CN214867481U - Aeroengine inclined hole drilling clamp with excellent positioning effect - Google Patents

Aeroengine inclined hole drilling clamp with excellent positioning effect Download PDF

Info

Publication number
CN214867481U
CN214867481U CN202120402294.6U CN202120402294U CN214867481U CN 214867481 U CN214867481 U CN 214867481U CN 202120402294 U CN202120402294 U CN 202120402294U CN 214867481 U CN214867481 U CN 214867481U
Authority
CN
China
Prior art keywords
screw rod
positioning seat
head
screw
positioning
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.)
Active
Application number
CN202120402294.6U
Other languages
Chinese (zh)
Inventor
蒋杰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hangshuo Suzhou Aviation Equipment Technology Co ltd
Original Assignee
Hangshuo Suzhou Aviation Equipment Technology Co ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hangshuo Suzhou Aviation Equipment Technology Co ltd filed Critical Hangshuo Suzhou Aviation Equipment Technology Co ltd
Priority to CN202120402294.6U priority Critical patent/CN214867481U/en
Application granted granted Critical
Publication of CN214867481U publication Critical patent/CN214867481U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The utility model discloses an aeroengine that location effect is excellent bores inclined hole anchor clamps, including anchor clamps main part and pressure head, the upper end fixedly connected with type piece of anchor clamps main part, No. two positioning seats of outside fixedly connected with of anchor clamps main part and a positioning seat, the one end of a positioning seat is provided with the screw rod No. one, the other end of a positioning seat is provided with the screw rod head No. one, the outside of screw rod head is provided with the briquetting No. one, the one end of No. two positioning seats is provided with the screw rod No. two. A aeroengine that location effect is excellent bores inclined hole anchor clamps, be equipped with the pressfitting positioning mechanism and the location type piece of two sets of slopes, can make things convenient for better treating the processing part and fix a position, fixed effect is more excellent, increases stability can, it is more swift convenient to drill, can also increase the performance of device, fixes a position more fast, convenient to use brings better use prospect.

Description

Aeroengine inclined hole drilling clamp with excellent positioning effect
Technical Field
The utility model relates to an anchor clamps field, in particular to aeroengine that location effect is excellent bores inclined hole anchor clamps.
Background
Drilling inclined hole anchor clamps are the support equipment of location of driling, and aviation part has very high requirement when carrying out the processing preparation, needs higher precision, and when engine part drilled, anchor clamps's use is more important, and along with the continuous development of science and technology, people also are more and more high to the manufacturing process requirement of drilling inclined hole anchor clamps.
The existing inclined hole drilling clamp has certain defects when in use, firstly, inclined hole drilling operation cannot be conveniently carried out, the positioning performance is poor, deviation easily occurs, the use of people is not facilitated, in addition, the movable condition easily occurs when in use, the stability is reduced, certain adverse effect is brought to the use process of people, and for the purpose, the inclined hole drilling clamp for the aircraft engine with excellent positioning effect is provided.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model provides a not enough to prior art, the utility model provides an aeroengine that location effect is excellent bores inclined hole anchor clamps is equipped with the pressfitting positioning mechanism and the location type piece of two sets of slopes, can make things convenient for better treating the processing part and fix a position, and fixed effect is more excellent, increases stability can, and it is more convenient to drill, can also increase the performance of device, and the location is faster, and convenient to use can effectively solve the problem in the background art.
(II) technical scheme
In order to achieve the above purpose, the utility model adopts the following technical scheme: the utility model provides an aeroengine that location effect is excellent bores inclined hole anchor clamps, includes anchor clamps main part and pressure head, the upper end fixedly connected with type piece of anchor clamps main part, No. two positioning seats of outside fixedly connected with of anchor clamps main part and a positioning seat, the one end of a positioning seat is provided with the screw rod No. one, the other end of a positioning seat is provided with the screw rod head No. one, the outside of screw rod head is provided with the briquetting No. one, the one end of No. two positioning seats is provided with the screw rod No. two, the other end of No. two positioning seats is provided with the screw rod head No. two, the outside of No. two screw rod heads is provided with the briquetting No. two, it remains the processing part to set up between briquetting and the briquetting No. two, the outside of type piece is provided with screw, drill bushing and pin, the lower extreme of pressure head is provided with the drilling rod.
Preferably, the angle between the first positioning seat and the second positioning seat is 90 degrees, and the inclination angle between the second positioning seat and the clamp main body is 45 degrees.
Preferably, the outer side of the upper end of the clamp main body is fixedly connected with one side of the profile block through a drill bushing, a screw and a pin.
Preferably, a first spiral groove is formed between the second positioning seat and the second screw rod, the inner portion of the second positioning seat is movably connected with the outer wall of the second screw rod through the first spiral groove, a second spiral groove is formed between the first positioning seat and the first screw rod, and the inner portion of the first positioning seat is movably connected with the outer wall of the first screw rod through the second spiral groove.
Preferably, be provided with the fixed block No. one between screw rod and the screw head, the one end fixed connection of one end through a fixed block and screw head of screw rod No. one, be provided with the fixed block No. two between No. two screw rods and the screw head No. two, the one end fixed connection of No. two fixed blocks and No. two screw heads is passed through to the one end of No. two screw rods.
Preferably, the second pressing block and the first pressing block are pressed at the positions of the part to be processed and the pressing head.
(III) advantageous effects
Compared with the prior art, the utility model provides an aeroengine bores inclined hole anchor clamps that location effect is excellent possesses following beneficial effect: the aero-engine inclined hole drilling clamp with excellent positioning effect can conveniently and better position a part to be processed through two groups of inclined pressing positioning mechanisms and positioning blocks, has more excellent fixing effect, increases the stability, can more quickly and conveniently drill holes, can also increase the service performance of a device, is quicker to position and convenient to use, places the part to be processed at the position among the blocks, the first pressing block and the second pressing block for fixing, can move among the first screw rod, the first screw head, the first pressing block, the second screw rod, the second screw head and the second pressing block, positions and adjusts the position of the part to be processed, is suitable for more part models, is convenient to adjust, positions the blocks through drill sleeves and screws, presses down the position of a pressing head after positioning, performs drilling operation after the drill rods are pressed to the position of the drill sleeves, the operation is more swift, and whole brill inclined hole anchor clamps simple structure, convenient operation, the effect of use is better for traditional mode.
Drawings
Fig. 1 is the utility model relates to an aeroengine that positioning effect is excellent bores inclined hole anchor clamps's overall structure sketch map.
Fig. 2 is the utility model relates to a positioning effect is excellent among aeroengine inclined hole anchor clamps pressure head's schematic structure diagram.
Fig. 3 is the utility model relates to an aeroengine that positioning effect is excellent bores inclined hole anchor clamps in positioning mechanism's schematic structure.
In the figure: 1. a clamp body; 2. molding blocks; 3. drilling a sleeve; 4. a screw; 5. a pin; 6. a first screw rod; 7. pressing blocks II; 8. a part to be processed; 9. a first positioning seat; 10. a first screw head; 11. pressing a block I; 12. a second screw head; 13. a second positioning seat; 14. a second screw; 15. a pressure head; 16. and (5) drilling a rod.
Detailed Description
The technical solutions of the present invention will be described clearly and completely with reference to the accompanying drawings and detailed description, but those skilled in the art will understand that the following described embodiments are some, not all, of the embodiments of the present invention, and are only used for illustrating the present invention, and should not be construed as limiting the scope of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention. The examples, in which specific conditions are not specified, were conducted under conventional conditions or conditions recommended by the manufacturer. The reagents or instruments used are not indicated by the manufacturer, and are all conventional products available commercially.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1-3, an aeroengine inclined hole drilling fixture with excellent positioning effect comprises a fixture main body 1 and a pressure head 15, wherein a section block 2 is fixedly connected to the upper end of the fixture main body 1, a second positioning seat 13 and a first positioning seat 9 are fixedly connected to the outer side of the fixture main body 1, a first screw rod 6 is arranged at one end of the first positioning seat 9, a first screw head 10 is arranged at the other end of the first positioning seat 9, a first pressing block 11 is arranged at the outer side of the first screw head 10, a second screw rod 14 is arranged at one end of the second positioning seat 13, a second screw head 12 is arranged at the other end of the second positioning seat 13, a second pressing block 7 is arranged at the outer side of the second screw head 12, a part 8 to be processed is arranged between the first pressing block 11 and the second pressing block 7, a screw 4, a drill bushing 3 and a pin 5 are arranged at the outer side of the section block 2, and a drill rod 16 is arranged at the lower end of the pressure head 15.
Further, the angle between the first positioning seat 9 and the second positioning seat 13 is 90 degrees, and the inclination angle between the second positioning seat 13 and the fixture main body 1 is 45 degrees, and has a certain inclination angle.
Furthermore, the outer side of the upper end of the clamp main body 1 is fixedly connected with one side of the profile block 2 through a drill bushing 3, a screw 4 and a pin 5, so that drilling and positioning can be conveniently and better carried out.
Furthermore, a first spiral groove is formed between the second positioning seat 13 and the second screw rod 14, the inner portion of the second positioning seat 13 is movably connected with the outer wall of the second screw rod 14 through the first spiral groove, a second spiral groove is formed between the first positioning seat 9 and the first screw rod 6, and the inner portion of the first positioning seat 9 is movably connected with the outer wall of the first screw rod 6 through the second spiral groove, so that positioning adjustment can be carried out.
Furthermore, a first fixing block is arranged between the first screw rod 6 and the first screw head 10, one end of the first screw rod 6 is fixedly connected with one end of the first screw head 10 through the first fixing block, a second fixing block is arranged between the second screw rod 14 and the second screw head 12, one end of the second screw rod 14 is fixedly connected with one end of the second screw head 12 through the second fixing block, and more machining part models are used.
Furthermore, the second pressing block 7 and the first pressing block 11 press the part 8 to be processed and the pressure head 15, so that pressing and fixing can be conveniently and better carried out.
The working principle is as follows: the utility model comprises a clamp main body 1, a pressure head 15, a molding block 2, a drill bushing 3, a screw 4, a pin 5, a screw rod 6, a second pressing block 7, a part 8 to be processed, a positioning seat 9, a screw head 10, a pressing block 11, a second screw head 12, a second positioning seat 13, a second screw rod 14 and a pressure head 15, wherein when in use, the part 8 to be processed is placed between the molding block 2, the first pressing block 11 and the second pressing block 7 for fixation, the first screw rod 6, the first screw head 10, the first pressing block 11, the second screw rod 14, the second screw head 12 and the second pressing block 7 can move, the position of the part 8 to be processed is positioned and adjusted, the device is suitable for more part models, the adjustment is convenient, the molding block 2 is positioned by the drill bushing 3 and the screw 4, after the positioning, the position of the pressure head 15 is pressed down, the drilling operation is carried out after the position of the drill bushing 3 is pressed through a drill rod 16, the operation is more swift, and the pressfitting positioning mechanism through two sets of slopes can be convenient better with the location type piece treat the processing part fix a position, and fixed effect is more excellent, increases the stability can, and it is more swift convenient to drill, can also increase the performance of device, fixes a position more fast, convenient to use.
It is noted that, herein, relational terms such as first and second (a, b, etc.) and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (6)

1. The utility model provides an aeroengine that positioning effect is excellent bores inclined hole anchor clamps, includes anchor clamps main part (1) and pressure head (15), its characterized in that: the fixture comprises a fixture main body (1), wherein a molding block (2) is fixedly connected to the upper end of the fixture main body (1), a second positioning seat (13) and a first positioning seat (9) are fixedly connected to the outer side of the fixture main body (1), a first screw rod (6) is arranged at one end of the first positioning seat (9), a first screw rod head (10) is arranged at the other end of the first positioning seat (9), a first pressing block (11) is arranged on the outer side of the first screw rod head (10), a second screw rod (14) is arranged at one end of the second positioning seat (13), a second screw rod head (12) is arranged at the other end of the second positioning seat (13), a second pressing block (7) is arranged on the outer side of the second screw rod head (12), a part (8) to be machined is arranged between the first pressing block (11) and the second pressing block (7), a screw (4), a drill bushing (3) and a pin (5) are arranged on the outer side of the molding block (2), the lower end of the pressure head (15) is provided with a drill rod (16).
2. The aero-engine inclined hole drilling clamp with excellent positioning effect as claimed in claim 1, wherein the clamp comprises: the angle between the first positioning seat (9) and the second positioning seat (13) is 90 degrees, and the inclination angle between the second positioning seat (13) and the clamp main body (1) is 45 degrees.
3. The aero-engine inclined hole drilling clamp with excellent positioning effect as claimed in claim 1, wherein the clamp comprises: the outer side of the upper end of the clamp main body (1) is fixedly connected with one side of the profile block (2) through a drill bushing (3), a screw (4) and a pin (5).
4. The aero-engine inclined hole drilling clamp with excellent positioning effect as claimed in claim 1, wherein the clamp comprises: a first spiral groove is formed between the second positioning seat (13) and the second screw rod (14), the inner portion of the second positioning seat (13) is movably connected with the outer wall of the second screw rod (14) through the first spiral groove, a second spiral groove is formed between the first positioning seat (9) and the first screw rod (6), and the inner portion of the first positioning seat (9) is movably connected with the outer wall of the first screw rod (6) through the second spiral groove.
5. The aero-engine inclined hole drilling clamp with excellent positioning effect as claimed in claim 1, wherein the clamp comprises: be provided with the fixed block No. one between screw rod (6) and screw head (10), the one end fixed connection of one fixed block and screw head (10) is passed through to the one end of screw rod (6), be provided with the fixed block No. two between No. two screw rod (14) and No. two screw head (12), the one end fixed connection of No. two fixed blocks and No. two screw head (12) is passed through to the one end of No. two screw rods (14).
6. The aero-engine inclined hole drilling clamp with excellent positioning effect as claimed in claim 1, wherein the clamp comprises: and the second pressing block (7) and the first pressing block (11) are pressed on the parts (8) to be processed and the pressure head (15).
CN202120402294.6U 2021-02-24 2021-02-24 Aeroengine inclined hole drilling clamp with excellent positioning effect Active CN214867481U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202120402294.6U CN214867481U (en) 2021-02-24 2021-02-24 Aeroengine inclined hole drilling clamp with excellent positioning effect

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202120402294.6U CN214867481U (en) 2021-02-24 2021-02-24 Aeroengine inclined hole drilling clamp with excellent positioning effect

Publications (1)

Publication Number Publication Date
CN214867481U true CN214867481U (en) 2021-11-26

Family

ID=78859240

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120402294.6U Active CN214867481U (en) 2021-02-24 2021-02-24 Aeroengine inclined hole drilling clamp with excellent positioning effect

Country Status (1)

Country Link
CN (1) CN214867481U (en)

Similar Documents

Publication Publication Date Title
CN214867481U (en) Aeroengine inclined hole drilling clamp with excellent positioning effect
CN109483435A (en) A kind of composite fixture that clip is detected, crosses, drilled
CN215510058U (en) Fixing device is used in spare part processing
CN215469724U (en) Machining clamp structure
CN213827970U (en) Stop device is used in anchor clamps processing
CN205519804U (en) Motor flange jig
CN105082003B (en) A kind of clamp method of micro-test sample clamping device
CN214868726U (en) Quick location aeroengine four-axis anchor clamps
CN103433533B (en) Microscope hinge drill jig
CN208427755U (en) Cylindrical work drilling processing tooling
CN213411161U (en) Medical instrument's quick location clamping tool
CN208976894U (en) A kind of processing device for oblique oil holes of crankshafts
CN213764066U (en) Wheel disc type radial drilling machine
CN217194022U (en) Marine U type pipe strap fluting auxiliary fixtures
CN209288781U (en) A kind of positioning clamp for machining of bracket holes
CN220741269U (en) Pipe exchange port cutting device
CN219484973U (en) Compression-resistant clamp with high adaptability
CN218946943U (en) Adjustable fixture for cutter production
CN210451871U (en) Axial fan blade back-drawing hole machining clamp
CN214770593U (en) Clamping device for oil tank valve body
CN213827070U (en) Boring cutter bar convenient to adjust
CN206967037U (en) A kind of lathe drilling-milling apparatus
CN212794068U (en) Vertical drilling fixture for plunger sleeves
CN211803929U (en) Desk-top lathe of inflation valve body production drilling
CN213729340U (en) Online turning mechanism of rotary kiln tyre profile modeling

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant