CN207846494U - Dead-loaded instrument - Google Patents
Dead-loaded instrument Download PDFInfo
- Publication number
- CN207846494U CN207846494U CN201721386807.9U CN201721386807U CN207846494U CN 207846494 U CN207846494 U CN 207846494U CN 201721386807 U CN201721386807 U CN 201721386807U CN 207846494 U CN207846494 U CN 207846494U
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- CN
- China
- Prior art keywords
- hood
- blocks
- side plates
- backboard
- fuselage
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- 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.)
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Abstract
The utility model provides a kind of dead-loaded instrument, it is characterised in that：With dead-loaded instrument fuselage；There are one hoods for tool, hood includes one piece of backboard, hood further includes two blocks of trapezoidal side plates being connected with backboard, the distance between two blocks of trapezoidal side plates are greater than or equal to the width of fuselage, the bevel edge of two blocks of side plates is located above, and with the minimum point that the backboard place of being connected is bevel edge, one piece of inclined top plate is connected with the top margin of the bevel edge of two blocks of side plates and backboard respectively, and above-mentioned backboard, two blocks of side plates, top plate are opaque organic plastics material；After hood is sleeved on fuselage, the liquid crystal display of fuselage upper surface is located at the lower section in the space that hood is surrounded and positioned at top plate, and button is located at except the space that hood is surrounded.Even if the utility model ambient light than it is stronger if testing crew can be allowed to be clearly seen that the content on dead-loaded instrument liquid crystal display.
Description
Technical field
The utility model is related to a kind of project quality inspection equipment, specifically a kind of dead-loaded instrument.
Background technology
When carrying out static load of pile foundation detection experiment, since experiment is all in building-site, and the detection device static load of core
Instrument is as shown in Figure 1, be a rectangular fuselage 1, upper surface has button 2, and using common liquid crystal display
3.When direct sunlight or ambient light slightly than it is stronger when, the liquid crystal display 3 of dead-loaded instrument will not see Chu, testing crew
It often to squat down and hide above the liquid crystal display 3 of dead-loaded instrument on the other hand, proficiency operation button is very inconvenient.
Utility model content
The utility model provides a kind of dead-loaded instrument, the purpose is to solve the disadvantage that the prior art, even if ambient light compares
Strongly, also testing crew can be allowed to be clearly seen that the content on dead-loaded instrument liquid crystal display.
Technical solution adopted by the utility model to solve its technical problems is：
A kind of dead-loaded instrument, it is characterised in that：With dead-loaded instrument fuselage；For tool there are one hood, hood includes one piece of back of the body
Plate, hood further include two blocks of trapezoidal side plates being connected with backboard, and the distance between two blocks of trapezoidal side plates are greater than or equal to fuselage
Width, the bevel edge of two blocks of side plates is located above, and with the minimum point that the backboard place of being connected is bevel edge, one piece of inclined top plate point
It is not connected with the top margin of the bevel edge of two blocks of side plates and backboard, above-mentioned backboard, two blocks of side plates, top plate are opaque organic plastics material
Matter；After hood is sleeved on fuselage, the liquid crystal display of fuselage upper surface is located in the space that hood is surrounded and positioned at top
The lower section of plate, button are located at except the space that hood is surrounded.
The utility model is beneficial in that：
The utility model will not influence the display effect of dead-loaded instrument display more by force because of ambient light, even if ambient light ratio
It is stronger, it can also allow testing crew to be clearly seen that the content on dead-loaded instrument liquid crystal display, operation are also more convenient.
Description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is the utility model dead-loaded instrument；
Fig. 2 is that the utility model dead-loaded instrument and hood combine.
Specific implementation mode
In order to illustrate more clearly of the technical solution of the utility model, attached drawing needed in description will be made below
Simply introduce, it should be apparent that, the accompanying drawings in the following description is only some embodiments of the utility model, for this field
For those of ordinary skill, without creative efforts, other implementations are can also be obtained according to these attached drawings
Example.
As shown in Fig. 2, the utility model reequips dead-loaded instrument fuselage appearance, a hood 4, hood are designed
4 are assembled by 4 pieces of lighttight organic plates, including one piece of backboard 41 and two pieces of 42 structures of trapezoidal side plate being connected with backboard 41
At, the distance between two blocks of trapezoidal side plates 42 are greater than or equal to the width of fuselage 1, and the bevel edge of two blocks of side plates 42 is located above, and
And with the minimum point that the place of being connected of backboard 41 is bevel edge, one piece of inclined top plate 43 bevel edge and backboard 41 with two blocks of side plates 42 respectively
Top margin be connected, the top plate 43 of the hood 4 formed in this way is inclined.
4 sets of hood on the fuselage 1 after, the liquid crystal display 3 of 1 upper surface of fuselage is located at the space that hood 4 is surrounded
Lower section interior and positioned at top plate 43, button 2 are located at except the space that hood 4 is surrounded.Hood 4 can just entangle in this way
The top half of the fuselage 1 of dead-loaded instrument, since button 2 is in the lower half portion of the fuselage 1 of dead-loaded instrument, so not interfering with experiment
Personnel's operation button 2.And the inclination of top plate 43 of the top has a certain degree, you can to obstruct the light, and will not block experiment
Personnel check the sight of 3 data of liquid crystal display.Since hood 4 is the upper surface of the fuselage 1 for being sleeved on dead-loaded instrument, test
Cheng Hou, hood 4 can be removed at any time, do not interfere with dead-loaded instrument and reinstall in chest.
Each embodiment is described by the way of progressive in this specification, the highlights of each of the examples are with other
The difference of embodiment, just to refer each other for identical similar portion between each embodiment.To the upper of the disclosed embodiments
State it is bright, enable professional and technical personnel in the field realize or use the utility model.Various modifications to these embodiments pair
It will be apparent for those skilled in the art, the general principles defined herein can not depart from this reality
In the case of with novel spirit or scope, realize in other embodiments.Therefore, the utility model is not intended to be limited to this
These embodiments shown in text, and it is to fit to widest range consistent with the principles and novel features disclosed in this article.
Claims (1)
1. a kind of dead-loaded instrument, it is characterised in that：With dead-loaded instrument fuselage；For tool there are one hood, hood includes one piece of backboard,
Hood further includes two blocks of trapezoidal side plates being connected with backboard, and the distance between two blocks of trapezoidal side plates are greater than or equal to the width of fuselage
Degree, the bevel edge of two blocks of side plates is located above, and with the minimum point that the backboard place of being connected is bevel edge, one piece of inclined top plate respectively with
The bevel edge of two blocks of side plates and the top margin of backboard are connected, and above-mentioned backboard, two blocks of side plates, top plate are opaque organic plastics material；
After hood is sleeved on fuselage, the liquid crystal display of fuselage upper surface is located in the space that hood is surrounded and positioned at top plate
Lower section, button are located at except the space that hood is surrounded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721386807.9U CN207846494U (en) | 2017-10-26 | 2017-10-26 | Dead-loaded instrument |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721386807.9U CN207846494U (en) | 2017-10-26 | 2017-10-26 | Dead-loaded instrument |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207846494U true CN207846494U (en) | 2018-09-11 |
Family
ID=63426403
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721386807.9U Active CN207846494U (en) | 2017-10-26 | 2017-10-26 | Dead-loaded instrument |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207846494U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112227428A (en) * | 2020-09-21 | 2021-01-15 | 台州市建设市政工程检测中心有限公司 | Static load tester with protection mechanism |
-
2017
- 2017-10-26 CN CN201721386807.9U patent/CN207846494U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112227428A (en) * | 2020-09-21 | 2021-01-15 | 台州市建设市政工程检测中心有限公司 | Static load tester with protection mechanism |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |