CN1487203A - Axial-flow blower - Google Patents
Axial-flow blower Download PDFInfo
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- CN1487203A CN1487203A CNA03133346XA CN03133346A CN1487203A CN 1487203 A CN1487203 A CN 1487203A CN A03133346X A CNA03133346X A CN A03133346XA CN 03133346 A CN03133346 A CN 03133346A CN 1487203 A CN1487203 A CN 1487203A
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Abstract
The axial flow blower consists of intake channel, intake device, front casing, middle casing, back casing, front bearing, middle bearing, back bearing, rotor, drive shaft, back bearing casing and other parts. The middle baring assembly has three rows thrust ball bearings forming the middle axial bearing unit to bear the giant forward axial force the rotor assembly produces; and the back bearing assembly has sealing casing and thrust cavity to form booster cavity, introduces high pressure air the blower exhaust channel exhausts and constitutes the back bearing high pressure air guiding unloader. The thrust disc produces backwards axial force to balance most forward axial force of the blower rotor assembly. The combined function of these two devices makes the axial-flow blower capable of bearing giant axial force. The present invention is used in gas turbine and air system air source machine.
Description
Affiliated technical field
The invention belongs to the fluid machines field, be particularly related to a kind of gas turbin test that both can be used for, can be used as air system source of the gas machine again, be applied to smelt air blast, mine ventilation, can bear enough larger axial forces, functional reliability is good, the axial-flow blower of long service life.
Background technique
In gas turbine performance test field, the method that adopt countries in the world is not quite similar, Germany etc. adopt hydrodynamometer, U.S. GE company adopts the generator measurement of power, Russia adopts generator around the resistance wire measurement of power, ubiquitous problem is: testing installation is huge, size is big, weight is big, investment is big, is difficult for grasping and operation.Adopting axial-flow blower is that to carry out the gas turbine performance test be initiative in load, can overcome the problem of above-mentioned existence, but existing axial-flow blower is because of its structural limitations, the axial force that can bear is too small, functional reliability is poor, working life is short, both be used in smelt air blast, also there are these problems in mine ventilation.
Summary of the invention
The purpose of this invention is to provide and a kind ofly can be used for performance tests such as gas turbine measurement of power as load device, again can be as the source of the gas machine, what be applied to metallurgical air blast, mine ventilation bears that enough big axial force, functional reliability are good, the axial-flow blower of long service life.
Axial-flow blower of the present invention is made up of intake duct, air inlet system, front housing, middle casing, fan rotor, transmission shaft, preceding supporting, back supporting, rear housing, middle supporting, back support case assembly.Before supporting, back supporting and middle bearing assembly form the supporting system of rotor assembly, preceding supporting and back bearing assembly are only born the radial force of rotor assembly, middle bearing assembly had both been born the radial force of rotor assembly and had also been born axial force, mainly bore axial force.The blower fan power demand drives fan rotor assembly high speed rotating by the input of rotor assembly rear propeller shaft, and working blade on the rotor assembly and the straightener(stator) blade on the stator transform energy into the pressure energy of air-flow, are exported by air outlet flue.One row's working blade and row's straightener(stator) blade are formed one-level, and totally 9 grades of this blower fans, the stream pressure of output can make rotor assembly generation axial force forward, and output gas flow pressure can be healed greatly, and the axial force forward of generation is bigger.
The middle supporting axial force bearing device of axial-flow blower of the present invention is arranged in the middle bearing assembly, constituting middle bearing assembly by three rows ball bearing arranged side by side, middle supporting casing, inner split ring, outer spacer ring, Coupling Shaft forms, it is the central bearing point of fan rotor, three row's bearing supporting Coupling Shaft, axle journal by dowel fixes together behind transaxle and the rotor, the fan rotor high speed rotating, bearing is the radial force and the axial force of bear rotor simultaneously, and three row's bearing pack mainly are subjected to axial force.
Because adopt said structure, advantage of the present invention is:
1, three vollyball bearings adopt the D1176720Q of two halves inner ring, 4 contact-types
1T
1Angular contact ball bearing, its wrapping angle is big, and the dress ball is many, and retainer is an integrated type, thereby its intensity height, the bearing capacity height.
2, be provided with inside and outside spacer ring between three row's bearings, select the outer ring spacer of different-thickness, can regulate the play of bearing, make it evenly, thereby make three row's axial force equalizations that bearing bore, certain row's bearing can not take place because of the stressed phenomenon of damaging of concentrating.
3, bearing three rows make up and stressed even equalization side by side, so can bear enough big axial force.
The back supporting high-pressure bleed air relief arrangement of axial-flow blower of the present invention is arranged in the bearing assembly of back, is made up of thrust disc, the housing of obturaging, comb ring gear, air duct.Horn-like rear end of blower fan transmission shaft and thrust disc are fixed together by radial peg, the obturage face of obturaging of two aluminising silicon coatings on comb tooth and the frame set of obturaging of inside and outside twice matches on the thrust disc, thrust disc rotates with transmission shaft, obturaging simultaneously forms booster cavity between housing and thrust disc, and this booster cavity communicates with blower fan air outlet flue and exhaust volute through air duct.
Because adopt the said structure device, advantage of the present invention is:
1, booster cavity is introduced high-pressure air in air duct and exhaust volute that the blower fan air outlet flue communicates, on thrust disc, form axial force backward, this power can balance most of fan rotor and produce and act on axial force forward on the transmission shaft, reaches the off-load effect.
2, the blower fan exhaust pressure becomes big or diminishes, and the booster cavity inner air pressure also becomes big thereupon or diminishes, and the balancing axial thrust of generation also becomes big thereupon or diminishes, and can reach identical off-load effect.
3, the axial force backward that forms on thrust disc of booster cavity has alleviated the axial load of three row's bearings in the middle bearing assembly effectively, has improved the operating conditions of bearing, thereby has improved the working life of axial-flow blower, has improved the reliability of blower fan.
Description of drawings
Fig. 1 is an axial-flow blower sectional arrangement drawing of the present invention;
Fig. 2 is axial-flow blower inlet component figure;
Fig. 3 is axial-flow blower air inlet system figure;
Fig. 4 is a casing component drawings in the axial-flow blower;
Fig. 5 is support case assembly behind the axial-flow blower, middle bearing assembly and the frame set figure that obturages;
Fig. 6 is the axial flow fans rotor component drawings;
Fig. 7 is axial-flow blower transmission shaft component figure;
Fig. 8 is supporting axial force bearing device figure in the axial-flow blower of the present invention;
Fig. 9 is supporting high-pressure bleed air relief arrangement figure behind the axial-flow blower of the present invention.
Embodiment
As shown in Figure 1, axial-flow blower of the present invention is made up of inlet component 1, air inlet system 2, preceding bearing assembly 3, front housing assembly 4, middle casing assembly 5, fan rotor assembly 6, rear housing assembly 7, back support case assembly 8, middle bearing assembly 9 (supporting axial force bearing device in containing), transmission shaft component 10, back bearing assembly 11 (containing back supporting high pressure leader relief arrangement).Axial-flow blower transmission shaft component 10 is through fixing with it thrust disc 47, with connecting bolt 58 (47,58 in Fig. 9) through coupling and the gas turbine main shaft (not shown) that links, gas turbine drives fan rotor assembly 6 high speed rotating, air enters blower fan from inlet component 1, guide vane on the air inlet system 2 is directed at optimum orientation with the air-flow angle of rotor inlet, straightener(stator) blade on the stator that working blade on the rotor assembly 6 and middle casing assembly 5 and rear housing assembly 7 are formed is converted into mechanical energy the pressure energy of air-flow under rotor assembly 6 high speed rotating states, totally 9 grades of axial-flow blowers of the present invention (one-level working blade and row's straightener(stator) blade are formed one-level), have the venting window behind the 5th grade of straightener(stator) blade, the venting window is opened the stable operation zone that can enlarge blower fan greatly when needing, and effectively air mass flow and compression ratio will reduce simultaneously.During the blower fan stable operation, the 1st level work blade air-flow reaches transonic speed, and all the other levels are subsonic speed.Be converted into pressure can pressurized air discharge (to the exhaust volute---not shown) by blower fan air outlet flue B.Stream pressure can raise step by step in the fan operation, and the comprehensive function of stream pressure energy makes fan rotor assembly 6 produce very big axial force forward, and output gas flow pressure can be healed greatly, and producing forward, axial force heals big.
The radial force of bearing assembly 3 and back 11 bear rotor assemblies 6 of bearing assembly and transmission shaft component 10 before the blower fan, middle bearing assembly 9 is bearing radial force and axial force simultaneously, and all radial forces that produce in the blower fan and axial force pass to blower fan supporting component and basis by back support case assembly 8.
As shown in Figure 2, inlet component is made up of the intake duct 12 of aluminum alloy plate materials manufacturing and the group section 13 of No. 45 steel cast member manufacturings.Be installed in axial-flow blower foremost,, be used for collecting air and import the blower fan runner with front housing assembly 4 end face bolt.Intake duct front-end face lip is that twisted-pair cable shape rear portion and cylindrical section join, and this design can make the air of importing smooth evenly and reduce flow resistance loss.
Have 4 baroports and 4 stagnation pressure gaging holes on the group section 13 in uniform way, be used for measuring total static pressure of air-flow in the intake duct, also can in the stagnation pressure gaging hole, insert the air mass flow that Pitot tube is measured blower fan when the total differential static pressure of air-flow is used for evaluation work in the intake duct.
As shown in Figure 3, air inlet system enters blower fan in order to guide air with the flow losses of minimum, is made up of cowling 14 and bearing 15.
Bearing 15 is welded by aluminium alloy plate, comprises the bearing cylinder 20 and double-deck support plate 19.
Front housing assembly 4 is between middle casing assembly 5 and air inlet system 2, and front and back all interfix so that the limit bolt to be installed, and establish hollow rectification support plate and adjustable guide vane in the front housing assembly 4, are directed at optimum orientation in order to the air-flow with rotor assembly 6 inlets.
As shown in Figure 4, middle casing assembly is one of main load spare of axial-flow blower.Form by forward and backward rectification cabin 21,22.Preceding rectification cabin 21 magnesium alloy manufacturing, the interior dress first order is to level V straightener(stator) blade 23.Back rectification cabin 22 usefulness Alloy Constructional Steels are made, in adorn the 6th grade to the 8th grade straightener(stator) blade 23.For the ease of assembling and decomposition, middle casing is divided into left and right sides two-part.
First and second, five, six, seven, eight grades be the steel straightener(stator) blade, all the other two-stages are aluminium straightener(stator) blades, but are steel for the rigidity that increases structure and intensity also have partial blade.Straightener(stator) blade 23 is fixed on the middle casing by the rectangle liner plate and the threaded cylindrical section on top, leans on the smooth cylindrical section of bottom to be connected with forward and backward semi-ring 24,25, and first to eight grade of forward and backward semi-ring 24,25 all adopted steel material.Front and back semi-ring bolt.The junction point in rectification cabin 21,22 has a discharging transom window mouth before and after the middle casing, and the venting band that can handle switching is stamped in the outside.
The cylindrical locating face on limits and the positioning boss on front housing assembly 4 installation limits are installed before the middle casing assembly 5 to match.The positioning boss on limit is installed in the back and the cylindrical locating face on rear housing assembly 7 installation limits matches.Middle casing is connected by bolt and clamping bolt with forward and backward casing assembly.
As shown in Figure 5, be back support case assembly and middle bearing assembly, the frame set of obturaging.Back support case assembly supports casing 27 by rear housing assembly 7, support case 26, back and support cylinder 28 assemblies are formed, and is the main load parts of axial-flow blower.
Rear housing 7 is made up of rear housing inner and outer rings 29,30, the 9th grade of straightener(stator) blade 31 and the rear housing ring 32 of obturaging, rear housing inner and outer rings 29,30 forms for stainless steel forgings machining, inner and outer rings links into an integrated entity by the 9th grade of straightener(stator) blade that 68 stainless steel castings form, form air-flow path, rear housing 17 radial peg of ring 32 usefulness of obturaging are fixed in the rear housing and encircle on 29.
Rear housing 7 is used bolt with support case 26, and support case 26 is main load-bearing parts of axial-flow blower, and the axial force that blower fan produces, radial force are delivered to by supporting component and main supporting component by it and install on the basis.
Support case 26 is rust steel cast member, and the casing inner and outer rings links to each other with eight wing support plates, and the inside and outside ring surface is taper, and inside and outside ring forms the air-flow path of diffusion.The limit is installed before the ring in the support case 26 has 18 bolts hole to be used for fixing middle supporting casing 33, and the bolt group is fixed together support case 26 and back supporting casing 27.
The back is supported casing 27 and is made by the stainless steel cast member, limit is installed before it links to each other with installation limit in the support case 26, and the back is installed the limit and is used for fixing the rear bearing casing 24 and the frame set 35 of obturaging.
As shown in Figure 6, the fan rotor assembly is a full steel structure, is made up of one to nine grade of wheel disc 36, forward and backward axle journal 37,38 and working blade 39.All obturaging between the wheel discs 36 at different levels, the semi-ring surface engagement form clearance seals in comb tooth 40 and the middle casing assembly 5, between each wheel disc 36 and wheel disc and being connected of axle journal be to locate by the cylndrical surface to press together and fix with pin radially.
The twice circle of obturaging is arranged on the axle journal before the rotor, form with front housing assembly 4 and seal.Bearing assembly 3 before roller bearing 41 forms with its support, the circle of obturaging, the anterior radial force of bear rotor assembly.
The conical surface of back axle journal 38 has row's comb tooth of obturaging, and cooperates the formation clearance seal with the rear housing ring 32 of obturaging.Back axle journal 38 rear ends are connected with Coupling Shaft 42, and by 43 supportings of three vollyball bearings, Coupling Shaft 42 is arranged each nine radially dowel fixes with back axle journal 38 usefulness two.In the back axle journal 38 coupling 44 is arranged, coupling 44 limits it and moves axially pin key 45 stop after coupling 44 leans on the axle journal behind the internal spline of the external splines insertion back axle journal 38 of transmission shaft.
As shown in Figure 7, transmission shaft component is made up of transmission shaft 46, thrust disc 47 and comb ring gear 48 etc.Transmission shaft component is used for transmitting the power fan rotor assembly 6 of driving machine, and transmission 46 is bearing in rotation in three row's bearings 43 and the back supporting roller bearing 56, and front end is connected with axle journal behind the fan rotor by coupling 44.
As shown in Figure 8, during being arranged on, middle supporting axial force bearing device in the bearing assembly, forms by three row's bearings 43, middle supporting casing 33, inner split ring 46, outer spacer ring 50, Coupling Shaft 42 etc.
Angular contact ball bearing (model D1176720Q
1T
1) 43 (three rows) inner ring supporting blower fan Coupling Shaft 42, fan rotor assembly 6 back axle journals 38 are fixed together the axial force of bearing bear rotor and radial force with Coupling Shaft 42 via pins; Be provided with outer ring spacer 50, cone spacer 49 between three row's bearings,, make play even in order to regulate bearing clearance; Bearing outer ring is loaded on and supports in the blower fan in the casing 33, and is spacing by locked spacer 51.In supporting casing 33 be provided with before and after lubricant oil nozzle 52 cooperate with disc 53 and arrange bearings 43 to three and carry out pressure lubrication; Screw is fixed together middle supporting casing 33 and back support case assembly 8, gives back support case assembly 8 with the radial force and the axial force transmission of being born.The involute splines of transmission shaft 46 front ends and the fan rotor 6 back axle journal 38 internal splines transmitting torque that is meshed; Inside and outside spline is circumferentially located by positioning block 54; Transmission shaft 46 front ends have 4 protuberances to cooperate with coupling 44 to be used for and transmit the axial force backward that thrust disc 47 produces.
As shown in Figure 9, back supporting high-pressure bleed air relief arrangement is made up of thrust disc 47, the housing 35 of obturaging, comb ring gear 48, air duct 55 by being arranged in the bearing assembly of back.
The back bearing assembly is formed in roller bearing 56 and supporting thereof, bear the radial force of transmission shaft component 10, transmission shaft 46 is fixed together by 19 pins 57 with thrust disc 47, the obturage face of obturaging of two aluminising silicon coatings on comb tooth and comb ring gear 48 and housing 35 assemblies of obturaging of the inside and outside twice of design matches on the thrust disc 47, form to rotate and pay sealing, so just make thrust disc 47 and obturage and formed booster cavity A between the housing 35, booster cavity A communicates with blower fan air outlet flue B and exhaust volute through air duct 55 and introduces the high-pressure air that axial-flow blower is discharged, on thrust disc 47, produce axial force backward, balance major part that rotor assembly 6 produces axial force forward.Attachment screw 58 on the thrust disc 47 links through coupling and gas turbine main shaft, through transmission shaft component 10 fan rotor assembly 6 input powers.Obturage and limit 59 usefulness bolts be installed before housing 35 and the housing of obturaging and connected firmly, simultaneously with connecting bolt nut 60 connect firmly the back support casing 27 and after on the support case assembly 8.
The synergy of supporting axial force bearing device and back supporting high-pressure bleed air relief arrangement shown in Figure 9 makes axial-flow blower can bear enough big axial force in shown in Figure 8, has improved the functional reliability and the working life of axial-flow blower, has realized purpose of the present invention.
Supporting axial force bearing device can be born 10 times of axial forces to common similar axial-flow blower among the present invention; Back supporting high-pressure bleed air relief arrangement falls 60% with the axial force off-load of fan rotor, makes its axial force reduce to original 40%.
Adopt axial-flow blower of the present invention to carry out gas turbin test, have advantages such as size is little, in light weight, investment is little, easy operating manipulation, reliable operation.
Axial-flow blower of the present invention is used as the source of the gas machine, is applied to smelt places such as air blast, mine ventilation, compares with common similar axial-flow blower, can improve greatly its functional reliability and working life.
Claims (4)
1, a kind of axial-flow blower, by inlet component, air inlet system, the front housing assembly, middle casing assembly, the rear housing assembly, the fan rotor assembly, transmission shaft component, preceding bearing assembly, middle bearing assembly, back bearing assembly, back support case assembly constitutes, the middle bearing assembly that it is characterized in that this axial-flow blower is provided with middle supporting axial force bearing device, back bearing assembly is provided with back supporting high-pressure bleed air relief arrangement, in supporting axial force bearing device in blower fan in the bearing assembly by three vollyball bearings, middle supporting casing, inner split ring, outer spacer ring, Coupling Shaft is formed, be provided with inner split ring and outer spacer ring between three row's thrust ball bearings, the Coupling Shaft and the transmission shaft of bearing inner race supporting fan rotor, bearing outer ring is loaded in the blower fan and supports in the casing, and bearing enclose is respectively by disc, locked spacer, nut forms axial constraint; Back supporting high-pressure bleed air relief arrangement is made up of thrust disc, the housing of obturaging, comb ring gear, air duct in the bearing assembly behind blower fan, blower fan transmission shaft rear end and thrust disc connect firmly, the inside and outside twice comb tooth of obturaging matches with the face of obturaging of comb ring gear, the frame set of obturaging on the thrust disc, thrust disc and obturage and form booster cavity between housing, air duct is communicated with booster cavity and blower fan air outlet flue and exhaust volute.
2, axial-flow blower according to claim 1, in it is characterized in that supporting axial force bearing device and in the supporting casing be fixed on behind the blower fan on the support case assembly.
3, axial-flow blower according to claim 1, three row's bearings implementation pressure lubrications in the supporting axial force bearing device in it is characterized in that.
4, axial-flow blower according to claim 1, it is characterized in that back supporting high-pressure bleed air relief arrangement before the housing of obturaging, installs behind limit and the blower fan support casing and afterwards the support case assembly connect firmly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB03133346XA CN1195153C (en) | 2003-05-21 | 2003-05-21 | Axial-flow blower |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB03133346XA CN1195153C (en) | 2003-05-21 | 2003-05-21 | Axial-flow blower |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1487203A true CN1487203A (en) | 2004-04-07 |
| CN1195153C CN1195153C (en) | 2005-03-30 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB03133346XA Expired - Lifetime CN1195153C (en) | 2003-05-21 | 2003-05-21 | Axial-flow blower |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101619745B (en) * | 2008-07-04 | 2011-02-02 | 沈阳黎明航空发动机(集团)有限责任公司 | Force-bearing device capable of bearing large axial load |
| CN104533840A (en) * | 2015-01-26 | 2015-04-22 | 成都成发科能动力工程有限公司 | Axial air incoming enclosure of axial-flow compressor |
| CN109357595A (en) * | 2018-12-07 | 2019-02-19 | 中国航发南方工业有限公司 | The measurement method of axial gap between centrifugal impeller and impeller outer cover |
| CN109632276A (en) * | 2018-12-16 | 2019-04-16 | 中国航发沈阳发动机研究所 | One kind subtracting whirlpool device experimental rig |
| CN113898419A (en) * | 2021-10-10 | 2022-01-07 | 中国航发沈阳发动机研究所 | Air inlet casing structure and assembling method thereof |
-
2003
- 2003-05-21 CN CNB03133346XA patent/CN1195153C/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101619745B (en) * | 2008-07-04 | 2011-02-02 | 沈阳黎明航空发动机(集团)有限责任公司 | Force-bearing device capable of bearing large axial load |
| CN104533840A (en) * | 2015-01-26 | 2015-04-22 | 成都成发科能动力工程有限公司 | Axial air incoming enclosure of axial-flow compressor |
| CN104533840B (en) * | 2015-01-26 | 2017-04-12 | 成都成发科能动力工程有限公司 | Axial air incoming enclosure of axial-flow compressor |
| CN109357595A (en) * | 2018-12-07 | 2019-02-19 | 中国航发南方工业有限公司 | The measurement method of axial gap between centrifugal impeller and impeller outer cover |
| CN109632276A (en) * | 2018-12-16 | 2019-04-16 | 中国航发沈阳发动机研究所 | One kind subtracting whirlpool device experimental rig |
| CN113898419A (en) * | 2021-10-10 | 2022-01-07 | 中国航发沈阳发动机研究所 | Air inlet casing structure and assembling method thereof |
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| Publication number | Publication date |
|---|---|
| CN1195153C (en) | 2005-03-30 |
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Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee after: AECC SHENYANG LIMING AERO-ENGINE Co.,Ltd. Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee before: Aecc Shenyang Liming Aero Engine Co., Ltd. |
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Granted publication date: 20050330 |
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