CN213195735U - Perforating device for wing skin - Google Patents
Perforating device for wing skin Download PDFInfo
- Publication number
- CN213195735U CN213195735U CN202021916813.2U CN202021916813U CN213195735U CN 213195735 U CN213195735 U CN 213195735U CN 202021916813 U CN202021916813 U CN 202021916813U CN 213195735 U CN213195735 U CN 213195735U
- Authority
- CN
- China
- Prior art keywords
- plate
- support
- servo
- servo motor
- servo electric
- 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
Links
Images
Landscapes
- Drilling And Boring (AREA)
Abstract
The utility model discloses a trompil device of wing covering relates to wing processing equipment technical field, including frame, support frame, backup pad, first servo electric jar, servo motor, drill bit, logical groove, the servo electric jar of second, fixed plate, the servo electric jar of third, clamp plate, support bar and pulley, the pulley extends to the support bar top, and servo motor outer wall both sides horizontal symmetry is equipped with the baffle, and the backup pad bottom is equipped with baffle assorted slide rail. The utility model discloses can carry out the centre gripping to the covering to servo motor and the lift adjustment and the horizontal adjustment of drill bit and handle, strengthen the stability of covering, and then realize carrying out diversified trompil processing to the covering, work efficiency is high, and production cycle is short, can roll the support to the covering, and covering processing feeding ejection of compact operation is more convenient, can add the piece that produces man-hour to servo motor and shelter from the processing, can protect the processing to servo motor, avoids impaired.
Description
Technical Field
The utility model relates to a wing processing equipment technical field specifically is a trompil device of wing covering.
Background
A wing is one of the important parts of an aircraft, mounted on the fuselage. The main function of the wing is to generate lift force, and good stability and maneuverability are formed by the wing and the tail wing. Wings are typically made up of spars, longitudinal walls, stringers, ribs, and skins. The skin is a dimensional component which is wrapped outside the framework structure of the airplane and is fixed on the framework by using an adhesive or rivets to form the aerodynamic appearance of the airplane. The skin functions directly to form a streamlined outer surface of the wing. In order to minimize the drag on the wing, the skin should be smooth. For this purpose, the transverse bending stiffness of the skin should be increased in order to reduce its in-flight buckling. From the aspect of stress, the aerodynamic load directly acts on the skin. The skin is thus subjected to local aerodynamic loads perpendicular to its surface.
The existing holing device for the wing skin mostly adopts manual handheld instruments to carry out holing, so that the holing processing efficiency is low, and the production cycle is long.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a trompil device of wing covering to solve the problem that proposes among the above-mentioned background art.
In order to solve the technical problem, the utility model provides a following technical scheme: a pore-forming device for a wing skin comprises a frame, wherein a support frame is arranged at the top of the frame, a support plate is arranged on the inner side of the support frame above the frame, a plurality of first servo electric cylinders are vertically arranged at the bottom of the support frame, the bottom of the first servo electric cylinders is fixedly connected with the top of the support plate, movably connected servo motors are symmetrically arranged on two sides of the top of the support plate, a drill bit is arranged below the support plate through an output shaft of the servo motors, through grooves matched with the servo motors are formed in the top of the support plate, second servo electric cylinders are horizontally and symmetrically arranged on two sides of the inner wall of the support plate, one end of each second servo electric cylinder is fixedly connected with the outer wall of the servo motor, fixing plates are symmetrically arranged at two ends of the inner wall of the support frame, a plurality of third servo, the third servo electric cylinder bottom with clamp plate top fixed connection, frame top both sides in support frame below symmetry is equipped with the support bar, the support bar inboard is equipped with the pulley that a plurality of rotation is connected, the pulley extends to the support bar top, servo motor outer wall both sides horizontal symmetry is equipped with the baffle, the backup pad bottom be equipped with baffle assorted slide rail.
Furthermore, the outer wall of the servo motor is horizontally provided with a sliding plate, the inner wall of the supporting plate is provided with a sliding groove matched with the sliding plate, and when the servo motor is moved and adjusted, the sliding plate slides along the sliding groove, so that the stability of the servo motor can be enhanced.
Further, the frame includes the workstation, the workstation bottom is equipped with a plurality of support column, and the workstation is used for supporting the equipment at frame top, and the support column can support the workstation bottom.
Furthermore, the length of the pressing plate is smaller than that of the fixing plate, so that the pressing plate can be adjusted in a lifting mode on the inner side of the support frame.
Furthermore, the height of the supporting bar is larger than the length of the drill bit, so that the drill bit can penetrate through the skin, and the drill bit is prevented from being in contact damage with the rack.
Furthermore, the distance between two adjacent pulleys is equal to the outer diameter of the pulleys, so that the sliding support effect of the pulleys is good, and the stability is good.
Furthermore, the length of the baffle is smaller than one eighth of the length of the supporting plate, so that the baffle can slide on the sliding rail at the bottom of the supporting plate, and the moving range is larger.
Compared with the prior art, the utility model discloses the beneficial effect who reaches is:
1. the utility model discloses a set up backup pad, first servo electric jar, servo motor, drill bit, second servo electric jar, third servo electric jar, clamp plate and support bar, can carry out the centre gripping to the covering to servo motor and the lift adjustment and the horizontal adjustment of drill bit, can strengthen the stability of covering, and then realize carrying out diversified trompil processing to the covering, work efficiency is high, production cycle is short;
2. the utility model discloses a set up pulley, baffle and slide rail, can roll the skin and support, skin processing feeding ejection of compact operation is more convenient, can add the piece that produces man-hour to the servo motor trompil and shelter from the processing, can protect the processing to servo motor, avoids impaired.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
FIG. 1 is a front view of the present invention as a whole;
FIG. 2 is a front sectional view of the whole body of the present invention;
fig. 3 is an enlarged schematic view of fig. 2 a according to the present invention;
fig. 4 is a front view of the servo motor of the present invention;
in the figure: 1. a frame; 2. a support frame; 3. a support plate; 4. a first servo electric cylinder; 5. a servo motor; 6. A drill bit; 7. a through groove; 8. a second servo electric cylinder; 9. a fixing plate; 10. a third servo electric cylinder; 11. pressing a plate; 12. a supporting strip; 13. a pulley; 14. a baffle plate; 15. a slide rail; 16. a sliding plate; 17. a chute; 18. a work table; 19. and (4) a support column.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. 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 perforating device for the wing skin shown in fig. 1-3 comprises a frame 1, wherein a support frame 2 is arranged at the top of the frame 1, a support plate 3 is arranged on the inner side of the support frame 2 above the frame 1, a plurality of first servo electric cylinders 4 are vertically arranged at the bottom of the support frame 2, the bottoms of the first servo electric cylinders 4 are fixedly connected with the top of the support plate 3, movably connected servo motors 5 are symmetrically arranged at two sides of the top of the support plate 3, a drill bit 6 is arranged below the support plate 3 at the output shaft of the servo motor 5, a through groove 7 matched with the servo motor 5 is arranged at the top of the support plate 3, second servo electric cylinders 8 are horizontally and symmetrically arranged at two sides of the inner wall of the support plate 3, one end of each second servo electric cylinder 8 is fixedly connected with the outer wall of the servo motor 5, and fixing plates 9, the bottom of the fixing plate 9 is provided with a plurality of third servo electric cylinders 10, a press plate 11 movably connected with the bottom of the fixing plate 9 is arranged below the fixing plate 9, the bottom of each third servo electric cylinder 10 is fixedly connected with the top of the press plate 11, and two sides of the top of the rack 1 are symmetrically provided with support bars 12 below the support frames 2.
The outer wall of the servo motor 5 is horizontally provided with a sliding plate 16, the inner wall of the supporting plate 3 is provided with a sliding groove 17 matched with the sliding plate 16, and when the servo motor 5 is moved and adjusted, the sliding plate 16 slides along the sliding groove 17, so that the stability of the servo motor 5 can be enhanced.
The length of the pressing plate 11 is smaller than that of the fixing plate 9, so that the pressing plate 11 can be adjusted in a lifting mode on the inner side of the support frame 2.
The height of the supporting bar 12 is larger than the length of the drill bit 6, so that the drill bit 6 can penetrate through the skin, and the drill bit 6 is prevented from being in contact damage with the rack 1.
The implementation mode is specifically as follows: when the adjustable skin-lifting device is used, the supporting plate 3, the first servo electric cylinder 4, the servo motor 5, the drill bit 6, the second servo electric cylinder 8, the third servo electric cylinder 10, the pressing plate 11 and the supporting bar 12 are arranged, the supporting bar 12 supports a skin, the supporting plate 3 can support the servo motor 5, the first servo electric cylinder 4 is adjusted to stretch, the supporting plate 3 can be adjusted to lift and adjust, further, the lifting adjustment of the servo motor 5 and the drill bit 6 is realized, the servo motor 5 drives the drill bit 6 to rotate, the drill bit 6 conducts hole forming processing on the skin, the third servo electric cylinder 10 is adjusted to stretch and adjust, the lifting adjustment of the pressing plate 11 can be realized, the pressing plate 11 clamps the skin, the stability of the skin is enhanced, the second servo electric cylinder 8 is adjusted to stretch and adjust, the servo motor 5 can be pushed to horizontally move along the through groove 7, and the horizontal position of the servo motor 5, the skin is subjected to multi-directional hole forming processing, so that the working efficiency is high, and the production period is short; the embodiment specifically solves the problems that in the prior art, most of the existing hole forming devices for the wing skins adopt manual handheld instruments to form holes, the hole forming processing efficiency is low, and the production period is long.
The opening device for the wing skin shown in the attached figures 1 to 4 further comprises a plurality of pulleys 13 rotatably connected with the inner side of the supporting bar 12, the pulleys 13 extend to the upper side of the supporting bar 12, baffles 14 are horizontally and symmetrically arranged on two sides of the outer wall of the servo motor 5, and slide rails 15 matched with the baffles 14 are arranged at the bottom of the supporting plate 3.
The distance between two adjacent pulleys 13 is equal to the outer diameter of the pulley 13, so that the sliding support effect of the pulley 13 is good, and the stability is good.
The length of the baffle plate 14 is less than one eighth of the length of the support plate 3, so that the baffle plate 14 can slide on the slide rail 15 at the bottom of the support plate 3, and the moving range is larger.
The implementation mode is specifically as follows: during the use, through setting up pulley 13, baffle 14 and slide rail 15, pulley 13 rolls the support to the covering in support bar 12 inboard, covering processing feeding ejection of compact operation is more convenient, when servo motor 5 carries out the horizontal motion, baffle 14 moves along servo motor 5, slide rail 15 guides baffle 14, strengthen baffle 14's stability, baffle 14 can shelter from the processing to the piece that produces during processing of servo motor 5 trompil, can protect servo motor 5 and handle, avoid impaired.
The utility model discloses the theory of operation:
referring to the attached drawings 1-3 of the specification, by arranging the supporting plate 3, the first servo electric cylinder 4, the servo motor 5, the drill bit 6, the second servo electric cylinder 8, the third servo electric cylinder 10, the pressing plate 11 and the supporting bars 12, the lifting adjustment and the horizontal adjustment of the servo motor 5 and the drill bit 6 can be realized, the skin can be clamped, the stability of the skin is enhanced, and then the multidirectional holing processing treatment on the skin is realized, so that the working efficiency is high, and the production period is short;
further, referring to the attached drawings 1-4 of the specification, the pulley 13, the baffle 14 and the slide rail 15 are arranged, so that the skin can be supported in a rolling mode, the skin processing feeding and discharging operation is more convenient, the generated fragments can be shielded during the hole opening processing of the servo motor 5, the servo motor 5 can be protected, and the damage can be avoided.
It is noted that, herein, relational terms such as first and second, 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.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (7)
1. The utility model provides a trompil device of wing skin, includes frame (1), its characterized in that: the support frame (2) is arranged at the top of the rack (1), a support plate (3) is arranged on the inner side of the support frame (2) and above the rack (1), a plurality of first servo electric cylinders (4) are vertically arranged at the bottom of the support frame (2), the bottom of each first servo electric cylinder (4) is fixedly connected with the top of the support plate (3), movably connected servo motors (5) are symmetrically arranged on two sides of the top of the support plate (3), drill bits (6) are arranged below the support plate (3) through output shafts of the servo motors (5), through grooves (7) matched with the servo motors (5) are formed in the top of the support plate (3), second servo electric cylinders (8) are horizontally and symmetrically arranged on two sides of the inner wall of the support plate (3), one ends of the second servo electric cylinders (8) are fixedly connected with the outer wall of the servo motors (5), fixing plates (9) are symmetrically arranged on two ends of, fixed plate (9) bottom is equipped with a plurality of third servo electric jar (10), fixed plate (9) below is equipped with swing joint's clamp plate (11), third servo electric jar (10) bottom with clamp plate (11) top fixed connection, frame (1) top both sides in support frame (2) below symmetry is equipped with support bar (12), support bar (12) inboard is equipped with pulley (13) that a plurality of rotated the connection, pulley (13) extend to support bar (12) top, servo motor (5) outer wall both sides horizontal symmetry is equipped with baffle (14), backup pad (3) bottom be equipped with baffle (14) assorted slide rail (15).
2. The hole forming device for the wing skin according to claim 1, wherein: the outer wall of the servo motor (5) is horizontally provided with a sliding plate (16), and the inner wall of the supporting plate (3) is provided with a sliding groove (17) matched with the sliding plate (16).
3. The hole forming device for the wing skin according to claim 1, wherein: the frame (1) comprises a workbench (18), and a plurality of supporting columns (19) are arranged at the bottom of the workbench (18).
4. The hole forming device for the wing skin according to claim 1, wherein: the length of the pressure plate (11) is smaller than that of the fixing plate (9).
5. The hole forming device for the wing skin according to claim 1, wherein: the height of the supporting strip (12) is greater than the length of the drill bit (6).
6. The hole forming device for the wing skin according to claim 1, wherein: the distance between two adjacent pulleys (13) is equal to the outer diameter of the pulleys (13).
7. The hole forming device for the wing skin according to claim 1, wherein: the length of the baffle plate (14) is less than one eighth of the length of the support plate (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021916813.2U CN213195735U (en) | 2020-09-04 | 2020-09-04 | Perforating device for wing skin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021916813.2U CN213195735U (en) | 2020-09-04 | 2020-09-04 | Perforating device for wing skin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213195735U true CN213195735U (en) | 2021-05-14 |
Family
ID=75844420
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021916813.2U Active CN213195735U (en) | 2020-09-04 | 2020-09-04 | Perforating device for wing skin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213195735U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117508630A (en) * | 2024-01-04 | 2024-02-06 | 成都市鸿侠科技有限责任公司 | Size-adjustable aircraft side aileron assembly type frame |
-
2020
- 2020-09-04 CN CN202021916813.2U patent/CN213195735U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117508630A (en) * | 2024-01-04 | 2024-02-06 | 成都市鸿侠科技有限责任公司 | Size-adjustable aircraft side aileron assembly type frame |
| CN117508630B (en) * | 2024-01-04 | 2024-04-05 | 成都市鸿侠科技有限责任公司 | Size-adjustable aircraft side aileron assembly type frame |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206046984U (en) | A kind of double riveter | |
| CN213195735U (en) | Perforating device for wing skin | |
| CN212917913U (en) | Aluminum template nicking mechanism | |
| CN208020394U (en) | A kind of building glued board shaping equipment | |
| CN212919621U (en) | Processing device for environment-friendly board | |
| CN207564246U (en) | A kind of front frame burr remover | |
| CN211161561U (en) | High-efficient group angle machine of aluminium door and window hydraulic pressure | |
| CN207840689U (en) | A kind of multi-functional copper coin processing machine for copper coin processing | |
| CN216406684U (en) | Support for pneumatic frame column type drilling machine | |
| CN202780349U (en) | End beam grouping forming device | |
| CN213197521U (en) | Fixing device of wing skin mechanism | |
| CN212682636U (en) | Aluminum profile cutting machine with clamping structure | |
| CN111958281A (en) | Titanium alloy stick processingequipment | |
| CN211768725U (en) | Turnover frame for forged products | |
| CN213197788U (en) | Cutting fixing support for aircraft wing production | |
| CN211968884U (en) | UV flatbed printer | |
| CN210132858U (en) | Printing machine capable of preventing crush injury for printing glass | |
| CN205394557U (en) | Special pneumatic two direction manipulators of compound compaction production line | |
| CN215788488U (en) | Clamping device is used in processing of car B post planking | |
| CN218318794U (en) | Multi-level gravity sliding frame | |
| CN206317517U (en) | A kind of metal flat pattern printing device | |
| CN212945693U (en) | Stringer cutting device for fuselage frame | |
| CN216138200U (en) | Cutting equipment of panel for building construction | |
| CN218556762U (en) | Clamping tool for machining cylinder mounting plate | |
| CN219383939U (en) | Feeding mechanism for photovoltaic aluminum profile frame |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: No.23, Hongbin Road, Yuhong District, Shenyang City, Liaoning Province Patentee after: Liaoning Huatian Aviation Technology Co.,Ltd. Address before: No.23, Hongbin Road, Yuhong District, Shenyang City, Liaoning Province Patentee before: SHENZHEN HUATIAN AVIATION MACHINERY CO.,LTD. |
|
| CP01 | Change in the name or title of a patent holder |