CN109676171A - Inner hole machinery tensioning device - Google Patents
Inner hole machinery tensioning device Download PDFInfo
- Publication number
- CN109676171A CN109676171A CN201910039352.0A CN201910039352A CN109676171A CN 109676171 A CN109676171 A CN 109676171A CN 201910039352 A CN201910039352 A CN 201910039352A CN 109676171 A CN109676171 A CN 109676171A
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- China
- Prior art keywords
- tensioner
- tension mandrel
- guiding
- product
- inner hole
- 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.)
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- 125000006850 spacer group Chemical group 0.000 claims abstract description 16
- 230000006835 compression Effects 0.000 claims abstract description 5
- 238000007906 compression Methods 0.000 claims abstract description 5
- 239000000203 mixture Substances 0.000 claims abstract description 4
- 239000000463 material Substances 0.000 claims description 9
- 238000003825 pressing Methods 0.000 claims description 4
- 229910000639 Spring steel Inorganic materials 0.000 claims description 3
- 238000012545 processing Methods 0.000 abstract description 7
- 238000005516 engineering process Methods 0.000 abstract description 3
- 239000000047 product Substances 0.000 description 20
- 238000000034 method Methods 0.000 description 7
- 238000003754 machining Methods 0.000 description 6
- 238000013461 design Methods 0.000 description 4
- 235000012745 brilliant blue FCF Nutrition 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000006227 byproduct Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B31/00—Chucks; Expansion mandrels; Adaptations thereof for remote control
- B23B31/40—Expansion mandrels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Gripping On Spindles (AREA)
Abstract
The invention belongs to aviation machine processing technology equipment fields, are related to a kind of inner hole machinery tensioning device.The device includes spindle flange, tension mandrel, end face positioning sleeve, tensioner, guiding tensioner, spacer, gasket and locking nut.Spindle flange one end is positioned at machine tool chief axis inner hole, and the other end is connect with tension mandrel;End face positioning sleeve covers on tension mandrel, and the end face for product positions;Tensioner, spacer, guiding tensioner, gasket and locking nut are sequentially sleeved on tension mandrel;Tensioner and guiding tensioner are thin-walled groove structure, generate expanding force to product by micro-deformation;Spacer excircle dimension is less than product hole size;Gasket is for being isolated guiding tensioner and locking nut, in order to avoid damage guiding tensioner;Locking nut is threadedly coupled with tension mandrel, and composition screw thread pair provides pressure.The present invention realizes the positioning and compression of the special-shaped product with hole characteristic, and machined surface is completely open, improves a sequence working modulus.
Description
Technical field
The invention belongs to aviation machine processing technology equipment fields, are related to a kind of inner hole machinery tensioning device.
Background technique
Either military aircraft or civil aircraft, all presence largely have hole characteristic in aviation machine manufacture field
Special-shaped part.Such External Shape is all more complicated, and the craftsmanship of processing is bad, it is difficult to ensure that final size requires, closes
Lattice rate is relatively low.But the design basis and machining benchmark of most such products are all Kong Yuansu, while with various multiplexing energy numbers
It controls combined machine to widely apply, to we provide a new solution routes.
The conventional clamp majority of conventional machine tool adapted originally is a set of fixture of a procedure, therefore the positioning and compression provided
Position it is more, as long as positioning with compress element be non-processing surface.But it is more to complete the processing of product needs
Procedure is completed, and the positioning datum of every procedure and machining benchmark are difficult unification, cause the Datum transfer larger;It is more
Process processing needs multiple sets of fixtures just to assist producing, cause in this way it is too long when beam worker keep efficiency relatively low, multiple sets of fixtures
Also relatively high economy is bad for cost.
With the development of numerically-controlled machine tool, various multi-function peripheral beds are widely applied.As turnning and milling combined numerically controlled machine is exactly
One is typical.This kind of lathe usually can a sequence complete 70%-100% processing;And it is overlapped design basis with machining benchmark, it mentions
High machining accuracy.But with the application of all kinds of advanced lathes, conventional fixture cannot be exactly matched.It to be processed in a sequence
More features, it is desirable to which the surface of processed product will begin completely, not allow to arrange pressing plate, this would have to fixed with inner hole
Position simultaneously clamps on.
Summary of the invention
In view of the problems of the existing technology, the present invention proposes a kind of inner hole machinery tensioning device, and spindle flange is according to machine
The connecting interface design of bed main shaft;By the special-shaped product clamping with hole characteristic on the tight device of inner hole mechanical expanding, locking nut
On mandrel;Nut lock clamp force, which is transmitted to tensioner, makes tensioner compressive deformation to radial tensioner;Tensioner inner hole and outer circle
Precision is had, thus by product orientation tensioner on device.
The technical solution of the present invention is as follows:
A kind of inner hole machinery tensioning device, including spindle flange 1, tension mandrel 2, end face positioning sleeve 3, tensioner 4, guiding
Tensioner 5, spacer 6, gasket 7, locking nut 8, interior six point cylindrical head bolt a9, interior six point cylindrical head bolt b10 and interior hexagonal
Cylinder head bolt c11;
The tension mandrel 2 is Pyatyi multi-diameter shaft, and second level ladder shaft diameter is maximum, and level V ladder shaft diameter is minimum,
First order multi-diameter shaft external cylindrical surface and shaft shoulder end face and spindle flange 1 cooperate, and pass through interior six point cylindrical head bolt b10 and method of principal axis
Blue 1 one end connection;1 other end of spindle flange is positioned at machine tool chief axis inner hole, is connected by interior six point cylindrical head bolt a9 and lathe
It connects;3 sets of end face positioning sleeve on the third level multi-diameter shaft of tension mandrel 2, lower end surface by interior six point cylindrical head bolt c11 with rise
The shaft shoulder connection of tight mandrel 2, end face of the upper surface for product 12 position;
The tensioner 4, spacer 6, guiding tensioner 5, gasket 7 and locking nut 8 are sequentially sleeved in the 5th of tension mandrel 5
On grade multi-diameter shaft;Tensioner 4 with guiding 5 material of tensioner it is identical, be spring steel material, be in thin-walled groove structure, inner hole with
Tension mandrel 2 cooperates, and middle part outside diameter Φ D2 is depending on the hole size of different product 12, in the case where applying pressure
Expanding force is generated to product 12 by micro-deformation;It is Φ D2 size that the guiding tensioner 5, which has an end face outside diameter, is played
Guiding role;6 inner hole of spacer and tension mandrel 2 cooperate, and excircle dimension is less than 12 hole size of product, and spacer 6 is for adapting to not
Length with product 12 changes;Gasket 7 is for being isolated guiding tensioner 5 and locking nut 8, in order to avoid damage guiding tensioner 5;Lock
Tight nut 8 is threadedly coupled with tension mandrel 2, and composition screw thread pair provides pressure, realizes the compression and positioning of product 12.
The end face positioning sleeve 3 is different according to the material of product to be processed, selects different material and heat treatment mode.
Beneficial effects of the present invention:
It is that positioning clamps element with hole characteristic, positions and compress while realizing the special-shaped product with hole characteristic, essence
It determines position, reliable clamping, and machined surface is completely open, greatly improves a sequence working modulus;Avoid the base of multistage manufacturing processes
Quasi- conversion, realizes being overlapped for design basis and machining benchmark, improves machining accuracy.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of inner hole machinery tensioning device;
Fig. 2 is the side view of inner hole machinery tensioning device;
Fig. 3 (a) is the schematic diagram for being oriented to tensioner;
Fig. 3 (b) is the cross-sectional view for being oriented to tensioner;
In figure: 1 spindle flange;2 tension mandrels;3 end face positioning sleeves;4 tensioners;5 guiding tensioners;6 spacers;7 gaskets;
8 locking nuts;Six point cylindrical head bolt a in 9;Six point cylindrical head bolt b in 10;Six point cylindrical head bolt c in 11;12 products.
Specific embodiment
Below in conjunction with attached drawing and technical solution, specific embodiments of the present invention are further illustrated.
As illustrated in fig. 1 and 2, a kind of inner hole machinery tensioning device, including spindle flange 1, tension mandrel 2, end face positioning sleeve
3, tensioner 4, guiding tensioner 5, spacer 6, gasket 7, locking nut 8, interior six point cylindrical head bolt a9, interior hexagonal cylindrical head spiral shell
Bolt b10 and interior six point cylindrical head bolt c11;
The tension mandrel 2 is Pyatyi multi-diameter shaft, and second level ladder shaft diameter is maximum, and level V ladder shaft diameter is minimum,
First order multi-diameter shaft external cylindrical surface and shaft shoulder end face and spindle flange 1 cooperate, and pass through interior six point cylindrical head bolt b10 and method of principal axis
Blue 1 one end connection;1 other end of spindle flange is positioned at machine tool chief axis inner hole, is connected by interior six point cylindrical head bolt a9 and lathe
It connects;3 sets of end face positioning sleeve on the third level multi-diameter shaft of tension mandrel 2, lower end surface by interior six point cylindrical head bolt c11 with rise
The shaft shoulder connection of tight mandrel 2, end face of the upper surface for product 12 position;
The tensioner 4, spacer 6, guiding tensioner 5, gasket 7 and locking nut 8 are sequentially sleeved in the 5th of tension mandrel 5
On grade multi-diameter shaft;Tensioner 4 and guiding tensioner 5 are a kind of spring steel material, are in thin-walled groove structure, inner hole and tensioner core
Axis 2 cooperates, and middle part outside diameter Φ D2 is depending on the hole size of different product 12, in the case where applying pressure by micro-
Quantitative change shape generates expanding force to product 12;It is Φ D2 size that the guiding tensioner 5, which has an end face outside diameter, plays guiding and makees
With;6 inner hole of spacer and tension mandrel 2 cooperate, and excircle dimension is less than 12 hole size of product, and spacer 6 is for adapting to different product
12 length variation;Gasket 7 is for being isolated guiding tensioner 5 and locking nut 8, in order to avoid damage guiding tensioner 5;Locking nut
8 are threadedly coupled with tension mandrel 2, and composition screw thread pair provides pressure, realize the compression and positioning of product 12.
The end face positioning sleeve 3 is different according to the material of product to be processed, selects different material and heat treatment mode.
In addition to the implementation, the present invention can also have other embodiments.It is all to use equivalent substitution or equivalent transformation shape
At technical solution, fall within the scope of protection required by the present invention.
Claims (1)
1. a kind of inner hole machinery tensioning device, which is characterized in that the inner hole machinery tensioning device include spindle flange (1),
Tension mandrel (2), end face positioning sleeve (3), tensioner (4), guiding tensioner (5), spacer (6), gasket (7), locking nut
(8), interior six point cylindrical head bolt a (9), interior six point cylindrical head bolt b (10) and interior six point cylindrical head bolt c (11);
The tension mandrel (2) is Pyatyi multi-diameter shaft, and second level ladder shaft diameter is maximum, and level V ladder shaft diameter is minimum, the
Step axis external cylindrical surface and shaft shoulder end face and spindle flange (1) cooperate, and pass through interior six point cylindrical head bolt b (10) and main shaft
The connection of flange (1) one end;Spindle flange (1) other end is positioned at machine tool chief axis inner hole, passes through interior six point cylindrical head bolt a (9)
It is connect with lathe;End face positioning sleeve (3) covers on the third level multi-diameter shaft of tension mandrel (2), and lower end surface passes through interior hexagonal cylindrical
Hook bolt c (11) is connect with the shaft shoulder of tension mandrel (2), and end face of the upper surface for product (12) positions;
The tensioner (4), spacer (6), guiding tensioner (5), gasket (7) and locking nut (8) are sequentially sleeved in tension mandrel
(2) on level V multi-diameter shaft;Tensioner (4) is identical with guiding tensioner (5) material, is spring steel material, is in thin-walled ring
Slot structure, inner hole and tension mandrel (2) cooperate, middle part outside diameter Φ D2 depending on the hole size of different product (12),
Expanding force is generated to product (12) by micro-deformation in the case where applying pressure;The guiding tensioner (5) has an end face
Outside diameter is Φ D2 size, plays guiding role;Spacer (6) inner hole and tension mandrel (2) cooperate, and excircle dimension is less than product
(12) hole size, spacer (6) are used to adapt to the length variation of different product (12);Gasket (7) is for being isolated guiding tensioner
(5) and locking nut (8), in order to avoid damage guiding tensioner (5);Locking nut (8) is threadedly coupled with tension mandrel (2), composition
Screw thread pair provides pressure, realizes the compression and positioning of product (12).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910039352.0A CN109676171B (en) | 2019-01-16 | 2019-01-16 | Inner hole mechanical tensioning device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910039352.0A CN109676171B (en) | 2019-01-16 | 2019-01-16 | Inner hole mechanical tensioning device |
Publications (2)
Publication Number | Publication Date |
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CN109676171A true CN109676171A (en) | 2019-04-26 |
CN109676171B CN109676171B (en) | 2024-01-23 |
Family
ID=66193168
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201910039352.0A Active CN109676171B (en) | 2019-01-16 | 2019-01-16 | Inner hole mechanical tensioning device |
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CN (1) | CN109676171B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111168441A (en) * | 2020-03-16 | 2020-05-19 | 沈阳飞机工业(集团)有限公司 | Stress-free pressing device |
CN112045213A (en) * | 2020-09-09 | 2020-12-08 | 马鞍山中金超硬材料科技发展有限公司 | Roller ring expansion clamp and machining process thereof |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102921983A (en) * | 2012-11-05 | 2013-02-13 | 中核(天津)科技发展有限公司 | Internal expanding type clamp device |
WO2013170475A1 (en) * | 2012-05-18 | 2013-11-21 | 浙江联宜电机股份有限公司 | Expanding and tightening clamping tool |
CN207288938U (en) * | 2017-10-23 | 2018-05-01 | 云科智能制造(沈阳)有限公司 | One kind automatic positioning tensioning clamper |
CN209632155U (en) * | 2019-01-16 | 2019-11-15 | 沈阳飞机工业(集团)有限公司 | Inner hole machinery tensioning device |
-
2019
- 2019-01-16 CN CN201910039352.0A patent/CN109676171B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013170475A1 (en) * | 2012-05-18 | 2013-11-21 | 浙江联宜电机股份有限公司 | Expanding and tightening clamping tool |
CN102921983A (en) * | 2012-11-05 | 2013-02-13 | 中核(天津)科技发展有限公司 | Internal expanding type clamp device |
CN207288938U (en) * | 2017-10-23 | 2018-05-01 | 云科智能制造(沈阳)有限公司 | One kind automatic positioning tensioning clamper |
CN209632155U (en) * | 2019-01-16 | 2019-11-15 | 沈阳飞机工业(集团)有限公司 | Inner hole machinery tensioning device |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111168441A (en) * | 2020-03-16 | 2020-05-19 | 沈阳飞机工业(集团)有限公司 | Stress-free pressing device |
CN111168441B (en) * | 2020-03-16 | 2024-04-16 | 沈阳飞机工业(集团)有限公司 | Stress-free pressing device |
CN112045213A (en) * | 2020-09-09 | 2020-12-08 | 马鞍山中金超硬材料科技发展有限公司 | Roller ring expansion clamp and machining process thereof |
Also Published As
Publication number | Publication date |
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CN109676171B (en) | 2024-01-23 |
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