CN202470977U - Airplane part profile verifying apparatus - Google Patents
Airplane part profile verifying apparatus Download PDFInfo
- Publication number
- CN202470977U CN202470977U CN2012200147549U CN201220014754U CN202470977U CN 202470977 U CN202470977 U CN 202470977U CN 2012200147549 U CN2012200147549 U CN 2012200147549U CN 201220014754 U CN201220014754 U CN 201220014754U CN 202470977 U CN202470977 U CN 202470977U
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- Prior art keywords
- detection
- detects
- frock
- hole
- rear side
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- Expired - Lifetime
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- 238000001514 detection method Methods 0.000 claims abstract description 49
- 210000002421 cell wall Anatomy 0.000 claims description 12
- 238000007689 inspection Methods 0.000 claims description 11
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000004519 manufacturing process Methods 0.000 abstract 1
- 230000000712 assembly Effects 0.000 description 4
- 238000000429 assembly Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
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Abstract
The utility model relates to an airplane part profile verifying apparatus, belonging to the field of part verifying apparatus, comprising a first detection tool and a second detection tool, characterized in that between the front side surface of the first detection tool and the rear side surface of the first detection tool there is provided a first detection hole, and the top end of the second detection tool is provided with a second detection groove. Compared with the prior art, the beneficial effects of the utility model are that the airplane part profile verifying apparatus can enable people to use the first and second detection tools to rapidly verify that whether the profile of a part to be verified is in accord with requirements or not, and the airplane part profile verifying apparatus is simple in structure, easy in manufacture, very convenient in use and rapid in detection speed, thereby greatly increasing detection efficiency, and effectively reducing the workload of verifying personnel.
Description
Technical field
The utility model relates to a kind of verifying attachment of part, more specifically to a kind of outline inspection device of airplane parts.
Background technology
Existing Large Civil Aircraft is assembled by ten hundreds of spare and accessory parts usually, and is because Large Civil Aircraft aloft flies, therefore in order to guarantee the flight safety of Large Civil Aircraft, very high to the requirement of the various parameters of spare and accessory parts.In these spare and accessory parts, some little parts and the fairly simple part of some profiles are measured easily, and big, the profile more complicated of some spare and accessory parts sizes is difficult to measure with conventional measurement in addition.
Part a kind of to be measured as shown in Figure 2; This part to be measured comprises brace and two " U " shape assemblies; The base of two " U " shape assemblies is oppositely arranged; The two ends of brace connect the base of two " U " shape assemblies respectively, and the angle on the base of brace and each " U " shape assembly is slightly larger than 90 degree.In said two " U " shape assemblies, what be positioned at the left side is first " U " shape assembly, what be positioned at the right is second " U " shape assembly.Said first " U " shape assembly comprises first base plate, first front panel, the first rear side panel, and the two ends of first base plate connect the first front panel right-hand member, the first rear side panel right-hand member respectively.Second " U " shape assembly comprises second base plate, second front panel, the second rear side panel, and the two ends of second base plate connect the second front panel left end, the second rear side panel left end respectively.
Because the profile of this part to be measured is rule not too, so detect cumbersomely, need the time and the manpower of labor.
Summary of the invention
The utility model technical matters to be solved provides a kind of outline inspection device of airplane parts, and the outline inspection device of this airplane parts can detect above-mentioned part to be measured fast.The technical scheme that adopts is following:
A kind of outline inspection device of airplane parts; Comprise that first detects the frock and the second detection frock; It is characterized in that: the said first detection frock leading flank and first detects between the frock trailing flank and has the first detection hole, and said second detects the frock top has the second detection groove.
The said first detection hole comprises that first front panel and the first rear side face plate configuration detect the hole, the brace profile detects hole, second front panel and the second rear side face plate configuration and detects the hole, and first front panel and first rear side face plate configuration detection hole, brace profile detection hole, second front panel and the second rear side face plate configuration detect the hole and be communicated with, form the first detection hole successively.Said first front panel and the first rear side face plate configuration detect the hole can detect the first front panel end to the width of the distance of first base plate, first front panel, the first rear side panel end to the distance of first base plate, the parameters such as width of the first rear side panel.The brace profile detects the hole can detect parameters such as the length of brace, thickness.Second front panel and the second rear side face plate configuration detect the hole can detect can detect the second front panel end to the width of the distance of second base plate, second front panel, the second rear side panel end to the distance of second base plate, the parameters such as width of the second rear side panel.
Said second detects groove comprises that the first base plate medial surface detects cell wall, cell wall, second base plate medial surface detection cell wall are detected in the brace bottom surface.The said first base plate medial surface can detect the angle of width, first base plate and brace that cell wall detects the first base plate medial surface.The length that cell wall detects brace can be detected in the brace bottom surface.The second base plate medial surface detects the angle that cell wall can detect width, second base plate and the brace of the second base plate medial surface.
More excellent scheme, said first detects the left end of the left end of frock through the left web member connection second detection frock, and the right-hand member of the said first detection frock detects the right-hand member of frock through right web member connection second.Be convenient to like this deposit, can effectively avoid the first detection frock or second to detect frock and lose.
The utility model beneficial effect against existing technologies is; Because whether the profile that the first detection frock and the second detection frock can let people's fast detecting go out part to be measured meets the requirements, it is simple in structure, is easy to make; Very easy to use; Detection speed is fast, has significantly improved the efficient that detects, and has effectively reduced testing staff's workload.
Description of drawings
Fig. 1 is the structural representation of the utility model embodiment 1;
Fig. 2 is the structural representation of part to be measured;
Fig. 3 is the user mode reference diagram of the utility model embodiment 1;
Fig. 4 is the structural representation of the utility model embodiment 2.
Embodiment
Embodiment 1
As shown in Figure 1; The outline inspection device of the airplane parts in the present embodiment; Comprise that first detects the frock 1 and the second detection frock 2, the said first detection frock leading flank and first detects between the frock trailing flank and has the first detection hole 3, and the said second detection frock top has second and detects groove 4.
The said first detection hole 3 comprises first front panel and first rear side face plate configuration detection hole 301, the brace profile detects hole 302, second front panel and second rear side face plate configuration detection hole 303, the first front panels and the first rear side face plate configuration detects hole 301, the brace profile detects hole 302, second front panel and second rear side face plate configuration detection hole 303 and is communicated with, forms the first detection hole 3 successively.
Said second detects groove 4 comprises that the first base plate medial surface detects cell wall 401, cell wall 402, second base plate medial surface detection cell wall 403 are detected in the brace bottom surface.
Said first detects the left end of the left end of frock 1 through the left web member 5 connections second detection frock 2, and the right-hand member of the said first detection frock 1 detects the right-hand member of frock 2 through right web member 6 connections second.Be convenient to like this deposit, can effectively avoid the first detection frock 1 or second to detect frock 2 and lose.
When detecting, can detect two parts to be measured simultaneously, as shown in Figure 3.
Embodiment 2
As shown in Figure 4, the outline inspection device of the airplane parts in the present embodiment and the difference of embodiment 1 are: the first detection frock 1 and second detects frock 2 and is not fixed together, and they are deposited separately and use.
Claims (4)
1. the outline inspection device of an airplane parts; Comprise that first detects the frock and the second detection frock; It is characterized in that: the said first detection frock leading flank and first detects between the frock trailing flank and has the first detection hole, and said second detects the frock top has the second detection groove.
2. the outline inspection device of airplane parts as claimed in claim 1; It is characterized in that: the said first detection hole comprises that first front panel and the first rear side face plate configuration detect the hole, the brace profile detects hole, second front panel and the second rear side face plate configuration and detects the hole, and first front panel and first rear side face plate configuration detection hole, brace profile detection hole, second front panel and the second rear side face plate configuration detect the hole and be communicated with, form the first detection hole successively.
3. the outline inspection device of airplane parts as claimed in claim 2 is characterized in that: said second detects groove comprises that the first base plate medial surface detects that cell wall, brace bottom surface detect cell wall, the second base plate medial surface detects cell wall.
4. the outline inspection device of airplane parts as claimed in claim 3; It is characterized in that: said first detects the left end of the left end of frock through the left web member connection second detection frock, and the right-hand member of the said first detection frock detects the right-hand member of frock through right web member connection second.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012200147549U CN202470977U (en) | 2012-01-12 | 2012-01-12 | Airplane part profile verifying apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012200147549U CN202470977U (en) | 2012-01-12 | 2012-01-12 | Airplane part profile verifying apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202470977U true CN202470977U (en) | 2012-10-03 |
Family
ID=46919131
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012200147549U Expired - Lifetime CN202470977U (en) | 2012-01-12 | 2012-01-12 | Airplane part profile verifying apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202470977U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105157534A (en) * | 2015-08-24 | 2015-12-16 | 苏州骏发精密机械有限公司 | Product shaping test tool |
-
2012
- 2012-01-12 CN CN2012200147549U patent/CN202470977U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105157534A (en) * | 2015-08-24 | 2015-12-16 | 苏州骏发精密机械有限公司 | Product shaping test tool |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20121003 |
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| CX01 | Expiry of patent term |