CN106429827A - Rotor overturning and hoisting device - Google Patents

Rotor overturning and hoisting device Download PDF

Info

Publication number
CN106429827A
CN106429827A CN201611046580.3A CN201611046580A CN106429827A CN 106429827 A CN106429827 A CN 106429827A CN 201611046580 A CN201611046580 A CN 201611046580A CN 106429827 A CN106429827 A CN 106429827A
Authority
CN
China
Prior art keywords
rotor
hoisting
link plate
shackle
pivot pin
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.)
Pending
Application number
CN201611046580.3A
Other languages
Chinese (zh)
Inventor
余雪
可成河
巩孟祥
陈大丽
吕英俊
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.)
Shenyang Liming Aero Engine Group Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group 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 Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201611046580.3A priority Critical patent/CN106429827A/en
Publication of CN106429827A publication Critical patent/CN106429827A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66CCRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C1/00Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles
    • B66C1/10Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means
    • B66C1/62Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means comprising article-engaging members of a shape complementary to that of the articles to be handled
    • B66C1/66Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means comprising article-engaging members of a shape complementary to that of the articles to be handled for engaging holes, recesses, or abutments on articles specially provided for facilitating handling thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66CCRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C1/00Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles
    • B66C1/10Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means
    • B66C1/12Slings comprising chains, wires, ropes, or bands; Nets
    • B66C1/125Chain-type slings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Load-Engaging Elements For Cranes (AREA)

Abstract

The invention discloses a rotor overturning and hoisting device. The rotor overturning and hoisting device is composed of a hoisting beam (1), a supporting frame (2), clamping rings (3), plugs (4), suspension plates (6), a hoisting ring (7), first shaft pins, second shaft pins (9), nuts, slotted nuts, cotters, hoisting hooks (15), shackles (16) and steel wire ropes (17), wherein a labyrinth disc of a turbine disc of a rotor (18) to be hoisted is provided with spigots, the two clamping rings (3) are fixedly connected to the outer sides of the spigots, and the clamping rings (3) are fixedly connected with one end of the supporting frame (2). The rotor overturning and hoisting device is a hoisting device which can overturn during rotation, balancing and blade tip machining of rotors with or without rear journals, and the hoisting reliability and quality of an engine during assembling, balancing and blade tip machining are ensured.

Description

A kind of rotor overturns hanging apparatus
Technical field
The present invention relates to the structure design of hanging apparatus and applied technical field, specifically provide a kind of upset lifting of rotor Device.
Background technology
As the thrust-weight ratio of electromotor and reliability are improved further, engine rotor design structure of new generation is in modern boat Increasingly it is widely used in empty electromotor, the rotor structure of special construction is also carried to rotor assembling, processing, balance and decomposition Higher requirement is gone out.
There are two states in this construction rotor during assembling and processing blade tip, that is, carry rear shaft neck and without rear shaft neck two The state of kind.In Special lifting device design process is carried out, emphasis consideration band rear shaft neck and without turning under rear shaft neck two states Turn space structure, fixing of clamping etc..
People are highly desirable to obtain a kind of excellent rotor upset hanging apparatus of technique effect.
Content of the invention
It is an object of the invention to provide a kind of excellent rotor upset hanging apparatus of technique effect.Solve certain aeroplane engine Lifting problem of the machine rotor in assembling, blade tip processing, balance and catabolic process, the rotor lifting of special construction is converted into one As structure rotor lifting, it is ensured that the stability in rotor hoisting process.
Institute's rotor upset hanging apparatus constitute as follows:Hanging beam 1, bracing frame 2, snap ring 3, latch 4, link plate 6, suspension ring 7, first Pivot pin, the second pivot pin 9, nut, slotted nut, split pin, suspension hook 15, shackle 16, steel wire rope 17;Wherein, hoisting rotor 18 is treated Seam is provided with the labyrinth of the turbine disk, two snap rings 3 are fixedly connected on the outside of seam, snap ring 3 is solid with one end of bracing frame 2 Fixed connection, the other end of bracing frame 2 is connected with the lower end of link plate 6 by latch 4, nut and the second pivot pin 9, the upper end of link plate 6 Be enclosed within suspension hook 15, the upper end of suspension hook 15 is connected with shackle 16, steel wire rope 17, shackle 16 by the first pivot pin, slotted nut and Split pin is connected with suspension ring 7, and hanging beam 1 is located at 7 lower section of suspension ring, and the two ends of hanging beam 1 support shackle 16 and steel wire rope 17.
Support frame as described above 2 is provided with spring washer with 6 junction of link plate.
Seam is provided with the labyrinth for treating 18 turbine disk of hoisting rotor, may be designed to two halves Snap ring structure to fix high pressure The turbine disk, this seam can bear axial force and radial force, but as seam size is less, need by entering to whole stressing conditions Row is calculated, and determines the size of snap ring.
Snap ring 3 needs to be connected with bracing frame 2, and bracing frame 2 is carried out by latch 4, nut and the second pivot pin 9 with link plate 6 again Connection, bearing pin 9 can achieve the upset of this hanging apparatus, carry rear shaft neck and without rear due to considering that rotor is present in assembling process The two states of axle journal, are required to be overturn under two states, and therefore carrying out Strength co-mputation and space structure needs when calculating Two states to be considered.
It is as follows that the rotor overturns the specifically used process of hanging apparatus:Rotor 18 is placed upright position, i.e.,:Place special In transport vehicle;Two halves snap ring 3 is fixed on the seam of rotor 18;Solid with latch 4 and the second pivot pin 9 with bracing frame and link plate 6 Fixed, pad and elastic washer is put, uses nut screwing clamping;Suspension hook 15 is enclosed within link plate 6, shackle 16 is connected with steel wire rope 17, will Steel wire rope 17 is connected with hanging beam 1, and hanging beam 1 is connected with suspension ring 7 by the first pivot pin, is loaded onto packing ring, split pin 14, is tightened fluting Nut, lock opening pin 14;Crane is connected with suspension ring 7, rotor of slowly slinging, is carrying out rotor balancing and on horizontal lathe When processing to blade tip, 90 ° of upsets are carried out by link plate 6 to rotor.
Rotor upset hanging apparatus be disclosure satisfy that rotor banding rear shaft neck and without rear shaft neck in rotor, balance, add Hanging apparatus are may be reversed during work blade tip, it is ensured that lifting reliability when engine assembly, balance, processing blade tip and quality.
Description of the drawings
Below in conjunction with the accompanying drawings and embodiment the present invention is further detailed explanation:
Fig. 1 overturns hanging apparatus structural representation for rotor;
Fig. 2 is sectional view at A A in Fig. 1.
Specific embodiment
Embodiment 1
Institute's rotor upset hanging apparatus constitute as follows:Hanging beam 1, bracing frame 2, snap ring 3, latch 4, link plate 6, suspension ring 7, first Pivot pin, the second pivot pin 9, nut, slotted nut, split pin, suspension hook 15, shackle 16, steel wire rope 17;Wherein, hoisting rotor 18 is treated Seam is provided with the labyrinth of the turbine disk, two snap rings 3 are fixedly connected on the outside of seam, snap ring 3 is solid with one end of bracing frame 2 Fixed connection, the other end of bracing frame 2 is connected with the lower end of link plate 6 by latch 4, nut and the second pivot pin 9, the upper end of link plate 6 Be enclosed within suspension hook 15, the upper end of suspension hook 15 is connected with shackle 16, steel wire rope 17, shackle 16 by the first pivot pin, slotted nut and Split pin is connected with suspension ring 7, and hanging beam 1 is located at 7 lower section of suspension ring, and the two ends of hanging beam 1 support shackle 16 and steel wire rope 17.
Support frame as described above 2 is provided with spring washer with 6 junction of link plate.
Seam is provided with the labyrinth for treating 18 turbine disk of hoisting rotor, may be designed to two halves Snap ring structure to fix high pressure The turbine disk, this seam can bear axial force and radial force, but as seam size is less, need by entering to whole stressing conditions Row is calculated, and determines the size of snap ring.
Snap ring 3 needs to be connected with bracing frame 2, and bracing frame 2 is carried out by latch 4, nut and the second pivot pin 9 with link plate 6 again Connection, bearing pin 9 can achieve the upset of this hanging apparatus, carry rear shaft neck and without rear due to considering that rotor is present in assembling process The two states of axle journal, are required to be overturn under two states, and therefore carrying out Strength co-mputation and space structure needs when calculating Two states to be considered.
It is as follows that the rotor overturns the specifically used process of hanging apparatus:Rotor 18 is placed upright position, i.e.,:Place special In transport vehicle;Two halves snap ring 3 is fixed on the seam of rotor 18;Solid with latch 4 and the second pivot pin 9 with bracing frame and link plate 6 Fixed, pad and elastic washer is put, uses nut screwing clamping;Suspension hook 15 is enclosed within link plate 6, shackle 16 is connected with steel wire rope 17, will Steel wire rope 17 is connected with hanging beam 1, and hanging beam 1 is connected with suspension ring 7 by the first pivot pin, is loaded onto packing ring, split pin 14, is tightened fluting Nut, lock opening pin 14;Crane is connected with suspension ring 7, rotor of slowly slinging, is carrying out rotor balancing and on horizontal lathe When processing to blade tip, 90 ° of upsets are carried out by link plate 6 to rotor.
Rotor upset hanging apparatus be disclosure satisfy that rotor banding rear shaft neck and without rear shaft neck in rotor, balance, add Hanging apparatus are may be reversed during work blade tip, it is ensured that lifting reliability when engine assembly, balance, processing blade tip and quality.

Claims (2)

1. a kind of rotor overturns hanging apparatus, it is characterised in that:Institute's rotor upset hanging apparatus constitute as follows:Hanging beam (1), support Frame (2), snap ring (3), latch (4), link plate (6), suspension ring (7), the first pivot pin, the second pivot pin (9), nut, slotted nut, opening Pin, suspension hook (15), shackle (16), steel wire rope (17);Wherein, only it is provided with the labyrinth for treating hoisting rotor (18) turbine disk Mouthful, two snap rings (3) are fixedly connected on the outside of seam, and snap ring (3) is fixedly connected with one end of bracing frame (2), bracing frame (2) The other end is connected with the lower end of link plate (6) by latch (4), nut and the second pivot pin (9), and the upper end of link plate (6) is enclosed within suspension hook (15) on, the upper end of suspension hook (15) is connected with shackle (16), steel wire rope (17), and shackle (16) passes through the first pivot pin, slotted nut It is connected with suspension ring (7) with split pin, hanging beam (1) is located at below suspension ring (7), the two ends of hanging beam (1) support shackle (16) and steel wire Rope (17).
2. according to rotor described in claim 1, hanging apparatus are overturn, it is characterised in that:Support frame as described above (2) is connected with link plate (6) Place is provided with spring washer.
CN201611046580.3A 2016-11-23 2016-11-23 Rotor overturning and hoisting device Pending CN106429827A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611046580.3A CN106429827A (en) 2016-11-23 2016-11-23 Rotor overturning and hoisting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611046580.3A CN106429827A (en) 2016-11-23 2016-11-23 Rotor overturning and hoisting device

Publications (1)

Publication Number Publication Date
CN106429827A true CN106429827A (en) 2017-02-22

Family

ID=58218405

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611046580.3A Pending CN106429827A (en) 2016-11-23 2016-11-23 Rotor overturning and hoisting device

Country Status (1)

Country Link
CN (1) CN106429827A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108408573A (en) * 2018-05-11 2018-08-17 广州南沙珠江啤酒有限公司 A kind of device and its application process vertically transported for large-scale plate
CN109279490A (en) * 2018-11-28 2019-01-29 嘉兴金鹏工具有限公司 A kind of Novel crane balance sling
CN109516362A (en) * 2018-11-30 2019-03-26 中国航发沈阳黎明航空发动机有限责任公司 The suspender and its application method of a kind of while hoisting rotor and stator component
CN111943014A (en) * 2020-06-30 2020-11-17 中国航发南方工业有限公司 Hanging device of aircraft engine starter and assembly method thereof
CN112177692A (en) * 2019-07-03 2021-01-05 中国航发商用航空发动机有限责任公司 Assembling tool and assembling method for low-pressure turbine rotor

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS541701A (en) * 1977-06-07 1979-01-08 Hitachi Ltd Inversion of turbne casing
EP0353545A2 (en) * 1988-08-03 1990-02-07 Siemens Aktiengesellschaft Transport and turning device for the core components of a nuclear reactor
CN201634306U (en) * 2010-02-10 2010-11-17 中国船舶重工集团公司第七一三研究所 Overturning lifting device
CN202337645U (en) * 2011-11-15 2012-07-18 国营红阳机械厂 Device for overturning large-tonnage heavy object
CN202687744U (en) * 2012-06-29 2013-01-23 鹰普机械(宜兴)有限公司 Lifting appliance with turning function
CN203513077U (en) * 2013-09-22 2014-04-02 西安航天化学动力厂 Lifting turnover tool for nonmetallic combustor
CN204643551U (en) * 2015-05-14 2015-09-16 内蒙古包钢钢联股份有限公司 Wheel is to reversal hanger

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS541701A (en) * 1977-06-07 1979-01-08 Hitachi Ltd Inversion of turbne casing
EP0353545A2 (en) * 1988-08-03 1990-02-07 Siemens Aktiengesellschaft Transport and turning device for the core components of a nuclear reactor
CN201634306U (en) * 2010-02-10 2010-11-17 中国船舶重工集团公司第七一三研究所 Overturning lifting device
CN202337645U (en) * 2011-11-15 2012-07-18 国营红阳机械厂 Device for overturning large-tonnage heavy object
CN202687744U (en) * 2012-06-29 2013-01-23 鹰普机械(宜兴)有限公司 Lifting appliance with turning function
CN203513077U (en) * 2013-09-22 2014-04-02 西安航天化学动力厂 Lifting turnover tool for nonmetallic combustor
CN204643551U (en) * 2015-05-14 2015-09-16 内蒙古包钢钢联股份有限公司 Wheel is to reversal hanger

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108408573A (en) * 2018-05-11 2018-08-17 广州南沙珠江啤酒有限公司 A kind of device and its application process vertically transported for large-scale plate
CN108408573B (en) * 2018-05-11 2024-05-07 广州南沙珠江啤酒有限公司 Device for vertically conveying large plate blocks and application method thereof
CN109279490A (en) * 2018-11-28 2019-01-29 嘉兴金鹏工具有限公司 A kind of Novel crane balance sling
CN109516362A (en) * 2018-11-30 2019-03-26 中国航发沈阳黎明航空发动机有限责任公司 The suspender and its application method of a kind of while hoisting rotor and stator component
CN109516362B (en) * 2018-11-30 2019-10-22 中国航发沈阳黎明航空发动机有限责任公司 The suspender and its application method of a kind of while hoisting rotor and stator component
CN112177692A (en) * 2019-07-03 2021-01-05 中国航发商用航空发动机有限责任公司 Assembling tool and assembling method for low-pressure turbine rotor
CN112177692B (en) * 2019-07-03 2022-12-27 中国航发商用航空发动机有限责任公司 Assembling tool and assembling method for low-pressure turbine rotor
CN111943014A (en) * 2020-06-30 2020-11-17 中国航发南方工业有限公司 Hanging device of aircraft engine starter and assembly method thereof
CN111943014B (en) * 2020-06-30 2022-05-03 中国航发南方工业有限公司 Hanging device of aircraft engine starter and assembly method thereof

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
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Application publication date: 20170222