CN210254885U - Aviation service equipment manufacturing tool - Google Patents
Aviation service equipment manufacturing tool Download PDFInfo
- Publication number
- CN210254885U CN210254885U CN201921207692.1U CN201921207692U CN210254885U CN 210254885 U CN210254885 U CN 210254885U CN 201921207692 U CN201921207692 U CN 201921207692U CN 210254885 U CN210254885 U CN 210254885U
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- CN
- China
- Prior art keywords
- positioning
- seat
- fixed
- plate spring
- battery support
- Prior art date
- 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.)
- Expired - Fee Related
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 22
- 238000009434 installation Methods 0.000 claims abstract description 7
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model relates to a aviation service equipment manufacturing frock, including frame, front panel mount pad, the anterior location mount pad of wallboard, front panel supporting seat, the first fixing base of preceding leaf spring, preceding leaf spring second fixing base, panel board positioning seat, the first installation positioning seat of storage battery support, storage battery support second installation positioning seat, oil tank supporting seat, the first fixing base of back leaf spring, wallboard rear portion location mount pad, back leaf spring second fixing base and back tailboard mount pad. Use the utility model discloses can be fast accurate equipment welded aviation service equipment, can shorten production cycle and improve product quality effectively.
Description
Technical Field
The utility model relates to a aviation service equipment manufacture equipment, specifically speaking are aviation service equipment manufacture frock.
Background
With the continuous upgrading of the industry, the efficiency requirements of enterprises on product production are continuously improved, and workers face various challenges on the control of the production quality and the production time of products. The current aviation service equipment is formed by manual welding, various defects of large error, strong quality difference, long time and long production period are easily caused, and the product faces the risk of low competitiveness.
Disclosure of Invention
The utility model aims at overcoming the not enough of existence among the prior art, provide one kind can be fast accurate equipment welded aviation service equipment, can effectively shorten production cycle and improve product quality's aviation service equipment manufacturing frock.
According to the technical scheme provided by the utility model, the aviation service equipment manufacturing tool comprises a frame, a front panel mounting seat is fixed on the upper surface of the frame, a wallboard front positioning mounting seat is fixed on the upper surface of the frame behind the front panel mounting seat, a front panel supporting seat is fixed on the upper surface of the frame behind the wallboard front positioning mounting seat, a front leaf spring first fixing seat is fixed on the upper surface of the frame behind the wallboard front positioning mounting seat, a front leaf spring second fixing seat is fixed on the frame behind the front leaf spring first fixing seat, an instrument panel positioning seat is fixed on the frame behind the front leaf spring second fixing seat, a battery support first mounting positioning seat is fixed on the frame on the right side behind the instrument panel positioning seat, a battery support second mounting positioning seat is fixed on the frame on the left behind the instrument panel positioning seat, an oil tank is fixed on the frame on the left behind the battery support second mounting positioning seat, the frame behind the first installation positioning seat of storage battery support and the second installation positioning seat of storage battery support intermediate position is fixed with the first fixing base of back leaf spring, is fixed with wallboard rear portion location mount pad in the frame behind the first fixing base of back leaf spring, is fixed with back leaf spring second fixing base in the frame behind wallboard rear portion location mount pad, is fixed with the back tailboard mount pad in the frame behind back leaf spring second fixing base.
First front plate spring positioning blocks are fixed on the left side and the right side of the upper surface of the first front plate spring fixing seat, and first front plate spring positioning holes are formed in the first front plate spring positioning blocks.
And a second front plate spring positioning block is fixed at the upper end part of the left side wall and the upper end part of the right side wall of the front plate spring second fixing seat, and a second front plate spring positioning hole is formed in the second front plate spring positioning block.
A first storage battery support positioning block is fixed on the upper surface of the first mounting and positioning seat of the storage battery support, and a first storage battery support positioning hole is formed in the first storage battery support positioning block.
And a second storage battery support positioning block is fixed on the upper surface of the second mounting and positioning seat of the storage battery support, and a second storage battery support positioning hole is formed in the second storage battery support positioning block.
First rear plate spring positioning plates are fixed to the upper end portion of the left side wall and the upper end portion of the right side wall of the first rear plate spring fixing seat respectively, and first rear plate spring positioning holes are formed in the first rear plate spring positioning plates.
And second rear plate spring positioning plates are fixed at the upper end parts of the left side wall and the right side wall of the rear plate spring second fixing seat, and second rear plate spring positioning holes are formed in the second rear plate spring positioning plates.
Use the utility model discloses can be fast accurate equipment welded aviation service equipment, can shorten production cycle and improve product quality effectively.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Detailed Description
The present invention will be further described with reference to the following specific embodiments.
The utility model discloses a aviation service equipment manufacturing tool, including frame 1, the upper surface of frame 1 is fixed with front panel mount pad 2, the upper surface of frame 1 behind front panel mount pad 2 is fixed with wallboard front positioning mount pad 3, the upper surface of frame 1 behind wallboard front positioning mount pad 3 is fixed with front panel supporting seat 4, the upper surface of frame 1 behind wallboard front positioning mount pad 3 is fixed with front leaf spring first fixing seat 51, the frame 1 behind front leaf spring first fixing seat 51 is fixed with front leaf spring second fixing seat 52, the frame 1 behind front leaf spring second fixing seat 52 is fixed with panel board positioning seat 6, the frame 1 on the right side behind panel board positioning seat 6 is fixed with battery support first mounting positioning seat 71, the frame 1 on the left behind panel board positioning seat 6 is fixed with battery support second mounting positioning seat 72, an oil tank supporting seat 8 is fixed on a rack 1 on the left side of a second mounting and positioning seat 72 of the battery support, a first rear plate spring fixing seat 91 is fixed on a rack 1 behind the middle positions of the first mounting and positioning seat 71 and the second mounting and positioning seat 72 of the battery support, a wallboard rear positioning and mounting seat 10 is fixed on the rack 1 behind the first rear plate spring fixing seat 91, a second rear plate spring fixing seat 92 is fixed on the rack 1 behind the wallboard rear positioning and mounting seat 10, and a rear tail plate mounting seat 11 is fixed on the rack 1 behind the second rear plate spring fixing seat 92.
First front plate spring positioning blocks 511 are fixed to the left and right sides of the upper surface of the front plate spring first fixing seat 51, and first front plate spring positioning holes 512 are formed in the first front plate spring positioning blocks 511.
A second front plate spring positioning block 521 is fixed to both the upper end of the left side wall and the upper end of the right side wall of the front plate spring second fixing seat 52, and a second front plate spring positioning hole 522 is formed in the second front plate spring positioning block 521.
A first battery support positioning block 711 is fixed on the upper surface of the first battery support mounting and positioning seat 71, and a first battery support positioning hole 712 is formed in the first battery support positioning block 711.
A second battery support positioning block 721 is fixed on the upper surface of the second battery support mounting positioning seat 72, and a second battery support positioning hole 722 is formed on the second battery support positioning block 721.
A first rear plate spring positioning plate 911 is fixed to both the left side wall upper end portion and the right side wall upper end portion of the rear plate spring first fixing seat 91, and a first rear plate spring positioning hole 912 is formed in the first rear plate spring positioning plate 911.
A second rear plate spring positioning plate 921 is fixed to both the left side wall upper end portion and the right side wall upper end portion of the rear plate spring second fixing seat 92, and a second rear plate spring positioning hole 922 is formed in the second rear plate spring positioning plate 921.
In the utility model, the front panel must be close to the front panel mounting seat 2 when mounting, the front panel front positioning mounting seat 3 is used for positioning the front part of the wallboard when mounting the wallboard, the wallboard rear positioning mounting seat 10 is used for positioning the rear part of the wallboard when mounting the wallboard, the front panel support seat 4 is used for supporting the front panel when mounting the front panel, the first front plate spring fixing seat 51 and the second front plate spring fixing seat 52 are used for fixing the front plate spring, the first front plate spring positioning hole 512 on the first front plate spring positioning block 511 is used for positioning the longitudinal fixing position of the front plate spring, the second front plate spring positioning hole 522 on the second front plate spring positioning block 521 is used for positioning the transverse fixing position of the front plate spring, the instrument panel positioning seat 6 is used for positioning when mounting the instrument panel, the first battery support positioning block 711 and the first battery support positioning hole 712, the second battery support positioning block 721 and the second, the first fixing seat 91 of the rear plate spring and the second fixing seat 92 of the rear plate spring are used for installing the rear plate spring, the first rear plate spring positioning hole 912 on the first rear plate spring positioning plate 911 and the second rear plate spring positioning hole 922 on the second rear plate spring positioning plate 921 are used for positioning the rear plate spring when installing, the oil tank supporting seat 8 is used for supporting the oil tank when installing, and the rear tail plate must be tightly attached to the rear tail plate installing seat 11 when installing.
Claims (7)
1. The utility model provides a tool for manufacturing aviation service equipment, includes frame (1), characterized by: a front panel mounting seat (2) is fixed on the upper surface of a rack (1), a wallboard front positioning mounting seat (3) is fixed on the upper surface of the rack (1) at the rear of the front panel mounting seat (2), a front panel supporting seat (4) is fixed on the upper surface of the rack (1) at the left side of the wallboard front positioning mounting seat (3), a front plate spring first fixing seat (51) is fixed on the upper surface of the rack (1) at the rear of the wallboard front positioning mounting seat (3), a front plate spring second fixing seat (52) is fixed on the rack (1) at the rear of the front plate spring first fixing seat (51), a dashboard positioning seat (6) is fixed on the rack (1) at the rear of the dashboard positioning seat (6), a battery support first mounting positioning seat (71) is fixed on the rack (1) at the rear right side of the dashboard positioning seat (6), a battery support second mounting positioning seat (72) is fixed on the rack (1) at the left side of the dashboard positioning seat (6), be fixed with oil tank supporting seat (8) on left frame (1) of storage battery support second installation positioning seat (72), be fixed with first fixing base of back leaf spring (91) on frame (1) at storage battery support first installation positioning seat (71) and storage battery support second installation positioning seat (72) intermediate position rear, be fixed with wallboard rear portion location mount pad (10) on frame (1) at first fixing base of back leaf spring (91) rear, be fixed with back leaf spring second fixing base (92) on frame (1) at wallboard rear portion location mount pad (10) rear, be fixed with back tailboard mount pad (11) on frame (1) at back second fixing base (92) rear.
2. The avionics equipment manufacturing tool of claim 1, characterized by: first front plate spring positioning blocks (511) are fixed on the left side and the right side of the upper surface of the first front plate spring fixing seat (51), and first front plate spring positioning holes (512) are formed in the first front plate spring positioning blocks (511).
3. The avionics equipment manufacturing tool of claim 1, characterized by: a second front plate spring positioning block (521) is fixed to the upper end portion of the left side wall and the upper end portion of the right side wall of the front plate spring second fixing seat (52), and a second front plate spring positioning hole (522) is formed in the second front plate spring positioning block (521).
4. The avionics equipment manufacturing tool of claim 1, characterized by: a first battery support positioning block (711) is fixed on the upper surface of the first battery support mounting positioning seat (71), and a first battery support positioning hole (712) is formed in the first battery support positioning block (711).
5. The avionics equipment manufacturing tool of claim 1, characterized by: a second battery support positioning block (721) is fixed on the upper surface of the second mounting and positioning seat (72) of the battery support, and a second battery support positioning hole (722) is formed in the second battery support positioning block (721).
6. The avionics equipment manufacturing tool of claim 1, characterized by: a first rear plate spring positioning plate (911) is fixed to the upper end portion of the left side wall and the upper end portion of the right side wall of the rear plate spring first fixing seat (91), and a first rear plate spring positioning hole (912) is formed in the first rear plate spring positioning plate (911).
7. The avionics equipment manufacturing tool of claim 1, characterized by: and a second rear plate spring positioning plate (921) is fixed at the upper end part of the left side wall and the upper end part of the right side wall of the rear plate spring second fixing seat (92), and a second rear plate spring positioning hole (922) is formed in the second rear plate spring positioning plate (921).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921207692.1U CN210254885U (en) | 2019-07-29 | 2019-07-29 | Aviation service equipment manufacturing tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921207692.1U CN210254885U (en) | 2019-07-29 | 2019-07-29 | Aviation service equipment manufacturing tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210254885U true CN210254885U (en) | 2020-04-07 |
Family
ID=70015008
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921207692.1U Expired - Fee Related CN210254885U (en) | 2019-07-29 | 2019-07-29 | Aviation service equipment manufacturing tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210254885U (en) |
-
2019
- 2019-07-29 CN CN201921207692.1U patent/CN210254885U/en not_active Expired - Fee Related
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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: 20200407 |