CN209112465U - A kind of Aircraft Tools fix device with internal frame - Google Patents
A kind of Aircraft Tools fix device with internal frame Download PDFInfo
- Publication number
- CN209112465U CN209112465U CN201821961029.6U CN201821961029U CN209112465U CN 209112465 U CN209112465 U CN 209112465U CN 201821961029 U CN201821961029 U CN 201821961029U CN 209112465 U CN209112465 U CN 209112465U
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- sliding
- support
- internal
- external
- supporting rod
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Abstract
The utility model discloses a kind of Aircraft Tools to fix device with internal frame, including curved support sliding rail, external sliding slot is provided on the outside of the curved support sliding rail, internal sliding slot is provided on the inside of the curved support sliding rail, the side of the external sliding slot is equipped with external support sliding block, the side of the internal sliding slot is equipped with mobile support rod, the utility model is scientific and reasonable for structure, it is safe and convenient to use, it is provided with curved support sliding rail, stable support effect can be provided for device by curved support sliding rail, guarantee the stability of device, sliding block can be made to make turnover along sliding rail simultaneously to move, facilitate the position of adjustment support rod, improve the flexibility that fixed device uses, keep its applicability higher, it is provided with telescopic supporting rod, telescopic supporting rod can freely adjust height, when meeting Aircraft Tools, different height requirements, it is not necessarily to Fixed operation can be completed in the fixation device of addition different height, improves the efficiency of work.
Description
Technical field
The utility model relates to aircraft assembly equipment technical field, specially a kind of Aircraft Tools fix device with internal frame.
Background technique
The manufacturing process of aircraft is by component assembly into component, is assembled into component by component, then be butted into complete machine by component.
The manufacture assembly tooling of aircraft is a kind of Cooperative process design, mainly include process modeling establishment, technique list pattern customization and
Generation, Work Process Management, Process knowledge database maintenance and the functions such as use, it is the indispensable dress of airplane parts manufacture and assembly
It is standby, it is one of key technology of aircraft manufacturing.To some degree, the Fixture Design of Aviation Enterprise and manufacture level represent
The aircraft manufacturing of enterprise is horizontal.The housing construction of aircraft is mainly made of sheet metal component of various shapes, and assembly technology equipment is
Guarantee the basis of airplane component positioning, installation, riveting.On conventional aircraft rigger skill equipment, airplane component be with
Origin reference location part on technological equipment positions, and these setting elements are usually that technique dress is fixed on by different media
On standby matrix, using aircraft product as the object of adjustment, by adjusting the related geometric element on aircraft product, be allowed to realize and
Positioning datum on technological equipment is overlapped, and finds correct position of the product in technological equipment accurately with this.Therefore fixed device is flying
It is very important during the tooling of machine.
But the fixed device design of internal frame at present on the market more falls behind, fixed height and range is not adjustable,
During assembly, being easy to appear some positions can not vacantly be supported, or need more fixation device to reach using mesh
, the efficiency of assembly is reduced, while also resulting in the waste of resource, and the hanging part in assembly, is easy to happen danger,
And the quality of assembly and the time of assembly are extremely influenced, fixes device with internal frame so being badly in need of a kind of Aircraft Tools to solve this
A problem.
Utility model content
The utility model provides a kind of Aircraft Tools and fixes device with internal frame, can effectively solve to mention in above-mentioned background technique
The fixed device design of internal frame on the market at present more fall behind, fixed height and range is not adjustable, in the process of assembly
In, being easy to appear some positions can not vacantly support, or need more fixation device to reach using purpose, reduce dress
The efficiency matched, while the waste of resource is also resulted in, and the hanging part in assembly, it is easy to happen danger, and extremely shadow
The problem of ringing the time of the quality and assembly assembled.
To solve the above-mentioned problems, the utility model provides the following technical solutions: a kind of Aircraft Tools fix dress with internal frame
Set, including curved support sliding rail, be provided with external sliding slot on the outside of the curved support sliding rail, the curved support sliding rail it is interior
Side is provided with internal sliding slot, and the side of the external sliding slot is equipped with external support sliding block, the side installation of the internal sliding slot
There is mobile support rod, the side of the mobile support rod is equipped with internal support slipper, is equipped on the external support sliding block
External telescopic supporting rod, the upper end of the external telescopic supporting rod are equipped with external support claw, on the external support claw
Fastening bolt one is installed, the side of the fastening bolt one is equipped with turning handle one, the upper end installation of the internal support slipper
There is internal telescopic supporting rod, the side of the internal telescopic supporting rod is equipped with internal support claw, the internal support claw
On fastening bolt two is installed, the side of the fastening bolt two is equipped with turning handle two, the external sliding slot and internal sliding slot
It is inside provided with limit slideway, the side of the external support sliding block is provided with fixed jaw, and the external support inner side of slider is set
It is equipped with sliding handle, the side of the sliding handle is provided with position limiting slide block, is provided with sliding handle one on the inside of the internal support slipper, described
The side of sliding handle one is provided with position limiting slide block one, and the other side of the internal support slipper is provided with sliding handle two, the sliding handle two
Side be provided with position limiting slide block two, longitudinal two sides of the mobile support rod are provided with limit sliding chutes, in the limit sliding chutes
It is provided with limit slideway, the both lateral sides of the mobile support rod are provided with sliding handle three, and the side setting of the sliding handle three is limited
Position sliding block three.
Preferably, positioning pin is provided on the external support sliding block and internal support slipper.
Preferably, limit hole and limit are provided on the external telescopic supporting rod and internal telescopic supporting rod
Pin.
Preferably, the external support sliding block and external telescopic supporting rod and internal support slipper and internal retractable support
Pass through welded connecting between bar.
Preferably, anti-skid chequer is provided on the turning handle one and turning handle two.
Preferably, the curved support sliding rail is sectional design, is divided into curved track and straight rail.
Compared with prior art, the utility model has the beneficial effects that the utility model is scientific and reasonable for structure, use is safe
It is convenient:
1, it is provided with curved support sliding rail, stable support effect can be provided for device by curved support sliding rail, is protected
The stability of card device, while sliding block can be made to make turnover along sliding rail and moved, facilitate the position of adjustment support rod, support rod can be made to exist
Arbitrary adjustment movement is carried out in device fixed range, is improved the flexibility that fixed device uses, is kept its applicability higher, fits
Range is wider.
2, it is provided with telescopic supporting rod, by being provided with the cooperation of limit hole and spacer pin on telescopic supporting rod, can be made
Telescopic supporting rod can freely adjust height, when meeting Aircraft Tools, different height requirement, without adding consolidating for different height
Determining device can be completed fixed operation, improve the efficiency of work, while also save resource.
3, it is provided with mobile support rod, internal support is provided on mobile support rod, mobile support rod can be in curved support
The inside of sliding rail automatically moves, while the sliding block being arranged on mobile support rod can move freely on mobile support rod, use
When, effective support is provided for the space on the inside of curved support sliding rail, makes fixed device when in use, it, can in fixed range
To accomplish that no dead angle is fixed, the scope of application of fixed stability and device is improved.
Detailed description of the invention
Attached drawing is used to provide a further understanding of the present invention, and constitutes part of specification, practical with this
Novel embodiment is used to explain the utility model together, does not constitute limitations of the present invention.
In the accompanying drawings:
Fig. 1 is the appearance diagram of the utility model；
Fig. 2 is the curved support sliding rail cross-sectional view of the utility model；
Fig. 3 is the external support slide block schematic diagram of the utility model；
Fig. 4 is the inside support slipper schematic diagram of the utility model；
Fig. 5 is the mobile support rod schematic diagram of the utility model；
Figure label: 1, curved support sliding rail；2, external sliding slot；3, internal sliding slot；4, external support sliding block；5, mobile branch
Strut；6, internal support slipper；7, external telescopic supporting rod；8, external support claw；9, fastening bolt one；10, turning handle one；
11, internal telescopic supporting rod；12, internal support claw；13, fastening bolt two；14, turning handle two；15, slideway is limited；16, fixed
Pawl；17, sliding handle；18, position limiting slide block；19, sliding handle one；20 position limiting slide blocks one；21, sliding handle two；22, position limiting slide block two；23, it limits
Sliding slot；24, sliding handle three；25, position limiting slide block three.
Specific embodiment
It is illustrated below in conjunction with preferred embodiment of the attached drawing to the utility model, it should be understood that described herein excellent
It selects embodiment to be only used for describing and explaining the present invention, is not used to limit the utility model.
Embodiment: as shown in Figs. 1-5, a kind of Aircraft Tools fix device, including curved support sliding rail 1 with internal frame, in order to
Facilitate the installation and maintenance of device, curved support sliding rail 1 is sectional design, is divided into curved track and straight rail, curved support
The outside of sliding rail 1 is provided with external sliding slot 2, and the inside of curved support sliding rail 1 is provided with internal sliding slot 3, the side of external sliding slot 2
External support sliding block 4 is installed, the side of internal sliding slot 3 is equipped with mobile support rod 5, and the side of mobile support rod 5 is equipped with
Internal support slipper 6, in order to guarantee stability that device is provided a supporting role at an arbitrary position, external support sliding block 4 and
It is provided with positioning pin on internal support slipper 6, external telescopic supporting rod 7, the flexible branch in outside are installed on external support sliding block 4
The upper end of strut 7 is equipped with external support claw 8, and fastening bolt 1 is equipped on external support claw 8, fastening bolt 1
Side is equipped with turning handle 1, and the upper end of internal support slipper 6 is equipped with internal telescopic supporting rod 11, in order to guarantee retractable support
Bar can be fixed in arbitrary height, be provided with limit hole and limit on external telescopic supporting rod 7 and internal telescopic supporting rod 11
Position pin, in order to further increase the stabilization and safety of device, external support sliding block 4 and outside telescopic supporting rod 7 and interior
By being welded to connect between portion's support slipper 6 and internal telescopic supporting rod 11, the side of internal telescopic supporting rod 11 is equipped with
Inside support claw 12, inside support and are equipped with fastening bolt 2 13 on claw 12, and the side of fastening bolt 2 13, which is equipped with, to be turned
Handle 2 14 is provided with anti-skid chequer, external sliding slot 2 in order to facilitate the fixation and use of device on turning handle 1 and turning handle 2 14
And limit slideway 15 is provided in internal sliding slot 3, the side of external support sliding block 4 is provided with fixed jaw 16, external support
Sliding handle 17 is provided on the inside of sliding block 4, the side of sliding handle 17 is provided with position limiting slide block 18, and the inside of internal support slipper 6 is provided with
Sliding handle 1, the side of sliding handle 1 are provided with position limiting slide block 1, and the other side of internal support slipper 6 is provided with sliding handle two
21, the side of sliding handle 2 21 is provided with position limiting slide block 2 22, and longitudinal two sides of mobile support rod 5 are provided with limit sliding chutes 23, limit
Limit slideway 15 is provided in the sliding slot 23 of position, the both lateral sides of mobile support rod 5 are provided with sliding handle 3 24, the side of sliding handle 3 24
It is provided with position limiting slide block 3 25.
The working principle and process for using of the utility model: when fixed using present apparatus progress internal frame, first according to reality
The fixed of border needs, and by adjusting the position of external support sliding block 4, mobile support rod 5 and internal support slipper 6, reaches it
To suitable position, while height as needed, adjust the height of external telescopic supporting rod 7 and internal telescopic supporting rod 11
Degree, reaches suitable height, facilitates external telescopic supporting rod 7 and internal telescopic supporting rod 11 that can provide better branch
Support effect after the completion of adjustment, is fixed internal frame by external support claw 8 and internal support claw 12, and pass through fastening
Bolt 1, fastening bolt 2 13 and turning handle 1 and turning handle 2 14 are fixed, and guarantee its stability fixed, fastening
After the completion, the fixation to aircraft internal frame is completed.
Finally, it should be noted that being not limited to this reality the foregoing is merely the preferred embodiment of the utility model
With novel, although the utility model is described in detail with reference to the foregoing embodiments, come for those skilled in the art
Say, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic into
Row equivalent replacement.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on, should all
It is included within the scope of protection of this utility model.
Claims (6)
1. a kind of Aircraft Tools fix device, including curved support sliding rail (1) with internal frame, it is characterised in that: the curved support
It is provided on the outside of sliding rail (1) external sliding slot (2), is provided with internal sliding slot (3), institute on the inside of the curved support sliding rail (1)
The side for stating external sliding slot (2) is equipped with external support sliding block (4), and the side of the internal sliding slot (3) is equipped with mobile support
The side of bar (5), the mobile support rod (5) is equipped with internal support slipper (6), is installed on the external support sliding block (4)
Have external telescopic supporting rod (7), the upper end of the external telescopic supporting rod (7) is equipped with external support claw (8), the outside
Fastening bolt one (9) is installed in support claw (8), the side of the fastening bolt one (9) is equipped with turning handle one (10), described
The upper end of internal support slipper (6) is equipped with internal telescopic supporting rod (11), the side peace of the internal telescopic supporting rod (11)
Claw (12) are supported equipped with inside, fastening bolt two (13), the fastening bolt are installed on internal support claw (12)
The side of two (13) is equipped with turning handle two (14), is provided with limit slideway in the external sliding slot (2) and internal sliding slot (3)
(15), the side of the external support sliding block (4) is provided with fixed jaw (16), is provided on the inside of the external support sliding block (4)
The side of sliding handle (17), the sliding handle (17) is provided with position limiting slide block (18), is provided on the inside of the internal support slipper (6)
Sliding handle one (19), the side of the sliding handle one (19) are provided with position limiting slide block one (20), the internal support slipper (6) it is another
Side is provided with sliding handle two (21), and the side of the sliding handle two (21) is provided with position limiting slide block two (22), the mobile support rod (5)
Longitudinal two sides be provided with limit sliding chutes (23), limit slideway (15), the mobile branch are provided in the limit sliding chutes (23)
The both lateral sides of strut (5) are provided with sliding handle three (24), and the side of the sliding handle three (24) is provided with position limiting slide block three (25).
2. a kind of Aircraft Tools according to claim 1 fix device with internal frame, it is characterised in that: the external support is sliding
Positioning pin is provided on block (4) and internal support slipper (6).
3. a kind of Aircraft Tools according to claim 1 fix device with internal frame, it is characterised in that: the flexible branch in the outside
Limit hole and spacer pin are provided on strut (7) and internal telescopic supporting rod (11).
4. a kind of Aircraft Tools according to claim 1 fix device with internal frame, it is characterised in that: the external support is sliding
Pass through welding between block (4) and external telescopic supporting rod (7) and internal support slipper (6) and internal telescopic supporting rod (11)
Connection.
5. a kind of Aircraft Tools according to claim 1 fix device with internal frame, it is characterised in that: the turning handle one (10)
And anti-skid chequer is provided on turning handle two (14).
6. a kind of Aircraft Tools according to claim 1 fix device with internal frame, it is characterised in that: the curved support is sliding
Rail (1) is sectional design, is divided into curved track and straight rail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821961029.6U CN209112465U (en) | 2018-11-26 | 2018-11-26 | A kind of Aircraft Tools fix device with internal frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821961029.6U CN209112465U (en) | 2018-11-26 | 2018-11-26 | A kind of Aircraft Tools fix device with internal frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209112465U true CN209112465U (en) | 2019-07-16 |
Family
ID=67206569
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821961029.6U Expired - Fee Related CN209112465U (en) | 2018-11-26 | 2018-11-26 | A kind of Aircraft Tools fix device with internal frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209112465U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112660412A (en) * | 2021-01-07 | 2021-04-16 | 中国航空工业集团公司北京长城航空测控技术研究所 | Shape-preserving tool for large part with adjustable weak rigidity and supporting method for aircraft cylinder section |
-
2018
- 2018-11-26 CN CN201821961029.6U patent/CN209112465U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112660412A (en) * | 2021-01-07 | 2021-04-16 | 中国航空工业集团公司北京长城航空测控技术研究所 | Shape-preserving tool for large part with adjustable weak rigidity and supporting method for aircraft cylinder section |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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: 20190716 Termination date: 20201126 |