CN201713287U - Gas turbine rotor hoisting device - Google Patents

Gas turbine rotor hoisting device Download PDF

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Publication number
CN201713287U
CN201713287U CN2010201614258U CN201020161425U CN201713287U CN 201713287 U CN201713287 U CN 201713287U CN 2010201614258 U CN2010201614258 U CN 2010201614258U CN 201020161425 U CN201020161425 U CN 201020161425U CN 201713287 U CN201713287 U CN 201713287U
Authority
CN
China
Prior art keywords
hoisting
plate
lifting
gas turbine
turbine rotor
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 - Fee Related
Application number
CN2010201614258U
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Chinese (zh)
Inventor
于海
鲁廷涛
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.)
Siemens Ltd China
Original Assignee
Shanghai Electric Power Generation Equipment 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 Shanghai Electric Power Generation Equipment Co Ltd filed Critical Shanghai Electric Power Generation Equipment Co Ltd
Priority to CN2010201614258U priority Critical patent/CN201713287U/en
Application granted granted Critical
Publication of CN201713287U publication Critical patent/CN201713287U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a gas turbine rotor hoisting device, which comprises a horizontal beam and a hoister. A motor is arranged on the horizontal beam and connected with a screw rod via a coupler, a nut is arranged on the screw rod, the hoister is fixed onto the nut, hoisting locking mechanisms are respectively arranged at two ends of the horizontal beam, each hoisting locking mechanism includes a hoisting plate, a projecting portion is formed on the front lateral surface of the hoisting plate, the rear lateral surface of the hoisting plate is connected with a lock plate in a sliding manner, and the lock plate can vertically slide along the hoisting plate. The hoisting has the advantages that (1)the hoisting device abandons the manner of hoisting at a shaft neck position and does not damage a rotor, (2) the arranged lock plate firmly fixes the stator at a hoisting position, and a rigid fixing mode is safer than before, (3) the hoisting device directly performs hoisting on a wheel plate of the rotor without disassembling bearing and the process is quicker, and (4) a sliding component can slide along the beam and adjust hoisting gravity center, and the gas turbine rotor hoisting device is suitable for hoisting rotors with different gravity centers and wide in applicable range.

Description

The gas turbine rotor lifting appliance
Technical field
The utility model relates to a kind of lifting appliance, particularly a kind ofly lifts by crane the lifting appliance that gas turbine rotor is used.
Background technology
Combustion engine power station is to be the simple cycle or the combined-cycle power plant of original power with the combustion machine, and it takes up an area of less, water is economized, the power supplying efficiency height, and combustion engine power station is increasing in China at present.Gas turbine rotor is the vitals that the combustion machine is realized transformation of energy, horsepower output, and its weight generally reaches 120 tons; Length is near 10 meters; Maximum gauge reaches 3.2 meters; Above the rotor more than 1,000 air compressor and turbine blade are installed simultaneously, therefore firing machine rotor is accurate, expensive, the big parts of heavy weight.Employed cable wire is used for the lifting of turbine rotor substantially in present China power station equipment, be characterized in that rope directly lifts by crane at the axle journal place, the characteristics of this lifting appliance are direct liftings, structure is very simple, but be easy to damage axle journal, should take away bearing shell earlier when lifting by crane simultaneously, the lifting cycle is long.It is meticulous that gas turbine component requires, can not damage, and requirement can open fast, stop, and fast service, maintenance, these characteristics have determined the cable wire rotor lifting mode of steam turbine to fail to satisfy requirements.Because industry gas turbine is at the early-stage at home, also there is not special rotor lifting device at present at automotive gas turbine, design a kind of gas turbine rotor lifting appliance, must meet the following conditions;
(1) lifting does not damage rotor, owing to use cable wire at the rotor journal place lifting precision machined axle journal of damage easily, so just requiring need be in the not high relatively place lifting of rotor requirement, contacts with the axle journal of sensitivity avoiding.
(2) lifting is safe and reliable, owing to do not adopt rope to surround the mode of rotor lifting, the rotor lifting device must be safe, hang, catch on rotor reliably, guarantees can not take place rotor and drop in the lifting process.
(3) lifting rapidly, but at high speed, lift by crane rotor simply.Specifically, the first, lifting appliance and power station travelling crane hook can be rapidly, be connected easily; The second, lifting appliance and combustion machine rotor can be rapidly, be connected easily; The 3rd, can catch on rotor rapidly before the lifting, the rapid and rotor unhook in lifting back.
(4) applicability is wide, and different rotors has different length, diameter, weight and blade distributes, i.e. center of gravity difference, and the rotor lifting device should be regulated the lifting center, and travelling crane hook and rotor c.g. are positioned on the same vertical line, so that lift by crane different rotors.
The utility model content
At above-mentioned the deficiencies in the prior art, the technical problems to be solved in the utility model provides and a kind ofly lifts by crane fast, flexible operation, gas turbine rotor lifting appliance that reliability is high.
For solving the problems of the technologies described above, the utility model adopts following technical scheme:
A kind of gas turbine rotor lifting appliance, it comprises horizontal gird, plays hanging piece, described horizontal gird is provided with a motor, described motor is connected with a screw rod by a coupler, described screw rod is provided with nut, described hanging piece is fixed on the described nut, the two ends of described horizontal gird respectively are provided with a lifting catch gear, described lifting catch gear comprises a boatswain chair, form a lug boss on the leading flank of described boatswain chair, the trailing flank of described boatswain chair and a jam plate sliding block joint, described jam plate can slide up and down along described boatswain chair.
Preferably, the trailing flank of described boatswain chair is provided with a guide plate and a baffle plate, described guide plate is relative with described baffle plate, form a guide groove between described guide plate and the described baffle plate, described jam plate is positioned at described guide groove, the middle part of a described guide plate and a control stalk is hinged, and an end of described control stalk is connected with described jam plate.
Preferably, described boatswain chair is provided with a counterweight back to a side of described guide plate.
Preferably, the lower end back to described lug boss one side forms an inclined-plane on the jam plate.
Preferably, be provided with bracing frame below the described horizontal gird.
Technique scheme has following beneficial effect: this lifting appliance is respectively offered a lifting groove at air compressor end that fires the machine rotor wheel disc and turbine end earlier before lifting, and offer a depressed part that caves inward on a side of lifting groove, the width of boatswain chair and jam plate addition should be suitable with the width of lifting groove.When lifting, at first boatswain chair is inserted in the lifting groove, and make the lug boss of boatswain chair corresponding with the depressed part of lifting groove, the jam plate that slides downwards then is inserted in the lifting groove jam plate, along with the lug boss of the downward sliding traveler of jam plate inserts in the depressed part of lifting groove, boatswain chair can not be moved by locked again in the time of in jam plate is stuck in the lifting groove fully, can effectively prevent to occur in hoisting process the problem of unhook like this.Can lift by crane after all installing Deng the lifting catch gear on both sides, the position that can play hanging piece by the motor adjustment when lifting makes the lifting position overlap with rotor c.g., can easily adjust to lift by crane the position, reaches the purpose of quick maintenance.In sum, this lifting appliance has following advantage: (1) abandons the mode in the lifting of axle journal place, does not damage rotor; (2) the lifting position has firmly been fixed in the existence of jam plate, and the mode that rigidly fixes is safer than before; (3) directly on rotor disk, lift by crane, need not to dismantle bearing, quicker; (4) slide assemblies can slide along crossbeam, regulates the lifting center of gravity, is fit to the rotor lifting of different centers of gravity, and applicability is wide.
Description of drawings
Fig. 1 is the front view of the utility model embodiment.
Fig. 2 is the birds-eye view of the utility model embodiment.
Fig. 3 is the structural representation of lifting catch gear among the utility model embodiment.
Fig. 4 is boatswain chair and a jam plate bonded assembly structural representation among the utility model embodiment.
Fig. 5 is the structural representation of the utility model embodiment rotor wheel disc lifting groove.
Fig. 6 is boatswain chair among the utility model embodiment, jam plate and lifting groove connection structure scheme drawing.
The specific embodiment
Below in conjunction with accompanying drawing preferred embodiment of the present utility model is described in detail.
As shown in Figure 1, 2, this gas turbine rotor lifting appliance comprises a horizontal gird 1, horizontal gird 1 is provided with a motor 3, motor 3 is connected with an end of a screw rod 7 by a coupler, the other end of screw rod 7 is fixed on the supporting seat 8, screw rod 7 is provided with nut, and nut is with hanging piece 4 captive joints.7 rotations of motor 3 drive screw rods can drive hanging piece 4 and move around along the screw rod direction.The two ends of horizontal gird 1 also respectively are provided with a lifting catch gear 2.The below of horizontal gird 1 also is provided with two bracing frames 5.
Shown in Fig. 3,4, lifting catch gear 2 comprises a boatswain chair 20, form a lug boss 26 on the leading flank of boatswain chair, the trailing flank of boatswain chair is provided with a guide plate 21 and a baffle plate 25, guide plate 21 is relative with baffle plate 25, forms a guide groove 28 between guide plate 21 and the baffle plate 25, is provided with a jam plate 23 in the guide groove 28, jam plate 23 and boatswain chair 20 sliding block joints, jam plate 23 can slide up and down in guide groove 28.The middle part of a guide plate 21 and a control stalk 22 is hinged, and an end of control stalk 22 is connected with jam plate 23, and control stalk 22 is provided with an elongated slot, and jam plate 23 is inserted in this elongated slot by a bearing pin and is connected with control stalk 22.Control stalk 22 just forms a lever like this, can drive jam plate 23 by operation control stalk 22 and move up and down.Side back to guide plate 21 on the boatswain chair 20 is provided with a counterweight 24.The effect of counterweight 24 is when not using this lifting appliance at ordinary times, and the weight of balance guide plate 21 and control stalk 22 guarantees that boatswain chair does not tilt.Side lower end back to lug boss 26 on jam plate 23 forms an inclined-plane 27.
As shown in Figure 5, this lifting appliance is respectively offered a lifting groove 61 at air compressor end that fires machine rotor wheel disc 6 and turbine end earlier before lifting, and offers a depressed part that caves inward 62 on a side of lifting groove 61.The width of lifting groove 61 can change accordingly according to the position that the lifting groove is offered, can be greater than the width of turbine end lifting groove as the width of air compressor end lifting groove.The distances of two liftings between the catch gear 2 should equate with the distances between two lifting grooves, and each lift by crane the width of boatswain chair and jam plate addition on catch gear should be suitable with the width of corresponding lifting groove.
As shown in Figure 6, when lifting, at first boatswain chair 20 is inserted in the lifting groove, and make the lug boss 26 of boatswain chair 20 corresponding with depressed part 62 positions of lifting groove, then by control stalk 22 downward slip jam plates 23, jam plate 23 is inserted in the lifting groove, and the inclined-plane 27 on the jam plate 23 can make things convenient for jam plate 23 to be inserted in this lifting groove.Along with jam plate 23 to lower slider, the lug boss 26 of boatswain chair 20 inserts in the depressed part 62 of lifting groove, in the time of in jam plate 23 is stuck in the lifting groove fully, boatswain chair 20 can not be moved by locked again, at this moment can control stalk 22 afterbodys and guide plate 21 be connected together by chain, to prevent that jam plate 23 from shifting out the lifting groove, can effectively prevent from hoisting process, to occur the problem that boatswain chair breaks off relations like this.Can lift by crane after being installed in the lifting groove Deng the lifting catch gear on both sides.
Again as shown in Figure 2, to play hanging piece 4 during lifting is connected with driving, can make driving apply a little pulling force to one side rotor and leave bearing, can judge which limit is the lifting position whether overlap and be partial to rotor c.g., rotate by motor 3 drive screws 7 then, driven hanging piece 4 and moved to the appropriate location, the lifting position is overlapped with rotor c.g., as seen adopt this lifting appliance very convenient adjustment to lift by crane the position, reach the purpose of quick maintenance.This lifting appliance can be placed on two bracing frames 5 after lifting is finished and support.
In sum, this lifting appliance has following advantage:
(1) abandons mode, do not damage rotor in axle journal place lifting;
(2) the lifting position has firmly been fixed in the existence of jam plate, and the mode that rigidly fixes is safer than before;
(3) directly on rotor disk, lift by crane, need not to dismantle bearing, quicker;
(4) slide assemblies can slide along crossbeam, regulates the lifting center of gravity, is fit to the rotor lifting of different centers of gravity, and applicability is wide.
More than gas turbine rotor lifting appliance that the utility model embodiment is provided be described in detail; for one of ordinary skill in the art; thought according to the utility model embodiment; part in specific embodiments and applications all can change; in sum; this description should not be construed as restriction of the present utility model, and all any changes of being made according to the utility model design philosophy are all within protection domain of the present utility model.

Claims (5)

1. gas turbine rotor lifting appliance, it is characterized in that: it comprises horizontal gird, plays hanging piece, described horizontal gird is provided with a motor, described motor is connected with a screw rod by a coupler, described screw rod is provided with nut, described hanging piece is fixed on the described nut, the two ends of described horizontal gird respectively are provided with a lifting catch gear, described lifting catch gear comprises a boatswain chair, form a lug boss on the leading flank of described boatswain chair, the trailing flank of described boatswain chair and a jam plate sliding block joint, described jam plate can slide up and down along described boatswain chair.
2. gas turbine rotor lifting appliance according to claim 1, it is characterized in that: the trailing flank of described boatswain chair is provided with a guide plate and a baffle plate, described guide plate is relative with described baffle plate, form a guide groove between described guide plate and the described baffle plate, described jam plate is positioned at described guide groove, the middle part of a described guide plate and a control stalk is hinged, and an end of described control stalk is connected with described jam plate.
3. gas turbine rotor lifting appliance according to claim 2 is characterized in that: described boatswain chair is provided with a counterweight back to a side of described guide plate.
4. gas turbine rotor lifting appliance according to claim 1 is characterized in that: the lower end back to described lug boss one side on the jam plate forms an inclined-plane.
5. gas turbine rotor lifting appliance according to claim 1 is characterized in that: described horizontal gird below is provided with bracing frame.
CN2010201614258U 2010-04-15 2010-04-15 Gas turbine rotor hoisting device Expired - Fee Related CN201713287U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010201614258U CN201713287U (en) 2010-04-15 2010-04-15 Gas turbine rotor hoisting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010201614258U CN201713287U (en) 2010-04-15 2010-04-15 Gas turbine rotor hoisting device

Publications (1)

Publication Number Publication Date
CN201713287U true CN201713287U (en) 2011-01-19

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010201614258U Expired - Fee Related CN201713287U (en) 2010-04-15 2010-04-15 Gas turbine rotor hoisting device

Country Status (1)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102900541A (en) * 2011-07-27 2013-01-30 通用电气公司 System and method for supporting a shaft inside a turbine
CN102923617A (en) * 2011-08-12 2013-02-13 北汽福田汽车股份有限公司 Lifting device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102900541A (en) * 2011-07-27 2013-01-30 通用电气公司 System and method for supporting a shaft inside a turbine
CN102900541B (en) * 2011-07-27 2016-10-05 通用电气公司 For the system and method in turbine interior support shaft
CN102923617A (en) * 2011-08-12 2013-02-13 北汽福田汽车股份有限公司 Lifting device
CN102923617B (en) * 2011-08-12 2015-07-08 北汽福田汽车股份有限公司 Lifting device

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: SIMENS CO LTD (CHINA)

Free format text: FORMER OWNER: SHANGHAI ELECTRIC STATION EQUIPMENT CO., LTD.

Effective date: 20130124

C41 Transfer of patent application or patent right or utility model
C53 Correction of patent for invention or patent application
CB03 Change of inventor or designer information

Inventor after: Becker Burckhard

Inventor before: Yu Hai

Inventor before: Lu Tingtao

COR Change of bibliographic data

Free format text: CORRECT: INVENTOR; FROM: YU HAI LU TINGTAO TO: BECKER B.

Free format text: CORRECT: ADDRESS; FROM: 200240 MINHANG, SHANGHAI TO: 100102 CHAOYANG, BEIJING

TR01 Transfer of patent right

Effective date of registration: 20130124

Address after: 100102 Beijing, Wangjing, Central South Road, No. 7, No.

Patentee after: Simens Co., Ltd. (China)

Address before: 200240 Jiangchuan Road, Shanghai, No. 333, No.

Patentee before: Shanghai Electric Station Equipment Co., Ltd.

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110119

Termination date: 20180415

CF01 Termination of patent right due to non-payment of annual fee