate, and parts are adjusted position and are not easy, and these should await technology and solve.
Summary of the invention
The invention provides a kind of integrated test test instrument heavy duty component integration case in order to address the above problem.
The technical solution used in the present invention is: a kind of integrated test test instrument heavy duty component integration case, comprise front baffle, afterframe, side box plate, base plate and cover plate, it is characterized in that side box plate has inside flanging up and down, it is U-shaped that section is, flanging inside surface is at least provided with together the groove with parallel sided, base plate is connected with the lower flanging of two side box plates, cover plate is connected with the upper flanging of two side box plates, front baffle is connected with the front end of base plate, cover plate, two side box plates, afterframe is connected with the rear end of base plate, cover plate, two side box plates, surrounds an outer case, in casing, be provided with one built-in, built-inly set up the side connecting plate that lower limb coincide respectively in the upper and lower groove of two side box plates, between two side connecting plates, relative four jiaos connect by crossbeam, below entablature, there is pilot hole with equal array above sill, between two entablatures, between two sills, be all connected with guide rail bar opposing upper and lower, guide rail bar is made up of guide rail and two side connectors, the face that upper/lower guide bar is relative is provided with bar-shaped trough, joint is connected with guide rail by the protruding falcon that inserts guide rail hollow part, joint is provided with the reference column coordinating with pilot hole, joint is provided with the buckle engaging with crossbeam, crossbeam is fixedly connected with side box plate, base plate, cover plate by web member.
Further, on described guide rail bar, be furnished with bracket, have the edge identical with guide rail bar-shaped trough on bracket, the same one end at this upper and lower edge is connected with the fixed-wing being connected with crossbeam.
Further, on described bracket, the opposite side relative with fixed-wing is provided with vertical edge strip, and to being provided with a fixed strip being connected with crossbeam by edge strip, fixed strip is provided with the vertical slot identical with this edge strip.
Further, on described joint, reference column is more than two, equidistant with pilot hole.
Further, described reference column is three, and the reference column of both sides is that the longitudinal profile of semicolumn is concordant with joint side along the axis semicolumn that longitudinally plane leaves.
When the present invention uses, internal functional unit module is fixedly mounted on built-in by guide rail bar, parts fixed-area is large, while being hit, module is stressed evenly, between member, in conjunction with firmly, even if the larger parts of quality also can strong bonded, can not cause certain a bit stressed excessive deformation or destroy syndeton, improve stability, guide rail stripe pitch can arbitrarily regulate, and sized parts configuration is convenient, flexible, module install and when maintenance built-in can also shift out easy to operate.
Brief description of the drawings
Fig. 1 is the embodiment of the present invention one one-piece construction schematic diagram.
Fig. 2 is the embodiment of the present invention one side box plate structural representation.
Fig. 3 is the embodiment of the present invention one inner structure schematic diagram.
Fig. 4 is the interior placing shelf structure schematic diagram of the embodiment of the present invention one.
Fig. 5 is that the embodiment of the present invention one is cutd open guide rail bar structural representation.
Fig. 6 is that the embodiment of the present invention one is cutd open joint design schematic diagram.
Fig. 7 is the embodiment of the present invention one beam structure schematic diagram.
Fig. 8 is the embodiment of the present invention one carrier structure schematic diagram.
Number in the figure title: 1 front baffle; 2 afterframes; 3 side box plates; 4 base plates; 5 cover plates; 6 flangings; 7 grooves; 8 side connecting plates; 9 entablatures; 10 sills; 11 pilot holes; 12 guide rails; 13 joints; 14 bar-shaped troughs; 15 protruding falcons; 16 reference columns; 17 buckles; 18 edges; 19 screw thread bars; 20 fixed-wings; 21 vertical edge strips; 22 fixed strips; 23 vertical slots.
Embodiment
The embodiment of the present invention is just like shown in Fig. 1 to 8, this integrated test test instrument heavy duty component integration case is provided with front baffle 1, afterframe 2, side box plate 3, base plate 4 and cover plate 5, side box plate has inside flanging 6 up and down, it is U-shaped that section is, flanging inside surface is at least provided with together the groove 7 with parallel sided, base plate is connected with the lower flanging of two side box plates, cover plate is connected with the upper flanging of two side box plates, front baffle is connected with the front end of base plate, cover plate, two side box plates, afterframe is connected with the rear end of base plate, cover plate, two side box plates, surrounds an outer case, in casing, be provided with one built-in, built-inly set up the side connecting plate 8 that lower limb coincide respectively in the upper and lower groove of two side box plates, this identical structure can reduce displacement and the distortion between casing and built-in in the time impacting, between two side connecting plates, relative four jiaos connect by crossbeam, entablature 9 below and sill 10 above equal array have pilot hole 11, between two entablatures, between two sills, be all connected with guide rail bar opposing upper and lower, guide rail bar is made up of guide rail 12 and two side connectors 13, the face that upper/lower guide bar is relative is provided with bar-shaped trough 14, joint is connected with guide rail by the protruding falcon 15 that inserts guide rail hollow part, joint is provided with the reference column 16 coordinating with pilot hole, reference column is more than two, equidistant with pilot hole, the present embodiment reference column is three, the reference column of both sides is along axis half cylinder that longitudinally plane leaves, the longitudinal profile of semicolumn is concordant with joint side, adjacent like this guide rail bar just can be realized seamless firm splicing, realize the intensive assembling of component models, can fixedly positioning and prevent skew, joint is provided with the buckle 17 engaging with crossbeam, crossbeam is fixedly connected with side box plate, base plate, cover plate by web member, ensures good globality, and each parts are related stressed even, and built-in integral disassembly, assembly is convenient, on guide rail bar, is furnished with bracket, on bracket, have the edge 18 identical with guide rail bar-shaped trough, the same one end at this upper and lower edge is connected with the fixed-wing 20 being connected with screw thread bar 19 interspersed on crossbeam, on bracket, the opposite side relative with fixed-wing is provided with vertical edge strip 21, to being provided with a fixed strip being connected with crossbeam 22 by edge strip, fixed strip is provided with the vertical slot identical with this edge strip 23.When use, build-in components module can be made to bracket size or be made into one with bracket, then be inserted in the bar-shaped trough that is fixed on guide rail bar, then fixed-wing is fixed by bolts on crossbeam, fixed strip is fixed on crossbeam with bolt at opposite side again, like this build-in components module be just fixedly mounted on built-in upper, the surrounding structure location of being strengthened, fixed-area is large, while being hit, module is stressed evenly, between member, combination firmly, even if the larger parts of quality also can strong bonded, can not cause certain a bit stressed excessive deformation or destruction syndeton, improve stability, guide rail stripe pitch can arbitrarily regulate, sized parts configuration is convenient, flexible, module is installing and built-in of when maintenance can also shift out easy to operate.
Be only preferred embodiment of the present invention in sum, all equivalence modifications of doing according to the application and prior art interpolation are all considered as the technology of the present invention category.
Claims (5)
1. an integrated test test instrument heavy duty component integration case, comprise front baffle, afterframe, side box plate, base plate and cover plate, it is characterized in that side box plate has inside flanging up and down, it is U-shaped that section is, flanging inside surface is at least provided with together the groove with parallel sided, base plate is connected with the lower flanging of two side box plates, cover plate is connected with the upper flanging of two side box plates, front baffle is connected with the front end of base plate, cover plate, two side box plates, afterframe is connected with the rear end of base plate, cover plate, two side box plates, surrounds an outer case, in casing, be provided with one built-in, built-inly set up the side connecting plate that lower limb coincide respectively in the upper and lower groove of two side box plates, between two side connecting plates, relative four jiaos connect by crossbeam, below entablature, there is pilot hole with equal array above sill, between two entablatures, between two sills, be all connected with guide rail bar opposing upper and lower, guide rail bar is made up of guide rail and two side connectors, the face that upper/lower guide bar is relative is provided with bar-shaped trough, joint is connected with guide rail by the protruding falcon that inserts guide rail hollow part, joint is provided with the reference column coordinating with pilot hole, joint is provided with the buckle engaging with crossbeam, crossbeam is fixedly connected with side box plate, base plate, cover plate by web member.
2. integrated test test instrument heavy duty component integration case according to claim 1, it is characterized in that being furnished with bracket on described guide rail bar, on bracket, have the edge identical with guide rail bar-shaped trough, the same one end at this upper and lower edge is connected with the fixed-wing being connected with crossbeam.
3. integrated test test instrument heavy duty component integration case according to claim 2, it is characterized in that opposite side relative with fixed-wing on described bracket is provided with vertical edge strip, to being provided with a fixed strip being connected with crossbeam by edge strip, fixed strip is provided with the vertical slot identical with this edge strip.
4. according to the arbitrary described integrated test test instrument heavy duty of claims 1 to 3 component integration case, it is characterized in that on described joint, reference column is more than two, equidistant with pilot hole.
5. integrated test test instrument heavy duty component integration case according to claim 4, is characterized in that described reference column is three, and the reference column of both sides is that the longitudinal profile of semicolumn is concordant with joint side along the axis semicolumn that longitudinally plane leaves.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410170883.0A CN103913187B (en) | 2014-04-26 | 2014-04-26 | Integrated test test instrument heavy duty parts integral box |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410170883.0A CN103913187B (en) | 2014-04-26 | 2014-04-26 | Integrated test test instrument heavy duty parts integral box |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103913187A true CN103913187A (en) | 2014-07-09 |
| CN103913187B CN103913187B (en) | 2016-06-29 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410170883.0A Active CN103913187B (en) | 2014-04-26 | 2014-04-26 | Integrated test test instrument heavy duty parts integral box |
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| Country | Link |
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| CN (1) | CN103913187B (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TW514339U (en) * | 2002-03-15 | 2002-12-11 | Mitac Technology Corp | Universal testing box |
| CN2549474Y (en) * | 2002-04-24 | 2003-05-07 | 神基科技股份有限公司 | Universal test box |
| CN200976013Y (en) * | 2006-11-15 | 2007-11-14 | 元弧科技股份有限公司 | Circuit board test box |
| CN201897755U (en) * | 2010-11-05 | 2011-07-13 | 中兴通讯股份有限公司 | Case |
| CN201995236U (en) * | 2011-03-15 | 2011-09-28 | 深圳市索行电子科技有限公司 | Case |
| KR101082733B1 (en) * | 2007-03-23 | 2011-11-10 | 니폰게이긴조쿠가부시키가이샤 | Electronic apparatus test box |
| CN202374612U (en) * | 2011-12-07 | 2012-08-08 | 中国航空无线电电子研究所 | Test adaptation case with built-in module mounting frame |
| CN202393401U (en) * | 2011-11-22 | 2012-08-22 | 深圳市英威腾电气股份有限公司 | Radiator test box |
| CN203811193U (en) * | 2014-04-26 | 2014-09-03 | 广西电网公司电力科学研究院 | Portable test instrument heavy-load component integrated box |
-
2014
- 2014-04-26 CN CN201410170883.0A patent/CN103913187B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TW514339U (en) * | 2002-03-15 | 2002-12-11 | Mitac Technology Corp | Universal testing box |
| CN2549474Y (en) * | 2002-04-24 | 2003-05-07 | 神基科技股份有限公司 | Universal test box |
| CN200976013Y (en) * | 2006-11-15 | 2007-11-14 | 元弧科技股份有限公司 | Circuit board test box |
| KR101082733B1 (en) * | 2007-03-23 | 2011-11-10 | 니폰게이긴조쿠가부시키가이샤 | Electronic apparatus test box |
| CN201897755U (en) * | 2010-11-05 | 2011-07-13 | 中兴通讯股份有限公司 | Case |
| CN201995236U (en) * | 2011-03-15 | 2011-09-28 | 深圳市索行电子科技有限公司 | Case |
| CN202393401U (en) * | 2011-11-22 | 2012-08-22 | 深圳市英威腾电气股份有限公司 | Radiator test box |
| CN202374612U (en) * | 2011-12-07 | 2012-08-08 | 中国航空无线电电子研究所 | Test adaptation case with built-in module mounting frame |
| CN203811193U (en) * | 2014-04-26 | 2014-09-03 | 广西电网公司电力科学研究院 | Portable test instrument heavy-load component integrated box |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103913187B (en) | 2016-06-29 |
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