CN206192249U - Aircraft part appearance verifying attachment - Google Patents
Aircraft part appearance verifying attachment Download PDFInfo
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- CN206192249U CN206192249U CN201621290949.0U CN201621290949U CN206192249U CN 206192249 U CN206192249 U CN 206192249U CN 201621290949 U CN201621290949 U CN 201621290949U CN 206192249 U CN206192249 U CN 206192249U
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Abstract
The utility model provides an aircraft part appearance verifying attachment, it relates to an outline inspection device, concretely relates to aircraft part appearance verifying attachment. The utility model discloses a solve present aircraft part appearance dimensional inspection and carry out one by one measure inspection through ordinary dipperstick to each size of part appearance by the manual work, inefficiency not only, and appear the problem of error easily. The utility model discloses a level bar, vertical chi, a plurality of horizontal location bolt and a plurality of vertical positioning bolt, the one end of level bar is connected with the one end of vertical chi, and the upper surface of level bar is equipped with a plurality of horizontal screws along its length direction is equidistant, every correspond horizontal location bolt of cartridge in the horizontal screw, be equipped with a plurality of vertical screws along its length direction is equidistant on the lateral wall of vertical chi, every correspond vertical positioning bolt of cartridge in the vertical screw. The utility model belongs to the aircraft manufacturing field.
Description
Technical field
The utility model is related to a kind of outline inspection device, and in particular to a kind of airplane parts outline inspection device, belongs to
Aircraft manufacturing field.
Background technology
The accuracy of airplane parts appearance and size directly affects the assembling in aircraft later stage, also during influence aircraft utilization
Security, therefore, the inspection to airplane parts appearance and size is especially strict.Existing airplane parts appearance and size inspection is by people
By common measuring scale, to External Shape, each size is measured inspection to work one by one, and not only efficiency is low, and easily occurs missing
Difference.
The content of the invention
The utility model is that the existing airplane parts appearance and size inspection of solution is by manually passing through common measuring scale pair
External Shape each size is measured inspection one by one, and not only efficiency is low, and the problem of error easily occurs, and then is proposed a kind of
Airplane parts outline inspection device.
The utility model is adopted the technical scheme that to solve the above problems：The utility model include horizon rule, vertical chi,
Multiple horizontal location bolts and multiple vertically oriented bolts, one end of horizon rule are connected with one end of vertical chi, horizon rule it is upper
Surface is equidistantly provided with multiple horizontal screws along its length, one horizontal location of correspondence inserting in each described horizontal screw
Bolt, is equidistantly provided with multiple screws vertically along its length on the lateral wall of vertical chi, right in each described vertical screw
A vertically oriented bolt should be inserted.
Further, the upper end of vertical chi is provided with jack, and one end of horizon rule is inserted into the jack, for fixing water
The fixing bolt of leveling ruler is inserted on the upper end end face of vertical chi.
Further, the positioning end of the positioning end of each horizontal location bolt and each vertically oriented bolt is equipped with rubber
Pad.
Further, the other end of horizon rule is provided with the first arc-shaped curved surface of evagination, and the lower end of vertical chi is provided with evagination
Second arc-shaped curved surface.
The beneficial effects of the utility model are：1st, vertical chi upper end is inserted into one end of horizon rule when the utility model is used
Jack in, and be fixed by fixing bolt, the profile according to airplane parts is inserted accordingly on horizon rule and vertical chi
The horizontal location bolt and vertically oriented bolt of quantity, the standard size controlled level bolt according to airplane parts profile are surveyed
Identical airplane parts after regulation is finished, are detected by amount end and the depth of vertically oriented bolt measurement end insertion, so may be used
Avoid using error of the ordinary measring tool every time produced by measurement；2nd, the utility model simple structure, it is easy to operate, and can have
Effect improves certainty of measurement；3rd, the detachable split of the utility model is preserved, and is easy to carry with.
Brief description of the drawings
Fig. 1 is overall structure diagram of the present utility model.
Specific embodiment
Specific embodiment one：Present embodiment, a kind of airplane parts profile inspection described in present embodiment are illustrated with reference to Fig. 1
Experiment device includes horizon rule 1, vertical chi 2, multiple horizontal location bolts 3 and multiple vertically oriented bolts 4, one end of horizon rule 1
One end with vertical chi 2 is connected, and the upper surface of horizon rule 1 is equidistantly provided with multiple horizontal screws along its length, each institute
One horizontal location bolt 3 of correspondence inserting in horizontal screw is stated, is equidistantly provided with along its length on the lateral wall of vertical chi 2
Multiple screws vertically, one vertically oriented bolt 4 of correspondence inserting in each described vertical screw.
Specific embodiment two：Present embodiment, a kind of airplane parts profile inspection described in present embodiment are illustrated with reference to Fig. 1
The upper end of the vertical chi 2 of experiment device is provided with jack, and one end of horizon rule 1 is inserted into the jack, for fixing horizon rule 1
Fixing bolt 5 is inserted on the upper end end face of vertical chi 2.Other compositions and annexation are identical with specific embodiment one.
Specific embodiment three：Present embodiment, a kind of airplane parts profile inspection described in present embodiment are illustrated with reference to Fig. 1
The positioning end of each horizontal location bolt 3 of experiment device and the positioning end of each vertically oriented bolt 4 are equipped with rubber sheet gasket 6.
Other compositions and annexation are identical with specific embodiment one.
Specific embodiment four：Present embodiment, a kind of airplane parts profile inspection described in present embodiment are illustrated with reference to Fig. 1
The other end of the horizon rule 1 of experiment device is provided with the first arc-shaped curved surface 7 of evagination, and the lower end of vertical chi 2 is provided with the second arc of evagination
Shape curved surface 8.Other compositions and annexation are identical with specific embodiment one.
The above, is only preferred embodiment of the present utility model, not makees any formal to the utility model
Limitation, although the utility model is disclosed above with preferred embodiment, but is not limited to the utility model, any ripe
Professional and technical personnel is known, is not being departed from the range of technical solutions of the utility model, when in the technology using the disclosure above
Appearance makes a little change or is modified to the Equivalent embodiments of equivalent variations, as long as being without departing from technical solutions of the utility model
Hold, according to technical spirit of the present utility model, within spirit of the present utility model and principle, what above example was made appoints
What simple modification, equivalent and improvement etc., still falls within the protection domain of technical solutions of the utility model.
Claims (4)
1. a kind of airplane parts outline inspection device, it is characterised in that：A kind of airplane parts outline inspection device includes water
Leveling ruler（1）, vertical chi（2）, multiple horizontal location bolts（3）With multiple vertically oriented bolts（4）, horizon rule（1）One end with
Vertical chi（2）One end connection, horizon rule（1）Upper surface be equidistantly provided with multiple horizontal screws along its length, each
One horizontal location bolt of correspondence inserting in the horizontal screw（3）, vertical chi（2）Lateral wall on along its length wait between
Away from multiple screws vertically are provided with, correspondence inserts a vertically oriented bolt in each described vertical screw（4）.
2. a kind of airplane parts outline inspection device according to claim 1, it is characterised in that：Vertical chi（2）Upper end set
There are jack, horizon rule（1）One end be inserted into the jack, for fixing horizon rule（1）Fixing bolt（5）It is inserted into perpendicular
Ruler（2）Upper end end face on.
3. a kind of airplane parts outline inspection device according to claim 1, it is characterised in that：Each horizontal location bolt
（3）Positioning end and each vertically oriented bolt（4）Positioning end be equipped with rubber sheet gasket（6）.
4. a kind of airplane parts outline inspection device according to claim 1, it is characterised in that：Horizon rule（1）The other end
It is provided with the first arc-shaped curved surface of evagination（7）, vertical chi（2）Lower end be provided with the second arc-shaped curved surface of evagination（8）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621290949.0U CN206192249U (en) | 2016-11-29 | 2016-11-29 | Aircraft part appearance verifying attachment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621290949.0U CN206192249U (en) | 2016-11-29 | 2016-11-29 | Aircraft part appearance verifying attachment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206192249U true CN206192249U (en) | 2017-05-24 |
Family
ID=58724119
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621290949.0U Active CN206192249U (en) | 2016-11-29 | 2016-11-29 | Aircraft part appearance verifying attachment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206192249U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109000543A (en) * | 2018-07-11 | 2018-12-14 | 安徽江淮汽车集团股份有限公司 | Gap width measuring appliance and gap shape measuring appliance |
-
2016
- 2016-11-29 CN CN201621290949.0U patent/CN206192249U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109000543A (en) * | 2018-07-11 | 2018-12-14 | 安徽江淮汽车集团股份有限公司 | Gap width measuring appliance and gap shape measuring appliance |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 519000 Room 612, 6th Floor, Office Building of Zhuhai Airport Group, Haicheng Township, Sanzao Town, Zhuhai City, Guangdong Province Patentee after: Guanglian Airlines (Zhuhai) Co., Ltd. Address before: 519000 Room 612, 6th Floor, Office Building of Zhuhai Airport Group, Haicheng Township, Sanzao Town, Zhuhai City, Guangdong Province Patentee before: Zhuhai Guanglian general aviation equipment Co. Ltd. |
|
| CP01 | Change in the name or title of a patent holder |