CN203737866U - Aircraft brake pad riveting machine - Google Patents
Aircraft brake pad riveting machine Download PDFInfo
- Publication number
- CN203737866U CN203737866U CN201320849296.5U CN201320849296U CN203737866U CN 203737866 U CN203737866 U CN 203737866U CN 201320849296 U CN201320849296 U CN 201320849296U CN 203737866 U CN203737866 U CN 203737866U
- Authority
- CN
- China
- Prior art keywords
- slide plate
- positioning disk
- supporting seat
- riveting machine
- aircraft brake
- 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.)
- Expired - Lifetime
Links
- 230000006835 compression Effects 0.000 claims description 6
- 238000007906 compression Methods 0.000 claims description 6
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 238000003825 pressing Methods 0.000 abstract description 6
- 238000000034 method Methods 0.000 description 12
- 230000006978 adaptation Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000001737 promoting effect Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 239000011435 rock Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
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- Braking Arrangements (AREA)
Abstract
The utility model discloses an aircraft brake pad riveting machine. The aircraft brake pad riveting machine comprises a rack and a rivet pressing machine head and is characterized in that a supporting base is arranged on the rack, a sliding plate is arranged on the supporting base, and a slide rail is arranged between the sliding plate and the supporting base; a rotary shaft is arranged in the middle of the sliding plate, the rotary shaft is rotationally connected with the sliding plate, and an index plate and a positioning disk are borne on the rotary shaft; the positioning disk is located above the index plate, the index plate is connected with the positioning disk, and the positioning disk is connected with the rotary shaft; an air cylinder is arranged at one end of the sliding plate, and a sliding plate limiting assembly is arranged at the other end of the sliding plate; the output end of the air cylinder is connected with an indexing block, and the indexing block can be clamped to the index plate; a stand column is arranged on the rack, the rivet pressing machine head is located above the positioning disk and connected with the stand column; a plurality of detachable supporting shafts are evenly distributed on the index plate. Through the aircraft brake pad riveting machine, riveting requirements of various kinds can be well met, slightly worn or deformed brake pads can also be adaptively riveted, and thus production cost is saved and production efficiency is improved.
Description
Technical field
The utility model belongs to riveting machine equipment technical field, and concrete is a kind of aircraft brake sheet riveting machine.
Background technology
Airplane wheel brake assembly is one of important object of aircraft regular maintenance, because brake block belongs to consumable accessory, thus need often to change, and install, detect and need require to carry out in strict accordance with airworthiness standard, to guarantee the safety of flight.At present, what adopt is to the brake block operation that presses on special-purpose equipment, but aircraft brake sheet type kind is various, riveting equipment is high to the coherence request of brake block again, be badly in need of a kind of can be applicable to can to multiple brake block press operation riveting machine.
Utility model content
For the problem existing in background technology, the purpose of this utility model be to provide a kind of can production cost low, production efficiency is high and can meet many kinds riveted joints, the aircraft brake sheet riveting machine that also can carry out self adaptation riveted joint to the brake block of mild wear or distortion.
In order to achieve the above object, the technical solution adopted in the utility model is: aircraft brake sheet riveting machine, comprise frame and the head that presses, and it is characterized in that: described frame is provided with supporting seat, described supporting seat is provided with slide plate, between described slide plate and described supporting seat, is provided with slide rail; Described slide plate middle part is provided with rotating shaft, and described rotating shaft and slide plate are rotationally connected, and carry index dial and positioning disk in described rotating shaft; Described positioning disk is positioned at described index dial top, and described index dial is connected with described positioning disk, and described positioning disk is connected with described rotating shaft; Described slide plate one end is provided with cylinder, and the other end is provided with slide plate limit assembly; The output of described cylinder is connected with calibration piece, and described calibration piece can engage with described index dial; Described frame is provided with column, described in the top that head is positioned at described positioning disk that presses be connected with described column; Uniform a plurality of dismountable back shafts on described index dial.
Preferably, described slide plate limit assembly comprise be positioned at described supporting seat end face positioning seat, be located at the latch on slide plate; Described positioning seat is provided with locating hole, and described latch can engage with described locating hole through described slide plate.Like this, initial position is accurately located and be limited in to slide plate, facilitate material loading or reload.
Preferably, described positioning disk is provided with dismountable compression plate.Like this, not can not the producing and rock of brake block in the process of pressing.
Preferably, comprise riveted joint switch keeper, described riveted joint switch keeper comprises the calibration bar that is arranged on slide plate side, is arranged on the sensor of supporting seat side.Like this, when slide plate is in riveted joint station sliding process, calibration bar is from sensor top process, and sensor sends signal and allows to start lower squeeze riveter head; Complete after riveted joint, slide plate is got back in initial position process, and calibration bar moves with slide plate, and sensor sends signal at stop and allows to start lower squeeze riveter head.
Preferably, described supporting seat is provided with block, and described block is provided with adjusting bolt.Like this, when promoting slide plate when riveting station, block is for the location of slide plate, by regulating the stroke that adjusting bolt can adjusting slider, thereby adapts to the riveted joint of different brake blocks.
Preferably, between described index dial and supporting seat, be provided with riveted joint seat, described riveted joint seat be fixed on the head that presses on supporting seat and described in being positioned under.Like this, in the process pressing, can provide support power, make to press more smooth.
The beneficial effects of the utility model are: can be good at meeting many kind riveted joints, to the brake block of mild wear or distortion, also can carry out self adaptation riveted joint, saved production cost, improved production efficiency.
Accompanying drawing explanation
Fig. 1 is that master of the present utility model looks schematic diagram
Fig. 2 is that schematic diagram is looked on a left side of the present utility model
Fig. 3 is schematic top plan view of the present utility model
In figure: frame 1, the head 2 that presses, supporting seat 3, slide plate 4, slide rail 5, rotating shaft 6, index dial 7, positioning disk 8, cylinder 9, slide plate limit assembly 10, calibration piece 11, back shaft 12, compression plate 13, riveted joint switch keeper 14, block 15, adjusting bolt 16, riveted joint seat 17, column 18, brake block 19;
Wherein: positioning seat 10.1, latch 10.2, locating hole 10.11, calibration bar 14.1, sensor 14.2.
The specific embodiment
As described in Fig. 1 to Fig. 3, aircraft brake sheet riveting machine, comprises frame 1 and the head 2 that presses, and described frame 1 is provided with supporting seat 3, and described supporting seat 3 is provided with slide plate 4, between described slide plate 4 and described supporting seat 3, is provided with slide rail 5; Described slide plate 4 middle parts are provided with rotating shaft 6, and described rotating shaft 6 is rotationally connected with slide plate 4, carries index dial 7 and positioning disk 8 in described rotating shaft 6; Described positioning disk 8 is positioned at described index dial 7 tops, and described index dial 7 is connected with described positioning disk 8, and described positioning disk 8 is connected with described rotating shaft 6; Described slide plate 4 one end are provided with cylinder 9, and the other end is provided with slide plate limit assembly 10; The output of described cylinder 9 is connected with calibration piece 11, and described calibration piece 11 can engage with described index dial 7; Described frame 1 is provided with column 18, described in the top that head 2 is positioned at described positioning disk 8 that presses be connected with described column 18; Uniform a plurality of dismountable back shafts 12 on described index dial 7.
Described slide plate limit assembly 10 comprise be positioned at described supporting seat 3 end faces positioning seat 10.1, be located at the latch 10.2 on slide plate 4; Described positioning seat 10.1 is provided with locating hole 10.11, and described latch 10.2 can engage with described locating hole 10.11 through described slide plate 4.Like this, initial position is accurately located and be limited in to slide plate 4, facilitate material loading or reload.
Preferably, described positioning disk 8 is provided with dismountable compression plate 13.Like this, by compression plate 13, brake block 19 is pressed on index dial 7 tightly, thus in the process of pressing can not the producing and rock of brake block 19.
Preferably, aircraft brake sheet riveting machine also comprises riveted joint switch keeper 14, and described riveted joint switch keeper 14 comprises the calibration bar 14.1 that is arranged on slide plate 4 sides, is arranged on the sensor 14.2 of supporting seat 3 sides.Like this, when slide plate 4 is in riveted joint station sliding process, calibration bar 14.1 is from sensor 14.2 top processes, and sensor 14.2 sends signal and allows to start lower squeeze riveter head 2; Complete after riveted joint, slide plate 4 is got back in initial position process, and calibration bar 14.1 is with slide plate 4 motions, and sensor 14.2 sends signal at stop and allows to start the head 2 that presses.
Preferably, described supporting seat 3 is provided with block 15, and described block 15 is provided with adjusting bolt 16.Like this, when promoting slide plate 4 to riveted joint station, block 15, for the location of slide plate 4, by regulating adjusting bolt 15 to get final product the stroke of adjusting slider 4, thereby adapts to the riveted joint of different brake blocks 19.
Preferably, between described index dial 7 and supporting seat 3, be provided with riveted joint seat 17, described riveted joint seat 17 be fixed on the head 2 that presses on supporting seat 3 and described in being positioned under.Like this, in the process pressing, can provide support power, make to press more smooth.
The course of work of the present utility model is as follows:
While being positioned at initial position, latch 10.2 inserts in locating hole 10.11, slide plate 4 is fixing, can not slide, now cylinder 9 is just in contraction state, and calibration piece 11 is separated with index dial 7, the riveting parts that will rivet with brake block 19 is installed on back shaft 12, then brake block 19 is placed on index dial 7 by positioning disk 8 location, compression plate 13 is connected with fixed disk, compress brake block 19.
Control cylinder 9 makes calibration piece 11 engage with index dial 7, extracts latch 10.2 out, promotes slide plate 4 and moves to riveted joint station, in moving process, calibration bar 14.1 is from sensor 14.2 tops through out-of-date, and sensor 14.2 sends the signal enabling head 2 that presses, and continues to promote slide plate 4 slide plates to riveting station, now slide plate 4 contacts with adjusting bolt 16, the head 2 that presses moves down, and completes riveted joint, when riveted joint, 17 pairs of index dials 7 of riveted joint seat play the effect of support, make to press more smooth.
Complete after a riveting parts riveted joint on back shaft 12, head 2 playback press, then control cylinder 9 shrinks, that calibration piece 11 is separated with index dial 7, rotation-indexing table 7, be the below that next back shaft 12 is positioned at the head 2 that presses, make calibration piece 11 engage with index dial 7 by control cylinder 9, the head 2 that presses has moved down riveted joint.
So circulation, so complete the riveting work on back shaft 12.
Promote again slide plate 4 and get back to initial position, in getting back to the process of initial position, calibration bar 14.1 from sensor 14.2 tops through out-of-date, sensor 14.2 sends the signal at stop head 2 that presses, slide plate 4 is got back to after initial position, latch 10.2 is inserted in locating hole 10.11, is slide plate 4 and supporting seat 3 location, changes brake block 19.
When brake block 19 models that replace with are different, to adjust adjusting bolt 16, thereby adjust the stroke of slide plate 4, replacing simultaneously to the back shaft 12 mating, like this, just goes for brake block 19 riveted joints of Multiple Type with brake block 19.
Claims (6)
1. aircraft brake sheet riveting machine, comprise frame (1) and the head that presses (2), it is characterized in that: described frame (1) is provided with supporting seat (3), described supporting seat (3) is provided with slide plate (4), between described slide plate (4) and described supporting seat (3), is provided with slide rail (5); Described slide plate (4) middle part is provided with rotating shaft (6), and described rotating shaft (6) is rotationally connected with slide plate (4), carries index dial (7) and positioning disk (8) in described rotating shaft (5); Described positioning disk (8) is positioned at described index dial (7) top, and described index dial (7) is connected with described positioning disk (8), and described positioning disk (8) is connected with described rotating shaft (6); Described slide plate (4) one end is provided with cylinder (9), and the other end is provided with slide plate limit assembly (10); The output of described cylinder (9) is connected with calibration piece (11), and described calibration piece (11) can engage with described index dial (7); Described frame (1) is provided with column (18), described in the top that head (2) is positioned at described positioning disk (8) that presses be connected with described column (18); The upper uniform a plurality of dismountable back shafts (12) of described index dial (7).
2. aircraft brake sheet riveting machine according to claim 1, is characterized in that: described slide plate limit assembly (10) comprise be positioned at described supporting seat (3) end face positioning seat (10.1), be located at the latch (10.2) on slide plate (4); Described positioning seat (10.1) is provided with locating hole (10.11), and described latch (10.2) can engage with described locating hole (10.11) through described slide plate (4).
3. aircraft brake sheet riveting machine according to claim 1, is characterized in that: described positioning disk (8) is provided with dismountable compression plate (13).
4. aircraft brake sheet riveting machine according to claim 1, it is characterized in that: comprise riveted joint switch keeper (14), described riveted joint switch keeper (14) comprises the calibration bar (14.1) that is arranged on slide plate (4) side, is arranged on the sensor (14.2) of supporting seat (3) side.
5. aircraft brake sheet riveting machine according to claim 1, is characterized in that: described supporting seat (3) is provided with block (15), and described block (15) is provided with adjusting bolt (16).
6. aircraft brake sheet riveting machine according to claim 1, it is characterized in that: between described index dial (7) and supporting seat (3), be provided with riveted joint seat (17), described riveted joint seat (17) be fixed on supporting seat (3) upper and be positioned at described in press head (3) under.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320849296.5U CN203737866U (en) | 2013-12-20 | 2013-12-20 | Aircraft brake pad riveting machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320849296.5U CN203737866U (en) | 2013-12-20 | 2013-12-20 | Aircraft brake pad riveting machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203737866U true CN203737866U (en) | 2014-07-30 |
Family
ID=51337730
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320849296.5U Expired - Lifetime CN203737866U (en) | 2013-12-20 | 2013-12-20 | Aircraft brake pad riveting machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203737866U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106311953A (en) * | 2016-08-18 | 2017-01-11 | 上海交通大学 | Automatic aircraft brake pad rotary riveting device |
| CN107442735A (en) * | 2017-07-27 | 2017-12-08 | 天津国际铁工焊接装备有限公司 | A kind of automatic riveting machine |
-
2013
- 2013-12-20 CN CN201320849296.5U patent/CN203737866U/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106311953A (en) * | 2016-08-18 | 2017-01-11 | 上海交通大学 | Automatic aircraft brake pad rotary riveting device |
| CN107442735A (en) * | 2017-07-27 | 2017-12-08 | 天津国际铁工焊接装备有限公司 | A kind of automatic riveting machine |
| CN107442735B (en) * | 2017-07-27 | 2023-09-22 | 天津国际铁工焊接装备有限公司 | Automatic riveter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140730 |
|
| CX01 | Expiry of patent term |