CN209225423U - A kind of airplane parts fixture for processing - Google Patents
A kind of airplane parts fixture for processing Download PDFInfo
- Publication number
- CN209225423U CN209225423U CN201822160830.7U CN201822160830U CN209225423U CN 209225423 U CN209225423 U CN 209225423U CN 201822160830 U CN201822160830 U CN 201822160830U CN 209225423 U CN209225423 U CN 209225423U
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- tapped
- positioning
- centering
- locating piece
- sliding block
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- 241000883990 Flabellum Species 0.000 abstract description 7
- 206010044565 Tremor Diseases 0.000 abstract description 5
- 238000000034 method Methods 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005194 fractionation Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000008961 swelling Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 210000001550 testis Anatomy 0.000 description 1
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Abstract
A kind of airplane parts fixture for processing, is related to a kind of fixture.Two centering locating piece approach ends are formed respectively with round table-like plug, two centering locating pieces are respectively fixed with ring flange far from end, two ring flanges pass through more Screw arbor with nut at both-ends fastening positioning, annular slide track horizontal circle is outside underlying ring flange and the more connecting rods by being arranged radially are connected thereto fixation, annular slide track is angularly equipped with a plurality of arc groove, every arc groove sliding is provided with sliding block, each sliding block is equipped with tapped through hole and is equipped with vibration-resistant locating piece together, vibration-resistant locating piece includes C-shaped plate frame and two positioning bolts, two supporting plates of C-shaped plate frame are respectively equipped with tapped through hole two, two positioning bolts are spirally connected with two tapped through holes two respectively, underlying positioning bolt is spirally connected with the tapped through hole one of corresponding sliding block simultaneously.Effective position can be carried out to blade in airplane parts or flabellum shape part, additionally it is possible to it avoids trembling, strong applicability.
Description
Technical field
The utility model relates to a kind of fixture, especially a kind of airplane parts fixture for processing.
Background technique
Airplane parts generally require to carry out all multi-form processing, such as plating, spray before being fabricated to fabricated part
The programs such as painting, antirust, reinforcing need effectively to be clamped using fixture at this time.
There are many blades or the part of flabellum shape in airplane parts, this kind of part lacks dedicated fixture at present, and general
Clamping position is carried out to its blade edge all over using conventional universal fixturing, is not only easy to lead to disadvantageous deformation because of the center of gravity swelling and hanging down of either of the testes, and
And it is difficult to control trembling of generating in process of part, it is unfavorable for effective progress of processing.
Therefore, a kind of special fixture for blade in airplane parts or flabellum shape part is very necessary.
Summary of the invention
The purpose of this utility model is to provide a kind of airplane parts fixture for processing, it can be to blade in airplane parts
Or flabellum shape part carries out effective position, additionally it is possible to it avoids trembling, strong applicability.
Realize above-mentioned purpose, the utility model takes following technical proposals: a kind of airplane parts fixture for processing, including ring
Shape slideway, two centering locating pieces, more Screw arbor with nut at both-ends, multiple sliding blocks and multiple vibration-resistant locating pieces, described two centerings
Locating piece is cylindrical component and is vertically coaxially disposed, and two centering locating piece approach ends are formed respectively with round table-like plug, and two
Centering locating piece is coaxially fixed with ring flange far from end respectively, and two ring flanges are fastened by the more Screw arbor with nut at both-ends
Position, the annular slide track horizontal circle is outside underlying ring flange and the more connecting rods by being arranged radially connect with it
Fixation is connect, annular slide track is angularly equipped with a plurality of arc groove, and every arc groove sliding is provided with sliding block, each sliding block
It is vertically equipped with tapped through hole and vibration-resistant locating piece is installed together, each vibration-resistant locating piece includes C-shaped plate frame and two
Positioning bolt, two supporting plates of the C-shaped plate frame are vertically equipped with tapped through hole two respectively, two positioning bolts respectively with two
The tapped through hole two is spirally connected, and underlying positioning bolt is spirally connected with the tapped through hole one of corresponding sliding block simultaneously.
Compared with prior art, the utility model has the beneficial effects that the utility model can be to blade in airplane parts
Or the processing of flabellum shape part carries out effective position, it, can be to blade or flabellum by the solid to tensing of two centering locating pieces
The center mounting hole of shape part is clamped, simple and convenient, when as needed to avoid trembling in process, can also pass through vibration-resistant
Locating piece is clamped, strong applicability.
Detailed description of the invention
Fig. 1 is the overall structure axonometric drawing of the airplane parts fixture for processing of the utility model；
Fig. 2 is the fractionation structure axonometric drawing of two centering locating pieces of the utility model；
Fig. 3 is the vibration-resistant locating piece of the utility model and the assembling structure axonometric drawing of annular slide track.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, to the technical solution in the utility model carry out it is clear,
It being fully described by, it is clear that described embodiment is only a part of the embodiment of utility model, instead of all the embodiments,
Based on the embodiments of the present invention, obtained by those of ordinary skill in the art without making creative efforts
Every other embodiment, fall within the protection scope of the utility model.
Specific embodiment 1: as shown in Fig. 1 ~ Fig. 3, the utility model discloses a kind of airplane parts fixture for processing,
Including 3, two centering locating pieces 1 of annular slide track, more Screw arbor with nut at both-ends 2, multiple sliding blocks 5 and multiple vibration-resistant locating pieces, institute
It states two centering locating pieces 1 to be cylindrical component and be vertically coaxially disposed, two 1 approach ends of centering locating piece are formed respectively with rotary table
Shape plug 1-1, two centering locating pieces 1 are coaxially fixed with ring flange 1-2 far from end respectively, and two ring flange 1-2 pass through
The more Screw arbor with nut at both-ends 2 fastening positioning, every 2 both ends of Screw arbor with nut at both-ends are screwed with nut and fasten to two ring flange 1-2 opposite directions,
3 horizontal circle of annular slide track is outside underlying ring flange 1-2 and passes through more connecting rods 4 being arranged radially and its
It is connected and fixed, annular slide track 3 is angularly equipped with a plurality of arc groove 3-1, and every arc groove 3-1 sliding is provided with sliding block 5, often
A sliding block 5 is vertically equipped with tapped through hole and is equipped with vibration-resistant locating piece together, and each vibration-resistant locating piece includes C-shaped
Grillage 7 and two positioning bolts 6, two supporting plates of the C-shaped plate frame 7 are vertically equipped with tapped through hole two, two positioning respectively
Bolt 6 is spirally connected with two tapped through holes two respectively, and underlying positioning bolt 6 is simultaneously and described in corresponding sliding block 5
Tapped through hole one is spirally connected.
Specific embodiment 2: as shown in Fig. 2, present embodiment is made furtherly to specific embodiment one
Bright, the end face round table-like plug 1-1 of one of them centering locating piece 1 is coaxially fixed with round inserted link 1-3, another centering is fixed
The end face round table-like plug 1-1 of position part 1 is coaxially recessed with round slot 1-4, the round inserted link 1-3 and the round slot 1-4 and inserts
It is equipped with.
Specific embodiment 3: as shown in figure 3, present embodiment is to specific embodiment one or specific embodiment two
The further explanation made, one end that the every positioning bolt 6 is located at 7 inside of C-shaped plate frame are formed with hemispherical contact 6-1.
Specific embodiment 4: as shown in Figure 1, 2, present embodiment is made furtherly to specific embodiment three
Bright, the underlying ring flange 1-2 is fixedly connected with branch cantilever crane 8.
The processing of the utility model blade or flabellum shape part suitable for airplane parts positions, and method used below is passed the imperial examinations at the provincial level
Example be blade 9, when in use by the center mounting hole of blade 9 be inserted into two centering locating pieces 1 round table-like plug 1-1 it
Between, two of them round table-like plug 1-1 is not contacted between end face, and circle inserted link 1-3 and circle slot 1-4 cooperation guarantee that two centerings are fixed
The coaxial relation of position part 1, the Screw arbor with nut at both-ends 2 for reusing suitable number fasten two two ring flange 1-2 opposite directions, and then to paddle
Leaf 9 is clamped, when needing that blade 9 is avoided to tremble in process, by sliding block 5 along annular slide track 3 arc groove 3-1 into
Row sliding, is clamped, positioning bolt 6 is formed with hemispherical contact 6-1, passes through using blade of the vibration-resistant locating piece to blade 9
The form of point contact carries out clamping control contact area, and for branch cantilever crane 8 for being installed with lathe, overall structure is simple and effective,
Strong applicability.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in the form of others dress body
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing the condition of equivalent for falling in claim
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (4)
1. a kind of airplane parts fixture for processing, it is characterised in that: including annular slide track (3), two centering locating pieces (1), more
Root Screw arbor with nut at both-ends (2), multiple sliding blocks (5) and multiple vibration-resistant locating pieces, described two centering locating pieces (1) are column structure
Part is simultaneously vertically coaxially disposed, and two centering locating piece (1) approach ends are formed respectively with round table-like plug (1-1), two centering positioning
Part (1) is coaxially fixed with ring flange (1-2) respectively far from end, and two ring flanges (1-2) pass through the more Screw arbor with nut at both-ends
(2) fastening positioning, annular slide track (3) horizontal circle are external in underlying ring flange (1-2) and by being arranged radially
More connecting rods (4) be connected thereto fixation, annular slide track (3) is angularly equipped with a plurality of arc groove (3-1), every arc
Slot (3-1) sliding is provided with sliding block (5), and each sliding block (5) is vertically equipped with tapped through hole and is equipped with vibration-resistant positioning together
Part, each vibration-resistant locating piece include C-shaped plate frame (7) Ji Lianggen positioning bolt (6), two supporting plates of the C-shaped plate frame (7)
It is vertically equipped with tapped through hole two respectively, two positioning bolts (6) are spirally connected with two tapped through holes two respectively, under being located at
The positioning bolt (6) of side is spirally connected with the tapped through hole one of corresponding sliding block (5) simultaneously.
2. a kind of airplane parts fixture for processing according to claim 1, it is characterised in that: one of them described centering is fixed
Position part (1) the end face round table-like plug (1-1) be coaxially fixed with round inserted link (1-3), another centering locating piece (1) it is round table-like
The end face plug (1-1) is coaxially recessed with round slot (1-4), and the round inserted link (1-3) sets with round slot (1-4) the inserting cooperation
It sets.
3. a kind of airplane parts fixture for processing according to claim 1 or 2, it is characterised in that: the every positioning spiral shell
One end that bolt (6) is located on the inside of C-shaped plate frame (7) is formed with hemispherical contact (6-1).
4. a kind of airplane parts fixture for processing according to claim 3, it is characterised in that: the underlying flange
Disk (1-2) is fixedly connected with branch cantilever crane (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822160830.7U CN209225423U (en) | 2018-12-22 | 2018-12-22 | A kind of airplane parts fixture for processing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822160830.7U CN209225423U (en) | 2018-12-22 | 2018-12-22 | A kind of airplane parts fixture for processing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209225423U true CN209225423U (en) | 2019-08-09 |
Family
ID=67508848
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822160830.7U Active CN209225423U (en) | 2018-12-22 | 2018-12-22 | A kind of airplane parts fixture for processing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209225423U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111571197A (en) * | 2020-05-09 | 2020-08-25 | 南京玛格耐特智能科技有限公司 | Fan production tool |
| CN114083468A (en) * | 2021-12-24 | 2022-02-25 | 江西省信航航空科技有限公司 | Rotor wing center piece frock clamp |
-
2018
- 2018-12-22 CN CN201822160830.7U patent/CN209225423U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111571197A (en) * | 2020-05-09 | 2020-08-25 | 南京玛格耐特智能科技有限公司 | Fan production tool |
| CN114083468A (en) * | 2021-12-24 | 2022-02-25 | 江西省信航航空科技有限公司 | Rotor wing center piece frock clamp |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240125 Address after: No.3, Hanan Third Road, core area of Hanan industrial new town, Pingfang District, Harbin City, Heilongjiang Province Patentee after: GUANGLIAN AVIATION INDUSTRY Co.,Ltd. Country or region after: China Address before: 311, Chuangye building, No.18, Gaoxin 2nd Road, Nanchang hi tech Industrial Development Zone, Jiangxi 330000 Patentee before: Guanglian Airlines (Nanchang) Co.,Ltd. Country or region before: China |
|
| TR01 | Transfer of patent right |