CN211517236U - Adjustable clamp for three-dimensional measurement of small aviation blade - Google Patents
Adjustable clamp for three-dimensional measurement of small aviation blade Download PDFInfo
- Publication number
- CN211517236U CN211517236U CN201922131544.2U CN201922131544U CN211517236U CN 211517236 U CN211517236 U CN 211517236U CN 201922131544 U CN201922131544 U CN 201922131544U CN 211517236 U CN211517236 U CN 211517236U
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- small
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- aviation
- blade
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Abstract
The utility model discloses an adjustable anchor clamps for three-dimensional measurement of small-size aviation blade. The utility model discloses to less and the fixed, unable scheduling problem of adjusting of size of the anchor clamps that use the structured light projection mode to measure small-size aviation blade now, designed an adjustable anchor clamps that is used for three-dimensional measurement of small-size aviation blade. The utility model consists of four modules which can move along the direction limited by respective T-shaped guide rail devices, and aviation blades with different sizes are adjusted and clamped by respective adjusting bolts; the bottom main module is a disc base and is provided with four threaded holes for connecting and fixing. Can stabilize the clamping to the small-size aviation blade of equidimension not in certain specification range through the adjusting bolt of adjustment top and horizontal direction to the screw hole that accessible disc base had is connected with corresponding measuring desk, with the stability of further improvement aviation blade when measuring.
Description
Technical Field
The utility model relates to a design of small-size anchor clamps especially relates to the adjustable anchor clamps design aspect of using the small-size aviation blade of structured light measurement.
Background
When the morphology of a small aviation blade or other precision parts is measured by using structured light, the aviation blade needs to be vertically placed and kept in a stable state, so that the effect and the precision of grating projection measurement are ensured. And current blade measurement anchor clamps kind is less, mostly is fixed size, can not adjust the type anchor clamps or directly adopts the sticky tape mode of pasting to fix the blade on the measuring table, carries out projection measurement with structured light. Therefore, the clamp can stably clamp small aviation blades of different sizes in a certain specification range, has certain universality and stability, meets the requirement of a structured light measurement process, can well solve the problems, and has high practicability.
Disclosure of Invention
In order to overcome the not enough of above-mentioned prior art, the utility model provides an adjustable anchor clamps for small-size aviation blade three-dimensional measurement makes things convenient for the scientific research or the social production process of the small-size aviation blade of structured light measurement.
The utility model adopts the technical proposal that: the fixture is mainly formed by combining four main body modules, and is provided with one T-shaped guide rail device at the bottom in the horizontal direction, and one T-shaped guide rail device at the left and right in the vertical direction; the corresponding modules move and are fastened according to the direction limited by the T-shaped guide rail device by screwing adjusting bolts in the horizontal direction and the vertical direction so as to clamp small aviation blades with different sizes in a certain specification range; the main module at the bottom is integrated with the disc base, and the disc base is provided with four threaded holes for fixing on the measuring table.
The utility model has the advantages that, compare with prior art, the beneficial effects of the utility model are that can adjust the distance between level, the vertical direction module through the adjusting bolt of rotatory level and vertical direction, realize the small-size aviation blade centre gripping of certain specification within range to the elasticity of centre gripping is adjusted to the rotatory each adjusting bolt of accessible, thereby improves the commonality of this anchor clamps. The bottom main module and the disc base are integrated and are provided with four threaded holes, so that the fixture is convenient to install and fix on a measuring table, and the stability of the fixture is effectively improved.
Drawings
Fig. 1 is a three-dimensional view of the overall structure of the clamp.
Fig. 2 is an exploded view of the entire clip.
Fig. 3 is a front view of the overall structure of the clamp.
Fig. 4 is a side view of the overall structure of the clamp.
Fig. 5 is a top view of the overall structure of the clamp.
Fig. 6 is a perspective three-dimensional view of the bottom main module.
Fig. 7 is a perspective three-dimensional view of the bottom sub-module.
Fig. 8 is a perspective three-dimensional view of the top module.
Fig. 9 is a front view of the effect of clamping the blade.
FIG. 10 is a perspective three-dimensional view of a blade clamping effect.
Reference numerals: 1-vertical T-shaped rail means; 2-a horizontal T-shaped rail arrangement; 3-top adjusting bolt; 4-top sub-module; 5-bottom sub-module; 6-horizontal adjusting bolt; 7-base threaded hole; 8-bottom main module; 9-top main module; 10-aviation blade model.
Detailed Description
The invention will be further described with reference to the accompanying drawings and specific embodiments:
fig. 1 is a three-dimensional view of the overall structure of the clamp. The bottom sub-module, the top main module and the top sub-module move in the direction limited by respective T-shaped guide rail devices by rotating the adjusting bolts in the horizontal direction and the vertical direction, so that the clamping device is suitable for clamping small aviation blades with different sizes in a certain specification range.
In fig. 2, the top sub-module (4) and the top main module (9) have the same specification. The top adjusting bolts (3) are connected with the corresponding bottom modules, move up and down in the direction limited by the vertical T-shaped guide rail device (1) in the vertical direction and are screwed tightly by the top adjusting bolts (3); the bottom sub-module (5) is connected with the bottom main module (8) through a horizontal adjusting bolt (6), and moves in the horizontal direction according to the direction limited by the horizontal T-shaped guide rail device (2) at the bottom, and finally is screwed through the horizontal adjusting bolt (6), so that stable clamping of the small aviation blade is finally realized. Wherein the base of the bottom main module (8) is disc-shaped, has larger stability and is provided with four base threaded holes (7) for connecting with corresponding measuring tables so as to further improve the stability of the clamp.
Fig. 9 is a front view of the clamping effect of a small aviation blade of a certain model, according to the size of the base of the aviation blade, the small aviation blade is clamped by adjusting the top adjusting bolt (3) and the horizontal adjusting bolt (6), and the blade base is clamped by screwing each adjusting bolt, so that the effect of stable clamping is achieved.
Claims (3)
1. The utility model provides an adjustable anchor clamps for three-dimensional measurement of small-size aviation blade, can stabilize the clamping to the small-size aviation blade of equidimension not within a certain specification range, affiliated anchor clamps include: vertical T type guide rail device, horizontal T type guide rail device, two, top main module, the vice module in top, bottom main module, the vice module in bottom, horizontal adjusting bolt are two, its characterized in that: the clamp consists of four modules which can move in the direction limited by respective T-shaped guide rail devices, and aviation blades with different sizes are adjusted and clamped by respective adjusting bolts; the bottom main module is a disc base and is provided with four threaded holes for connecting and fixing.
2. The adjustable clamp for three-dimensional measurement of small aviation blades of claim 1, wherein: the top main module and the top auxiliary module are modules with the same size and specification, and the respective T-shaped guide rail devices are also same in size, so that the universality of parts of the clamp device is increased to a certain extent.
3. The adjustable clamp for three-dimensional measurement of small aviation blades of claim 1, wherein: the bottom main module is a disc base, and threaded holes in the bottom main module can be fixedly connected with corresponding measuring tables, so that the clamping stability of the aviation blade is further improved.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201922131544.2U CN211517236U (en) | 2019-12-03 | 2019-12-03 | Adjustable clamp for three-dimensional measurement of small aviation blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201922131544.2U CN211517236U (en) | 2019-12-03 | 2019-12-03 | Adjustable clamp for three-dimensional measurement of small aviation blade |
Publications (1)
Publication Number | Publication Date |
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CN211517236U true CN211517236U (en) | 2020-09-18 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201922131544.2U Expired - Fee Related CN211517236U (en) | 2019-12-03 | 2019-12-03 | Adjustable clamp for three-dimensional measurement of small aviation blade |
Country Status (1)
Country | Link |
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CN (1) | CN211517236U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114523313A (en) * | 2022-03-16 | 2022-05-24 | 江苏集萃华科智能装备科技有限公司 | Online adjusting mechanism for blade axis |
-
2019
- 2019-12-03 CN CN201922131544.2U patent/CN211517236U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114523313A (en) * | 2022-03-16 | 2022-05-24 | 江苏集萃华科智能装备科技有限公司 | Online adjusting mechanism for blade axis |
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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: 20200918 Termination date: 20211203 |
|
CF01 | Termination of patent right due to non-payment of annual fee |