CN116086763A - Large continuous wind tunnel axial flow compressor bearing overhauling method and overhauling device - Google Patents

Large continuous wind tunnel axial flow compressor bearing overhauling method and overhauling device Download PDF

Info

Publication number
CN116086763A
CN116086763A CN202310266861.3A CN202310266861A CN116086763A CN 116086763 A CN116086763 A CN 116086763A CN 202310266861 A CN202310266861 A CN 202310266861A CN 116086763 A CN116086763 A CN 116086763A
Authority
CN
China
Prior art keywords
bearing
rotor
overhauling
jack
wind tunnel
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.)
Granted
Application number
CN202310266861.3A
Other languages
Chinese (zh)
Other versions
CN116086763B (en
Inventor
许岭松
王浩然
文旭锋
薄磊
艾宏伟
罗劲
崔晓春
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.)
AVIC Shenyang Aerodynamics Research Institute
Original Assignee
AVIC Shenyang Aerodynamics Research Institute
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 AVIC Shenyang Aerodynamics Research Institute filed Critical AVIC Shenyang Aerodynamics Research Institute
Priority to CN202310266861.3A priority Critical patent/CN116086763B/en
Publication of CN116086763A publication Critical patent/CN116086763A/en
Application granted granted Critical
Publication of CN116086763B publication Critical patent/CN116086763B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25HWORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
    • B25H1/00Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby
    • B25H1/06Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby of trestle type
    • 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
    • B66C1/22Rigid members, e.g. L-shaped members, with parts engaging the under surface of the loads; Crane hooks
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F3/00Devices, e.g. jacks, adapted for uninterrupted lifting of loads
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02Wind tunnels
    • G01M9/04Details
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Structural Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A method and a device for overhauling a bearing of a large continuous wind tunnel axial flow compressor belong to the field of wind tunnel construction. The invention solves the problems that when the bearing of the existing large-scale continuous wind tunnel axial flow compressor is overhauled, the disassembly and assembly workload is large, the disassembly and assembly period is long, the rotor moving blades are easy to damage, and the overhauling work is not easy to be smoothly carried out. The invention firstly removes the upper half shells of the air inlet shell and the air outlet shell, then removes the upper cover of the bearing box and the upper half part of the bearing in sequence, lifts the rotor upwards by 0.5mm through the axle supporting tool and the jack, and then pulls out the bearing bush of the lower half part of the bearing through the chain block for overhauling. The method and the device for overhauling the bearing of the large continuous wind tunnel axial compressor avoid the risk of damaging the blades in the process of hoisting the rotor, have better protection effect on the rotor, and reduce the workload, the disassembly difficulty and the disassembly period of the disassembly and assembly axial compressor.

Description

Large continuous wind tunnel axial flow compressor bearing overhauling method and overhauling device
Technical Field
The invention belongs to the field of wind tunnel construction, and particularly relates to a method and a device for overhauling a bearing of a large continuous wind tunnel axial flow compressor.
Background
Wind tunnel tests are widely adopted as aerodynamic research methods, and necessary guarantees are provided for development in the fields of aviation, aerospace, railway transportation and the like. In a continuous transonic wind tunnel, an axial compressor is used for driving air flow in a wind tunnel loop to provide an operating pressure ratio required for establishing a wind tunnel flow field, and belongs to important equipment of the continuous wind tunnel.
The bearing component of the continuous wind tunnel axial flow compressor is arranged in the wind tunnel flow channel, is mostly a sliding bearing divided up and down and is used for supporting a compressor rotor and bearing the axial force of the compressor unit during operation; when the bearing assembly is overhauled, the upper half bearing can be directly dismantled, and when the lower half bearing is overhauled by bearing the weight of the rotor, the rotor of the axial flow compressor is usually required to be lifted out for overhauling.
The rotor of the large-scale continuous wind tunnel axial flow compressor has the advantages of large weight, large rotor diameter and sealing assembly arranged on the rotor, and the conventional method of bearing overhaul after the rotor of the axial flow compressor is lifted out is adopted, so that the disassembly and assembly workload is large, the disassembly and assembly overhaul period is long, the rotor moving blades are easy to damage, and the smooth operation of overhaul work is not facilitated.
Therefore, the application provides a method and a device for overhauling a bearing of a large continuous wind tunnel axial flow compressor, and the overhauling work of the bearing is completed on the premise that a compressor rotor does not need to be lifted out.
Disclosure of Invention
The invention aims to solve the problems that when the bearing of the existing large-scale continuous wind tunnel axial flow compressor is overhauled, the workload of disassembly and assembly is large, the disassembly and overhaul period is long, rotor moving blades are easy to damage, and the overhauling work is not easy to smoothly carry out. The following presents a simplified summary of the invention in order to provide a basic understanding of some aspects of the invention. It should be understood that this summary is not an exhaustive overview of the invention. It is not intended to identify key or critical elements of the invention or to delineate the scope of the invention.
The technical scheme of the invention is as follows:
scheme one: a method for overhauling a bearing of a large continuous wind tunnel axial flow compressor comprises the following steps:
step one: respectively dismantling the upper half shells of the air inlet shell and the air outlet shell, and dismantling the upper cover of the bearing box and the upper half part of the bearing in sequence;
step two: placing the shaft supporting tool at the bottom of the rotor, respectively installing two screw rods at two ends of the shaft supporting tool, placing a jack on a lower cover of a bearing box, horizontally placing a transverse plate at an execution end of the jack through the two screw rods, screwing a nut into each screw rod, and screwing the nut to fix the transverse plate;
step three: the height of the jack is adjusted to enable the jack to lift the rotor by 0.5mm and maintain the height;
step four: the fixed bracket is arranged on the central shell, the chain block is arranged on the fixed bracket, the other end of the chain block is sequentially connected with the hanging strip and the hanging ring, and then the hanging ring is fixed on a threaded hole in the lower half part of the bearing;
step five: tensioning the lower end of the chain block, driving the hanging strip, the hanging ring and the lower half part of the bearing to enable the lower half part of the bearing to rotate around the journal of the rotor until the bearing bush is unscrewed from the lower cover of the bearing box, and overhauling the bearing bush of the bearing;
step six: after the maintenance is finished, the height of the jack is adjusted, so that the jack lowers the rotor by 0.5mm, then the upper half part of the bearing is combined with the lower half part of the bearing, the upper cover of the bearing box is combined with the lower cover of the bearing box, and finally the upper half shells of the air inlet shell and the air outlet shell are installed, so that the maintenance work of the bearing is completed.
Further, in the second step, a copper sheet is arranged on the inner side wall of the shaft supporting tool, and when the shaft supporting tool is placed at the bottom of the rotor, a layer of copper sheet protection is arranged between the inner side wall of the shaft supporting tool and the shaft neck of the rotor.
Scheme II: according to the overhauling device of the overhauling method for the bearing of the large continuous wind tunnel axial compressor, the overhauling device comprises a shaft supporting tool, the shaft supporting tool supports a rotor, screws are symmetrically arranged at two ends of the shaft supporting tool, two jacks are symmetrically arranged at two ends of a lower cover of a bearing box, a transverse plate is arranged on the jacks, the screws penetrate through the transverse plate to be arranged, nuts are arranged on the screws, and the bottoms of the nuts are in contact with the end faces of the transverse plate.
Further, a fixed support is arranged on the central casing, a chain block is arranged on the fixed support, the other end of the chain block is sequentially connected with a hanging strip and a hanging ring, and the hanging ring is in threaded connection with the lower half part of the bearing.
Further, the jack is a mechanical self-locking jack.
The invention has the following beneficial effects:
according to the method for overhauling the bearing of the large-scale continuous wind tunnel axial flow compressor, in the overhauling process of the bearing bush of the large-scale continuous wind tunnel axial flow compressor, devices such as a rotor and a rotor-related lubricating oil seal are not required to be removed, the risk of damage to blades in the hoisting process of the rotor is avoided, a good protection effect is achieved on the rotor, and the service life of the rotor is prolonged.
According to the method for overhauling the bearing of the large continuous wind tunnel axial flow compressor, provided by the invention, the disassembly and assembly workload, the disassembly and assembly difficulty and the disassembly and assembly overhauling period are reduced, and in the overhauling process, the weight of the rotor is borne by the mechanical self-locking jack, so that the rotor is effectively prevented from suddenly falling down and being damaged due to failure of the jack.
Drawings
FIG. 1 is a schematic view of the overall structure of an axial flow compressor;
FIG. 2 is a schematic illustration of an axial flow compressor with an upper half of the intake housing removed;
FIG. 3 is a top view of FIG. 2 with the bearing housing upper cover removed;
FIG. 4 is a top view of the upper half of the bearing of FIG. 3 with the bearing removed;
FIG. 5 is a cross-sectional view taken along A-A of FIG. 4;
fig. 6 is a schematic diagram of the use of a chain block to hoist the lower half of the bearing.
In the figure: the device comprises a 1-air inlet machine shell, a 2-central machine shell, a 3-rotor, a 4-air outlet machine shell, a 5-hole body, a 6-bearing box upper cover, a 7-bearing box lower cover, an 8-bearing upper half part, a 9-bearing lower half part, a 10-jack, an 11-shaft supporting tool, a 12-screw rod, a 13-transverse plate, a 14-nut, a 15-chain, a 16-fixed support, a 17-hanging strip and an 18-hanging ring.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the present invention more apparent, the present invention is described below by means of specific embodiments shown in the accompanying drawings. It should be understood that the description is only illustrative and is not intended to limit the scope of the invention. In addition, in the following description, descriptions of well-known structures and techniques are omitted so as not to unnecessarily obscure the present invention.
The connection mentioned in the present invention is divided into a fixed connection and a detachable connection, wherein the fixed connection (i.e. the non-detachable connection) includes, but is not limited to, a conventional fixed connection manner such as a hemmed connection, a rivet connection, an adhesive connection, a welded connection, etc., and the detachable connection includes, but is not limited to, a conventional detachable manner such as a threaded connection, a snap connection, a pin connection, a hinge connection, etc., and when the specific connection manner is not specifically limited, at least one connection manner can be found in the existing connection manner by default, so that the function can be realized, and a person skilled in the art can select the connection according to needs. For example: the fixed connection is welded connection, and the detachable connection is hinged connection.
In the present invention, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art according to the specific circumstances.
Embodiment 1, referring to fig. 1-6, a bearing maintenance method for a large-scale continuous wind tunnel axial compressor of the present embodiment is described, the axial compressor includes an intake housing 1, a central housing 2, an exhaust housing 4 and a hole 5, the intake housing 1, the central housing 2 and the exhaust housing 4 are sequentially connected through flanges, the other sides of the intake housing 1 and the exhaust housing 4 are connected with the hole 5 through flanges, a bearing housing is installed in each of the intake housing 1 and the exhaust housing 4, the bearing housing includes a bearing housing upper cover 6 and a bearing housing lower cover 7, the bearing housing lower cover 7 is disposed in the intake housing 1 and the exhaust housing 4, a bearing lower half 9 is disposed in the bearing housing lower cover 7, a rotor 3 is disposed on the bearing lower half 9, the bearing upper half 8 is disposed in the bearing housing upper cover 6 through pins and nails, the bearing housing upper cover 6 and the bearing housing lower cover 7 are respectively made of the upper half and the lower half.
When the axial compressor bearing is overhauled, the method specifically comprises the following steps of:
step one: the upper half shells of the air inlet shell 1 and the air outlet shell 4 are respectively dismantled, and the bearing box upper cover 6 and the bearing upper half part 8 in the air inlet shell 1 and the air outlet shell 4 are sequentially dismantled;
step two: placing the shaft supporting tool 11 at the bottom of the rotor 3, respectively installing two screw rods 12 at two ends of the shaft supporting tool 11, placing the jack 10 on the lower cover 7 of the bearing box, horizontally placing the transverse plate 13 at the execution end of the jack 10 through the two screw rods 12, screwing a nut 14 into each screw rod 12, and screwing the nut 14 to fix the transverse plate 13;
step three: adjusting the height of the jack 10 so that the jack 10 lifts the rotor 3 by 0.5mm and maintains the height;
step four: the fixed bracket 16 is arranged on the central shell 2 through screws, the chain block 15 is arranged on the fixed bracket 16, the other end of the chain block 15 is sequentially connected with the hanging strip 17 and the hanging ring 18, and then the hanging ring 18 is fixed on a threaded hole of the lower half part 9 of the bearing;
step five: the lower end of the chain 15 is pulled tightly to drive the hanging strip 17, the hanging ring 18 and the lower half part 9 of the bearing, so that the lower half part 9 of the bearing rotates around the journal of the rotor 3 until the bearing bush is screwed out of the lower cover 7 of the bearing box, and the bearing bush of the bearing is overhauled;
step six: after the maintenance is finished, the height of the jack 10 is adjusted, so that the jack 10 lowers the rotor 3 by 0.5mm, then the upper half 8 of the bearing is combined with the lower half 9 of the bearing, the upper cover 6 of the bearing box is combined with the lower cover 7 of the bearing box, and finally the upper half shells of the air inlet shell 1 and the air outlet shell 4 are installed, so that the maintenance work of the bearing is completed.
In order to avoid damage to the rotor when the shaft supporting tool 11 supports the rotor 3, a layer of copper sheet is arranged on the inner wall of the shaft supporting tool 11, and when the shaft supporting tool 11 is used for lifting the rotor 3 upwards, the rotor 3 cannot be damaged under the protection of the copper sheet.
An embodiment 2, referring to fig. 1-6, illustrates a large continuous wind tunnel axial flow compressor bearing maintenance device in this embodiment, including a supporting shaft tooling 11, where the supporting shaft tooling 11 is a U-shaped tooling, the rotor 3 is towed by the supporting shaft tooling 11, threaded holes are machined at two ends of the supporting shaft tooling 11, two screws 12 are in threaded connection with the supporting shaft tooling 11 through the threaded holes, a jack 10 is installed at two ends of a bearing box lower cover 7, a diaphragm 13 passes through the two screws 12 and is arranged on the jack 10, a nut 14 is connected to each screw 12, the nut 14 is arranged above the diaphragm 13, the bottom of the nut 14 contacts with the upper end surface of the diaphragm 13, and the rotor 3 is lifted upwards by a certain distance under the action of the jack 10 and the supporting shaft tooling 11, so that the rotor 3 is separated from the lower half 9 of the bearing;
a fixed support 16 is arranged on the central casing 2 through a screw, a chain block 15 is arranged on the fixed support 16, the other end of the chain block 15 is sequentially connected with a hanging belt 17 and a hanging ring 18, the hanging ring 18 is in threaded connection with the lower half 9 of the bearing, and under the action of the chain block 15, the bearing bush on the lower half 9 of the bearing is taken out through the hanging ring 18;
further, in order to improve stability of the jack 10, the jack 10 adopts a mechanical self-locking jack to bear weight of the rotor 3, so that the rotor 3 is prevented from suddenly falling down and damaging the rotor 3 due to failure of the jack 10.
The present embodiment is only illustrative of the present invention and does not limit the scope thereof, and those skilled in the art may make modifications to the part thereof without departing from the spirit of the invention.

Claims (5)

1. The method for overhauling the bearing of the large continuous wind tunnel axial flow compressor is characterized by comprising the following steps of:
step one: respectively dismantling the upper half shells of the air inlet shell (1) and the air outlet shell (4), and dismantling the upper cover (6) of the bearing box and the upper half part (8) of the bearing in sequence;
step two: placing a shaft supporting tool (11) at the bottom of a rotor (3), respectively installing two screws (12) at two ends of the shaft supporting tool (11), placing a jack (10) on a lower cover (7) of a bearing box, horizontally placing a transverse plate (13) at the execution end of the jack (10) through the two screws (12), screwing a nut (14) on each screw (12), and screwing the nut (14) to fix the transverse plate (13);
step three: adjusting the height of the jack (10) to enable the jack (10) to raise the rotor (3) by 0.5mm and maintain the height;
step four: the fixed support (16) is arranged on the central casing (2), the chain block (15) is arranged on the fixed support (16), the other end of the chain block (15) is sequentially connected with the hanging belt (17) and the hanging ring (18), and then the hanging ring (18) is fixed on a threaded hole of the lower half part (9) of the bearing;
step five: the lower end of the chain block (15) is pulled tightly to drive the hanging strip (17), the hanging ring (18) and the lower half part (9) of the bearing, so that the lower half part (9) of the bearing rotates around the shaft neck of the rotor (3) until the bearing bush is screwed out of the lower cover (7) of the bearing box, and the bearing bush of the bearing is overhauled;
step six: after the maintenance is finished, the height of the jack (10) is adjusted, so that the jack (10) lowers the rotor (3) by 0.5mm, then the upper half part (8) of the bearing is combined with the lower half part (9) of the bearing, the upper cover (6) of the bearing box is combined with the lower cover (7) of the bearing box, and finally the upper half shells of the air inlet shell (1) and the air outlet shell (4) are installed to finish the maintenance work of the bearing.
2. The method for overhauling a bearing of a large continuous wind tunnel axial compressor according to claim 1, wherein the method comprises the following steps: in the second step, copper sheets are arranged on the inner side walls of the shaft supporting tool (11), and when the shaft supporting tool (11) is placed at the bottom of the rotor (3), a layer of copper sheet protection is arranged between the inner side walls of the shaft supporting tool (11) and the shaft neck of the rotor (3).
3. The utility model provides a large-scale continuous type wind tunnel axial compressor bearing overhauls device which characterized in that: the device is applied to the large-scale continuous wind tunnel axial compressor bearing overhauling method according to claim 1 or 2, the device comprises a shaft supporting tool (11), the shaft supporting tool (11) supports a rotor (3), screw rods (12) are symmetrically arranged at two ends of the shaft supporting tool (11), two jacks (10) are symmetrically arranged at two ends of a lower cover (7) of a bearing box, a transverse plate (13) is arranged on the jacks (10), the screw rods (12) penetrate through the transverse plate (13) to be arranged, nuts (14) are arranged on the screw rods (12), and the bottoms of the nuts (14) are in contact with the end faces of the transverse plate (13).
4. A large continuous tunnel axial compressor bearing service apparatus according to claim 3, wherein: the central casing (2) is provided with a fixed support (16), the fixed support (16) is provided with a chain block (15), the other end of the chain block (15) is sequentially connected with a hanging belt (17) and a hanging ring (18), and the hanging ring (18) is in threaded connection with the lower half part (9) of the bearing.
5. A large continuous tunnel axial compressor bearing service apparatus according to claim 3, wherein: the jack (10) is a mechanical self-locking jack.
CN202310266861.3A 2023-03-20 2023-03-20 Large continuous wind tunnel axial flow compressor bearing overhauling method and overhauling device Active CN116086763B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202310266861.3A CN116086763B (en) 2023-03-20 2023-03-20 Large continuous wind tunnel axial flow compressor bearing overhauling method and overhauling device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202310266861.3A CN116086763B (en) 2023-03-20 2023-03-20 Large continuous wind tunnel axial flow compressor bearing overhauling method and overhauling device

Publications (2)

Publication Number Publication Date
CN116086763A true CN116086763A (en) 2023-05-09
CN116086763B CN116086763B (en) 2023-06-06

Family

ID=86204739

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202310266861.3A Active CN116086763B (en) 2023-03-20 2023-03-20 Large continuous wind tunnel axial flow compressor bearing overhauling method and overhauling device

Country Status (1)

Country Link
CN (1) CN116086763B (en)

Citations (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61104184A (en) * 1984-10-29 1986-05-22 Hitachi Ltd Device for detecting abnormality of rotary compressor
JP2004301258A (en) * 2003-03-31 2004-10-28 Toshiba Corp Journal bearing
CN201218221Y (en) * 2008-06-02 2009-04-08 中国神华能源股份有限公司 Fan tile-turning apparatus
CN102306979A (en) * 2011-09-10 2012-01-04 中国十七冶集团有限公司 Core pulling and threading method for overhauling of large motor
CN203660778U (en) * 2013-11-08 2014-06-18 中国石油化工股份有限公司 Multifunctional motor overhauling device
CN103940611A (en) * 2014-04-09 2014-07-23 中国水利水电科学研究院 Self-adaptive anomaly detection method for rolling bearing of wind generator set under variable working conditions
CN204578306U (en) * 2015-05-12 2015-08-19 华电(北京)热电有限公司 High-rating generator inspection platform
CN204913214U (en) * 2015-08-25 2015-12-30 高德占 Specialized tool of dismouting compressor main shaft tile
CN206175295U (en) * 2016-11-23 2017-05-17 中国航空工业集团公司沈阳空气动力研究所 For continuous wind tunnel fan turbine axle head composite seal structure
CN207132832U (en) * 2017-08-17 2018-03-23 沈阳工业大学 A kind of adjustable centrifugal compressor bearing clearance measurement specific purpose tool
CN108195551A (en) * 2018-01-18 2018-06-22 倪惠芳 A kind of sealing structure for aerospace wind tunnel test nozzle component
CN108547871A (en) * 2018-06-25 2018-09-18 武汉科技大学 Axi-symmetric Contraction and its design method for high pressure disk gas bearing constant-current stabilizer
CN110451392A (en) * 2019-08-31 2019-11-15 山东黄金矿业(玲珑)有限公司 Console model multi-rope friction hoist's head sheave bearing shell replacing options
CN111618559A (en) * 2020-05-31 2020-09-04 中海油能源发展股份有限公司 Device and method for disassembling and assembling mechanical seal and bearing of hot oil circulating pump
CN216008624U (en) * 2021-10-18 2022-03-11 西安陕鼓动力股份有限公司 Main shaft bracket for split type turbine maintenance adjustment
CN114348870A (en) * 2021-12-02 2022-04-15 中石化宁波工程有限公司 Installation device and installation method for internal equipment of large-scale chemical equipment
CN114934917A (en) * 2022-07-21 2022-08-23 中国航空工业集团公司沈阳空气动力研究所 Pipeline noise elimination structure for large continuous wind tunnel axial flow compressor
CN115788944A (en) * 2023-01-16 2023-03-14 中国电建集团透平科技有限公司 Large-scale wind-tunnel fan drive shafting structure

Patent Citations (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61104184A (en) * 1984-10-29 1986-05-22 Hitachi Ltd Device for detecting abnormality of rotary compressor
JP2004301258A (en) * 2003-03-31 2004-10-28 Toshiba Corp Journal bearing
CN201218221Y (en) * 2008-06-02 2009-04-08 中国神华能源股份有限公司 Fan tile-turning apparatus
CN102306979A (en) * 2011-09-10 2012-01-04 中国十七冶集团有限公司 Core pulling and threading method for overhauling of large motor
CN203660778U (en) * 2013-11-08 2014-06-18 中国石油化工股份有限公司 Multifunctional motor overhauling device
CN103940611A (en) * 2014-04-09 2014-07-23 中国水利水电科学研究院 Self-adaptive anomaly detection method for rolling bearing of wind generator set under variable working conditions
CN204578306U (en) * 2015-05-12 2015-08-19 华电(北京)热电有限公司 High-rating generator inspection platform
CN204913214U (en) * 2015-08-25 2015-12-30 高德占 Specialized tool of dismouting compressor main shaft tile
CN206175295U (en) * 2016-11-23 2017-05-17 中国航空工业集团公司沈阳空气动力研究所 For continuous wind tunnel fan turbine axle head composite seal structure
CN207132832U (en) * 2017-08-17 2018-03-23 沈阳工业大学 A kind of adjustable centrifugal compressor bearing clearance measurement specific purpose tool
CN108195551A (en) * 2018-01-18 2018-06-22 倪惠芳 A kind of sealing structure for aerospace wind tunnel test nozzle component
CN108547871A (en) * 2018-06-25 2018-09-18 武汉科技大学 Axi-symmetric Contraction and its design method for high pressure disk gas bearing constant-current stabilizer
CN110451392A (en) * 2019-08-31 2019-11-15 山东黄金矿业(玲珑)有限公司 Console model multi-rope friction hoist's head sheave bearing shell replacing options
CN111618559A (en) * 2020-05-31 2020-09-04 中海油能源发展股份有限公司 Device and method for disassembling and assembling mechanical seal and bearing of hot oil circulating pump
CN216008624U (en) * 2021-10-18 2022-03-11 西安陕鼓动力股份有限公司 Main shaft bracket for split type turbine maintenance adjustment
CN114348870A (en) * 2021-12-02 2022-04-15 中石化宁波工程有限公司 Installation device and installation method for internal equipment of large-scale chemical equipment
CN114934917A (en) * 2022-07-21 2022-08-23 中国航空工业集团公司沈阳空气动力研究所 Pipeline noise elimination structure for large continuous wind tunnel axial flow compressor
CN115788944A (en) * 2023-01-16 2023-03-14 中国电建集团透平科技有限公司 Large-scale wind-tunnel fan drive shafting structure

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
刘高计等: "风洞试验微量滚转力矩测量试验技术", 《弹箭与制导学报》, vol. 38, no. 4 *

Also Published As

Publication number Publication date
CN116086763B (en) 2023-06-06

Similar Documents

Publication Publication Date Title
JP2012533276A (en) Vertical wind power generator
CN116086763B (en) Large continuous wind tunnel axial flow compressor bearing overhauling method and overhauling device
CN110762053A (en) Large water pump capable of realizing integral hoisting and upward dismounting and construction method thereof
CN207162024U (en) A kind of bridge monitoring equipment used suitable for bad weather
CN112027883B (en) High-altitude hoisting quick-release device for generator
CN215592478U (en) Large-scale hydroelectric generating set stopper dismouting mechanism
CN215433450U (en) Disassembling tool for pump seal assembly of reactor cooler
CN114229673A (en) Leaf disc hoisting device and method
CN113336120B (en) Large hydroelectric generating set brake dismounting mechanism and use method
CN212951076U (en) Sail hydraulic cylinder mounting structure
CN212189789U (en) Screw greasing device for supercharger
CN201659397U (en) Hydraulic pressing machine
CN216336131U (en) Marine diesel cylinder liner hoist device
CN216098601U (en) Turbocharger core assembly fixture
CN215854755U (en) Hoisting device for mounting wind power generation tower
CN215748961U (en) Special combination tool for dismounting bearing box cover of 600MW steam turbine unit main engine
CN217926558U (en) Split type pressure cylinder
CN218546136U (en) Become oar bearing testing machine based on internal force method
CN220234404U (en) Cooling device of aluminum electrolysis cell anode lifting motor
CN214771999U (en) Special tool for screw air compressor
CN218801987U (en) Device convenient to dismouting large-scale air compressor machine cooler core
CN220844226U (en) Pre-buried type transverse conveying chain of aluminum profile frame
CN215807369U (en) Network security inspection device convenient to overhaul
CN215804920U (en) Piston rod pulling tool for assembling rotating wheel of axial-flow type plug structure
CN220726620U (en) High temperature fan transmission speed adjusting device

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant