CN102922471B - Device for mounting and decomposing bolt-free connecting baffle plate - Google Patents
Device for mounting and decomposing bolt-free connecting baffle plate Download PDFInfo
- Publication number
- CN102922471B CN102922471B CN201210429535.1A CN201210429535A CN102922471B CN 102922471 B CN102922471 B CN 102922471B CN 201210429535 A CN201210429535 A CN 201210429535A CN 102922471 B CN102922471 B CN 102922471B
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- CN
- China
- Prior art keywords
- upper cover
- baffle plate
- cover plate
- main shaft
- decomposing
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Abstract
The invention provides a device for mounting and decomposing a bolt-free connecting baffle plate, belongs to the technical field of assembling of aircraft engines, and particularly relates to a device for mounting and decomposing a bolt-free connecting baffle plate. The device for mounting and decomposing the bolt-free connecting baffle plate, provided by the invention, can be used for assembling the bolt-free connecting baffle of a high pressure turbine rotor. By adopting the device, the assembling efficiency of the rotor can be improved, and the assembling quality of the baffle plate can be ensured. The device comprises a pedestal; a supporting block and an angular positioning pin are arranged on the pedestal; an upper cover plate is arranged above the pedestal, and is connected with the pedestal by a main shaft; one end of the main shaft is fixedly connected with the pedestal while the other end of the main shaft is connected with a nut by the upper cover plate; a bearing is arranged between the main shaft and the upper cover plate; a tight propping nut is arranged on the main shaft below the upper cover plate; and a baffle plate limiting pin is arranged on the upper cover plate.
Description
Technical field
The invention belongs to aero-engine mounting technology field, particularly relate to a kind of device of installing and decomposing non-bolted joint baffle plate.
Background technology
Further raising along with engine thrust-weight ratio and reliability, a new generation's engine rotor project organization is day by day widely used in modern aeroengine, and the special structure form of rotor non-bolted joint baffle plate is also had higher requirement to rotor assembling and decomposition; The appearance of rotor non-bolted joint baffle plate, to rotor, assembling has proposed new challenge.
For many years, the assembling of aero-turbine rotor baffle plate is to be all connected with wheel disc by screw or bolt; The method that adopts cold charge or hot charging, coordinates baffle plate to be assembled on wheel disc by seam, then screw on screw or bolt.This kind of structure installed easily, but because of screw or bolt quantity more, the difference of the own weight differential of screw or bolt and limiter moment, has affected the balance result of rotor to a certain extent.
Summary of the invention
The problem existing for prior art, the invention provides a kind of installation of assembling and device of decomposition non-bolted joint baffle plate of realizing High Pressure Turbine Rotor non-bolted joint baffle plate.This device can improve the efficiency of assembling of rotor, guarantees the assembly quality of baffle plate.
To achieve these goals, the present invention adopts following technical scheme, and the device of a kind of installation and decomposition non-bolted joint baffle plate, comprises base, is provided with back-up block and angle alignment pin on described base; Above base, be provided with upper cover plate, described upper cover plate is connected with base by main shaft; One end of main shaft is fixedly connected with base, and the other end is connected with nut by upper cover plate, between described main shaft and upper cover plate, is provided with bearing, on the main shaft below upper cover plate, is provided with and holds out against nut, is provided with baffle limiting pin on described upper cover plate.
For the ease of rotary upper cover plate, on one end of described upper cover plate, be provided with handle.
For the ease of rotary upper cover plate, on the other end of described upper cover plate, be provided with the spanner seat with spanner installing hole.
Described main shaft is fixedly connected with base through screws.
For the ease of observing, on described upper cover plate, be provided with observation window.
On described base, be provided with set bolt.
Beneficial effect of the present invention:
1, the present invention can realize assembling and the decomposition of High Pressure Turbine Rotor non-bolted joint baffle plate, and this device can improve the efficiency of assembling of rotor, guarantees the assembly quality of baffle plate, prevents from affecting because of faulty operation the surface quality of baffle plate and the turbine disk;
2, highly versatile of the present invention, the scope of application is wider, is convenient to promote.
Accompanying drawing explanation
Fig. 1 is installation of the present invention and the structural representation that decomposes the device of non-bolted joint baffle plate;
Fig. 2 is that the A of Fig. 1 is to view;
Fig. 3 is the use state diagram of the device of installation of the present invention and decomposition non-bolted joint baffle plate;
In figure, 1-back-up block, 2-base, 3-screw, 4-main shaft, 5-set bolt, 6-angle alignment pin, 7-baffle limiting pin, 8-spanner seat, 9-hold out against nut, 10-bearing, 11-nut, 12-upper cover plate, 13-handle, 14-spanner installing hole, 15-observation window, 16-baffle plate, 17-turbine disk.
The specific embodiment
Below in conjunction with the drawings and specific embodiments, the present invention is described in further detail.
As shown in FIG. 1 to 3, a kind of device of installing and decomposing non-bolted joint baffle plate, comprises base 2, is provided with back-up block 1 and angle alignment pin 6 on described base 2; Above base 2, be provided with upper cover plate 12, described upper cover plate 12 is connected with base 2 by main shaft 4; One end of main shaft 4 is fixedly connected with by screw 3 with base 2, and the other end is connected with nut 11 by upper cover plate 12, between described main shaft 4 and upper cover plate 12, is provided with bearing 10, on the main shaft 4 below upper cover plate 12, is provided with and holds out against nut 9; On described base 2, be provided with set bolt 5, on described upper cover plate 12, be provided with baffle limiting pin 7.
For the ease of rotary upper cover plate 12, on one end of described upper cover plate 12, be provided with handle 13; On the other end of described upper cover plate 12, be provided with the spanner seat 8 with spanner installing hole 14.
For the ease of observing, on described upper cover plate 12, be provided with observation window 15.
The turbine disk and the baffle plate of turbine rotor of now take is example, and once mounting of the present invention and decomposable process are described:
Described baffle plate 16 is thin-wall annular part, on the mounting edge of core wheel position, there are 9 place's lugs, and on each lug, are all processed with the hole of a Ф 3.2mm, be used for installing balancing weight and latch, to reach the requirement of radial stop and adjustment amount of unbalance, it is the baffle arrangement of non-bolted joint.
The turbine disk 17 of described turbine rotor coordinates with baffle plate 16, has 9 place's hook grooves in turbine card, and wherein 9 place's hook grooves coordinate with 9 lugs of baffle plate 16, and baffle plate 16 is carried out to axial location; After 9 place's hook grooves align with 9 place's lug end faces of baffle plate 16, fixture block is installed, baffle plate 16 is carried out to circumferential stop, and with latch to fixture block stop.Because baffle plate 16 and the turbine disk 17 axially and radially all exist a certain amount of interference, its assemble sequence is first baffle plate 16 to be applied to axial compressive force, then it is rotated, the lug of baffle plate 16 is packed in the hook groove of the turbine disk 17, make the end face alignment of lug and hook groove, then pack spacer pin into, prevent mutual rotation.
The present invention selects a wide narrow endless belt of the lower mounting edge 1mm of baffle plate 16, and as the seal face of frock, the axial stroke of frock is exactly the deflection of baffle plate 16, than being easier to, controls.
During installation, first, the turbine disk of turbine rotor 17 is placed on the back-up block 1 of base 2 above upward, and will in the hole of the 6 insertion turbine disk 17 rear mounting edges of two angle alignment pins on base 2, carries out angle location, prevent that the turbine disk 17 from rotating.By the nut 11 on rotary main shaft 4, press cover plate 12 downwards, make 12 pairs of baffle plates 16 of upper cover plate apply axial pressure, make baffle plate 16 produce axial elasticity distortion, the mounting edge of upper cover plate 12 is pressed onto on the lug of 16 times mounting edges of baffle plate, and by 3 baffle limiting pins 7, is close to lug one side of 16 times mounting edges of baffle plate; The strength that can bear is like this larger, also can not cause damage to baffle plate 16.Then, by N in Fig. 3, to the nut 11 on (clockwise) rotary main shaft 4, by M in figure, to (downwards), press cover plate 12, thereby drive baffle plate 16 to produce axial elasticities distortion; Meanwhile, by the position of the 16 times mounting edge lugs of observation window 15 viewing hood on upper cover plate 12 and the hook groove on the turbine disk 17, check and whether be seated; When baffle plate 16 can rotate, the interior assembly wrench of spanner installing hole 14 at spanner seat 8, utilize spanner and handle 13 rotary upper cover plates 12, drive baffle plate 16 to rotate, 16 times mounting edge lugs of baffle plate are entered in the hook groove on the turbine disk 17, until the limit pin hole of 16 times mounting edge lugs of baffle plate and the turbine disk 17 are risen to the bait, the limit pin hole of groove aligns, even the alignment of the end face of lug and hook groove; Press in Fig. 3 N rotating nut 11 round about, take off upper cover plate 12, mounting limit pin in limit pin hole, installation.
During decomposition, only need to press direction rotation upper cover plate 12 contrary while installing.
When rotary resistance is large especially, can base 2 be installed on square chest by two set bolts 5, in case locking apparatus unitary rotation.
Claims (6)
1. install and decompose a device for non-bolted joint baffle plate, it is characterized in that comprising base, on described base, be provided with back-up block and angle alignment pin; Above base, be provided with upper cover plate, described upper cover plate is connected with base by main shaft; One end of main shaft is fixedly connected with base, and the other end, through upper cover plate, is then connected with nut, between described main shaft and upper cover plate, is provided with bearing, on the main shaft below upper cover plate, is provided with and holds out against nut, is provided with baffle limiting pin on described upper cover plate.
2. a kind of device of installing and decomposing non-bolted joint baffle plate according to claim 1, is characterized in that being provided with handle on one end of described upper cover plate.
3. a kind of device of installing and decomposing non-bolted joint baffle plate according to claim 2, is characterized in that being provided with the spanner seat with spanner installing hole on the other end of described upper cover plate.
4. a kind of device of installing and decomposing non-bolted joint baffle plate according to claim 1, is characterized in that described main shaft is fixedly connected with base through screws.
5. a kind of device of installing and decomposing non-bolted joint baffle plate according to claim 1, is characterized in that being provided with observation window on described upper cover plate.
6. a kind of device of installing and decomposing non-bolted joint baffle plate according to claim 1, is characterized in that being provided with set bolt on described base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210429535.1A CN102922471B (en) | 2012-10-31 | 2012-10-31 | Device for mounting and decomposing bolt-free connecting baffle plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210429535.1A CN102922471B (en) | 2012-10-31 | 2012-10-31 | Device for mounting and decomposing bolt-free connecting baffle plate |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102922471A CN102922471A (en) | 2013-02-13 |
| CN102922471B true CN102922471B (en) | 2014-11-19 |
Family
ID=47637471
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210429535.1A Expired - Fee Related CN102922471B (en) | 2012-10-31 | 2012-10-31 | Device for mounting and decomposing bolt-free connecting baffle plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102922471B (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104259718A (en) * | 2014-09-26 | 2015-01-07 | 徐州华恒机器人系统有限公司 | High-load-bearing easily detached pressing plate mechanism |
| CN105328627B (en) * | 2015-12-02 | 2017-04-12 | 中国南方航空工业(集团)有限公司 | Tool for replacing bolts at external field |
| CN105500269A (en) * | 2015-12-10 | 2016-04-20 | 广西玉柴机器股份有限公司 | Pressurizer assembling and conveying device |
| CN106392957A (en) * | 2016-12-21 | 2017-02-15 | 中国南方航空工业(集团)有限公司 | Assembly clamp and assembly method for front baffle plate of gas turbine disc |
| CN107971727B (en) * | 2017-11-23 | 2019-07-05 | 中国航发沈阳黎明航空发动机有限责任公司 | A kind of installation method of snap ring-type connection baffle |
| CN108098673A (en) * | 2017-12-11 | 2018-06-01 | 中国航发沈阳发动机研究所 | Low-pressure turbine blade baffle assembling and disassembling device |
| CN113798401B (en) * | 2021-09-09 | 2023-10-20 | 中国航发南方工业有限公司 | Turbine rotor locking plate assembly device and use method thereof |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4890981A (en) * | 1988-12-30 | 1990-01-02 | General Electric Company | Boltless rotor blade retainer |
| JPH06277964A (en) * | 1993-03-31 | 1994-10-04 | Ishikawajima Harima Heavy Ind Co Ltd | Assembling and disassembling device for boltless turbine rotor |
| CN102554825A (en) * | 2011-12-23 | 2012-07-11 | 四川亚美动力技术有限公司 | Turbine blade assembling insurance clamp and method for performing impeller clamping thereof |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7765658B2 (en) * | 2005-10-17 | 2010-08-03 | Pratt & Whitney Canada Corp. | Blade tip grinding tooling |
| US8683670B2 (en) * | 2010-12-20 | 2014-04-01 | Turbine Tooling Solutions Llc | Method for partial disassembly of a bypass turbofan engine |
-
2012
- 2012-10-31 CN CN201210429535.1A patent/CN102922471B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4890981A (en) * | 1988-12-30 | 1990-01-02 | General Electric Company | Boltless rotor blade retainer |
| JPH06277964A (en) * | 1993-03-31 | 1994-10-04 | Ishikawajima Harima Heavy Ind Co Ltd | Assembling and disassembling device for boltless turbine rotor |
| CN102554825A (en) * | 2011-12-23 | 2012-07-11 | 四川亚美动力技术有限公司 | Turbine blade assembling insurance clamp and method for performing impeller clamping thereof |
Non-Patent Citations (2)
| Title |
|---|
| 涡轮盘与挡板的无螺栓连接结构;马健等;《燃气涡轮试验与研究》;20080515;第21卷(第02期);24-26 * |
| 马健等.涡轮盘与挡板的无螺栓连接结构.《燃气涡轮试验与研究》.2008,第21卷(第02期),24-26. * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102922471A (en) | 2013-02-13 |
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Granted publication date: 20141119 Termination date: 20171031 |
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| CF01 | Termination of patent right due to non-payment of annual fee |