CN208811153U - A kind of airplane parts drill jig - Google Patents
A kind of airplane parts drill jig Download PDFInfo
- Publication number
- CN208811153U CN208811153U CN201820928900.6U CN201820928900U CN208811153U CN 208811153 U CN208811153 U CN 208811153U CN 201820928900 U CN201820928900 U CN 201820928900U CN 208811153 U CN208811153 U CN 208811153U
- Authority
- CN
- China
- Prior art keywords
- fixedly installed
- retaining ring
- pedestal
- plate
- drill jig
- 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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Abstract
The utility model relates to drill jig technical fields, and disclose a kind of airplane parts drill jig, including pedestal, bore channel is offered at the top of the pedestal, the top of the pedestal and be located at bore channel two sides be fixedly installed with compression spring, top plate is fixedly installed at the top of the compression spring, the top of the pedestal and the outside for being located at compression spring are fixedly installed with interior retaining ring, and the bottom of the top plate and the outside for being located at compression spring are fixedly installed with the outer retaining ring with the clamping of interior retaining ring.The airplane parts drill jig, by having reset spring in setting position-limited box, it can be by making clip-connecting rod achieve the effect that reset, there is limited block by being arranged on outer retaining ring and interior retaining ring, outer retaining ring and interior retaining ring can be made to carry out clamping by limited block to avoid falling off, to effective solution, some drill jigs are not adjustable the problem of causing mold fixed unstable, will lead to burn failure when drill jig when fixing mould.
Description
Technical field
The utility model relates to drill jig technical field, specially a kind of airplane parts drill jig.
Background technique
It is used to determine position of the workpiece relative to cutter (drill bit, reamer and reamer etc.) on drilling machine, and tight by toast
Equal measures, the device processing such as bored, expanded, cut with scissors in the case where remaining unchanged its relative position is referred to as drill jig, simple
Claim drill jig, drill jig generally all have guide and determine tool position various drill bushings, drill jig type is more, be often divided into it is fixed,
The main Types such as movable type, cover-plate type, rotary, convertible and slide column type, when design should according to the shape of workpiece, size plus
Work requires and type, the specification of production batch and used lathe, reasonably selects corresponding structure type, the structure of drill jig
Feature is the position distribution in also with good grounds processed hole and the drill bushing and drill jig that are arranged except the positioning for having workpiece, in addition to clamping device
Plate to determine the position of cutter, and prevents cutter from tilting in process, to guarantee the position precision for being processed hole.
When designing drill jig, it is necessary first to according to the shape of workpiece, size, weight and processing request, and consider production batch
It measures with actual conditions such as the technology status of factory technics equipment and selects the structure type of fixture, but some drill jigs are in stent
Not being adjustable when tool causes mold fixed unstable, will lead to burn failure when drill jig, so propose a kind of aircraft
Part drill jig come solve the problems, such as it is above-mentioned proposed in.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of airplane parts drill jig, has the advantages of adjusting, solution
Some drill jigs of having determined are not adjustable when fixing mould and cause mold fixed unstable, will lead to mold damage when drill jig
Bad problem.
(2) technical solution
For the purpose for realizing above-mentioned adjusting, the utility model is provided the following technical solutions: a kind of airplane parts drill jig, including
Pedestal, offers bore channel at the top of the pedestal, the top of the pedestal and two sides for being located at bore channel are fixedly installed with
Compression spring is fixedly installed with top plate, the top of the pedestal and the outside for being located at compression spring at the top of the compression spring
It is fixedly installed with interior retaining ring, the bottom of the top plate and the outside for being located at compression spring are fixedly installed with outer with the clamping of interior retaining ring
Retaining ring, the bottom of the top plate are fixedly installed with the electric drill base at the top of bore channel, and the bottom of the electric drill base is fixedly mounted
There is an electric drill head extended to inside bore channel, the top of the pedestal and left and right side for being located at bore channel is fixedly installed with
Outer card plate, the internal activity of the outer card plate are equipped with interior snap-gauge, and the top and bottom of the outer card plate are fixedly mounted limited
Position box, the external activity of the position-limited box are equipped with the clip-connecting rod through outer card plate and interior snap-gauge, on the clip-connecting rod and are located at
The outside of position-limited box is fixedly installed with pulling plate, on the clip-connecting rod and is located at the internal activity of position-limited box and is equipped with reset spring,
On the clip-connecting rod and be located at the inside of position-limited box and be fixedly installed with limit plate close to one end of outer card plate, the interior snap-gauge it is outer
Portion is fixedly installed with nut, and the nut is connected with the threaded post through interior snap-gauge, the spiral shell far from the threaded one end of interior snap-gauge
Line column is fixedly installed with the push plate inside card adapter plate far from one end of nut.
Preferably, blocked hole corresponding with clip-connecting rod is offered on the interior snap-gauge and outer card plate.
Preferably, movable span corresponding with threaded post is offered on the interior snap-gauge, and is fixedly installed in movable span resistance to
Grinding.
Preferably, the bottom of the pedestal is fixedly installed with non-slip mat, and the material of non-slip mat can be nitrile rubber.
Preferably, the limited block being mutually clamped is fixedly installed on the outer retaining ring and interior retaining ring.
Preferably, the top plate is flexibly connected by compression spring and bottom plate.
(3) beneficial effect
Compared with prior art, the utility model provides a kind of airplane parts drill jig, have it is following the utility model has the advantages that
1, there are non-slip mat in the airplane parts drill jig, the bottom by the way that pedestal is arranged, pedestal can be made to keep away when placing
Exempt to slide error when leading to drill jig, by having push plate in setting threaded post, the mold of drill jig can will be needed by push plate
It is fixed, has position-limited box by being arranged on outer card plate, clip-connecting rod can be made to fix outer card plate and interior snap-gauge by position-limited box,
Achieve the effect that adjust.
2, the airplane parts drill jig can be by making clip-connecting rod reach reset by having reset spring in setting position-limited box
Effect, have limited block by being arranged on outer retaining ring and interior retaining ring, outer retaining ring and the progress of interior retaining ring can be made by limited block
Clamping avoids falling off, and causes mold fixed not so that some drill jigs of effective solution are not adjustable when fixing mould
Surely, the problem of will lead to burn failure when drill jig.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the structural schematic diagram of the utility model outer card plate；
Fig. 3 is the structure enlargement diagram of A in the utility model Fig. 2.
In figure: 1 pedestal, 2 top plates, 3 electric drill bases, 4 electric drill heads, 5 compression springs, 6 outer retaining rings, retaining ring, 8 bore channels, 9 in 7
Outer card plate, snap-gauge in 10,11 clip-connecting rods, 12 limit plates, 13 position-limited box, 14 pulling plates, 15 reset springs, 16 push plates, 17 threaded posts,
18 nuts.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
It please refers to Fig. 1-3, a kind of airplane parts drill jig, including pedestal 1, the bottom of pedestal 1 and is fixedly installed with non-slip mat, and
The material of non-slip mat can be nitrile rubber, and the top of pedestal 1 offers bore channel 8, the top of pedestal 1 and be located at bore channel 8
Two sides are fixedly installed with compression spring 5, and the top of compression spring 5 is fixedly installed with top plate 2, and top plate 2 passes through 5 He of compression spring
Bottom plate 1 is flexibly connected, the top of the pedestal 1 and outside for being located at compression spring 5 is fixedly installed with interior retaining ring 7, the bottom of top plate 2 and
It is fixedly installed with the outer retaining ring 6 with the clamping of interior retaining ring 7 positioned at the outside of compression spring 5, is fixed on outer retaining ring 6 and interior retaining ring 7
The limited block being mutually clamped is installed, the bottom of top plate 2 is fixedly installed with the electric drill base 3 positioned at 8 top of bore channel, electric drill base 3
Bottom be fixedly installed with the electric drill head 4 extended to inside bore channel 8, the top of pedestal 1 and the left side and the right side for being located at bore channel 8
Side is fixedly installed with outer card plate 9, and the internal activity of outer card plate 9 is equipped with interior snap-gauge 10, and the top and bottom of outer card plate 9 are solid
Dingan County is equipped with position-limited box 13, and the external activity of position-limited box 13 is equipped with the clip-connecting rod 11 through outer card plate 9 and interior snap-gauge 10, interior card
It offers blocked hole corresponding with clip-connecting rod 11 on plate 10 and outer card plate 9, on clip-connecting rod 11 and is located at the outside of position-limited box 13
It is fixedly installed with pulling plate 14, on clip-connecting rod 11 and is located at the internal activity of position-limited box 13 reset spring 15, clip-connecting rod 11 are installed
Inside that is upper and being located at position-limited box 13 is fixedly installed with limit plate 12 close to one end of outer card plate 9, and the external of interior snap-gauge 10 is fixed
Nut 18 is installed, nut 18 is connected with the threaded post 17 through interior snap-gauge 10, interior snap-gauge far from the threaded one end of interior snap-gauge 10
Movable span corresponding with threaded post 17 is offered on 10, and is fixedly installed with wear plate in movable span, and threaded post 17 is far from nut
18 one end is fixedly installed with the push plate 16 inside card adapter plate 10, the airplane parts drill jig, by the bottom that pedestal 1 is arranged
There is non-slip mat, error when can making pedestal 1 that sliding be avoided to lead to drill jig when placing, by setting threaded post 17
There is push plate 16, the mold of drill jig can will be needed to be fixed by push plate 16, by having position-limited box 13 on setting outer card plate 9,
Clip-connecting rod 11 can be made by position-limited box 13 that outer card plate 9 and interior snap-gauge 10 is fixed, achieved the effect that adjust, and the aircraft zero
Part drill jig can be by making clip-connecting rod 11 achieve the effect that reset, by setting by having reset spring 15 in setting position-limited box 13
Setting on outer retaining ring 6 and interior retaining ring 7 has limited block, and outer retaining ring 6 and interior retaining ring 7 can be made to carry out clamping by limited block and avoid taking off
It falls, causes mold fixed unstable so that some drill jigs of effective solution are not adjustable when fixing mould, in drill jig
When the problem of will lead to burn failure.
In conclusion the airplane parts drill jig, non-slip mat is arranged at the bottom by the way that pedestal 1 is arranged, and pedestal 1 can be made to place
When error when avoid sliding from leading to drill jig, by having push plate 16 in setting threaded post 17, can pass through push plate 16 will
It needs the mold of drill jig to be fixed, by having position-limited box 13 on setting outer card plate 9, clip-connecting rod 11 can be made to pass through position-limited box 13
Outer card plate 9 and interior snap-gauge 10 is fixed, achieve the effect that adjust.
Also, the airplane parts drill jig can be by making clip-connecting rod 11 by having reset spring 15 in setting position-limited box 13
Achieve the effect that reset, has limited block by being arranged on outer retaining ring 6 and interior retaining ring 7, outer 6 He of retaining ring can be made by limited block
Interior retaining ring 7 carries out clamping and avoids falling off, so that some drill jigs of effective solution are not adjustable when fixing mould to be caused
The problem of mold is fixed unstable, will lead to burn failure when drill jig.
It should be noted that the terms "include", "comprise" or its any other variant are intended to the packet of nonexcludability
Contain, so that the process, method, article or equipment for including a series of elements not only includes those elements, but also including
Other elements that are not explicitly listed, or further include for elements inherent to such a process, method, article, or device.
In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that including the element
Process, method, article or equipment in there is also other identical elements.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of airplane parts drill jig, including pedestal (1), it is characterised in that: offer bore channel at the top of the pedestal (1)
(8), the top of the pedestal (1) and be located at bore channel (8) two sides be fixedly installed with compression spring (5), the pressure bullet
It is fixedly installed at the top of spring (5) top plate (2), the top of the pedestal (1) and the external fixed installation for being located at compression spring (5)
Have interior retaining ring (7), the bottom of the top plate (2) and be located at compression spring (5) outside be fixedly installed with and interior retaining ring (7) be clamped
Outer retaining ring (6), the bottom of the top plate (2) is fixedly installed with the electric drill base (3) at the top of bore channel (8), the electric drill
The bottom of seat (3), which is fixedly installed with, extends to the internal electric drill head (4) of bore channel (8), and the top of the pedestal (1) and being located at is bored
The left and right side of hole slot (8) is fixedly installed with outer card plate (9), and the internal activity of the outer card plate (9) is equipped with interior snap-gauge
(10), the top and bottom of the outer card plate (9) are fixedly installed with position-limited box (13), the external activity of the position-limited box (13)
Clip-connecting rod (11) through outer card plate (9) and interior snap-gauge (10) is installed, on the clip-connecting rod (11) and positioned at position-limited box (13)
Outside be fixedly installed with pulling plate (14), on the clip-connecting rod (11) and be located at position-limited box (13) internal activity reset is installed
Spring (15) on the clip-connecting rod (11) and is located at the inside of position-limited box (13) and is fixedly installed with close to one end of outer card plate (9)
The outside of limit plate (12), the interior snap-gauge (10) is fixedly installed with nut (18), and the nut (18) is far from interior snap-gauge (10)
Threaded one end be connected with the threaded post (17) through interior snap-gauge (10), the one end of the threaded post (17) far from nut (18) is solid
Dingan County, which is equipped with, is located at interior snap-gauge (10) internal push plate (16).
2. a kind of airplane parts drill jig according to claim 1, it is characterised in that: the interior snap-gauge (10) and outer card plate
(9) blocked hole corresponding with clip-connecting rod (11) is offered on.
3. a kind of airplane parts drill jig according to claim 1, it is characterised in that: offered on the interior snap-gauge (10) with
The corresponding movable span of threaded post (17), and wear plate is fixedly installed in movable span.
4. a kind of airplane parts drill jig according to claim 1, it is characterised in that: the fixed peace in the bottom of the pedestal (1)
Material equipped with non-slip mat, and non-slip mat can be nitrile rubber.
5. a kind of airplane parts drill jig according to claim 1, it is characterised in that: the outer retaining ring (6) and interior retaining ring (7)
On be fixedly installed with the limited block being mutually clamped.
6. a kind of airplane parts drill jig according to claim 1, it is characterised in that: the top plate (2) passes through compression spring
(5) it is flexibly connected with pedestal (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820928900.6U CN208811153U (en) | 2018-06-15 | 2018-06-15 | A kind of airplane parts drill jig |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820928900.6U CN208811153U (en) | 2018-06-15 | 2018-06-15 | A kind of airplane parts drill jig |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208811153U true CN208811153U (en) | 2019-05-03 |
Family
ID=66269760
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820928900.6U Expired - Fee Related CN208811153U (en) | 2018-06-15 | 2018-06-15 | A kind of airplane parts drill jig |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208811153U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116900366A (en) * | 2023-09-13 | 2023-10-20 | 辽宁华天航空科技股份有限公司 | Self-positioning, fixing and clamping anti-damage drill jig for aircraft assembly and use method thereof |
-
2018
- 2018-06-15 CN CN201820928900.6U patent/CN208811153U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116900366A (en) * | 2023-09-13 | 2023-10-20 | 辽宁华天航空科技股份有限公司 | Self-positioning, fixing and clamping anti-damage drill jig for aircraft assembly and use method thereof |
| CN116900366B (en) * | 2023-09-13 | 2023-12-12 | 辽宁华天航空科技股份有限公司 | Self-positioning, fixing and clamping anti-damage drill jig for aircraft assembly and use method thereof |
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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 |
Granted publication date: 20190503 Termination date: 20210615 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |