CN103182621B - Reverse flow method for shrinkage fitting of large sleeve type part - Google Patents

Reverse flow method for shrinkage fitting of large sleeve type part Download PDF

Info

Publication number
CN103182621B
CN103182621B CN201310087489.6A CN201310087489A CN103182621B CN 103182621 B CN103182621 B CN 103182621B CN 201310087489 A CN201310087489 A CN 201310087489A CN 103182621 B CN103182621 B CN 103182621B
Authority
CN
China
Prior art keywords
cover parts
sleeve type
type part
air
air quantity
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
CN201310087489.6A
Other languages
Chinese (zh)
Other versions
CN103182621A (en
Inventor
任小伟
雷广进
虞文
王秉武
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.)
Baoji Oilfield Machinery Co Ltd
Original Assignee
Baoji Oilfield Machinery 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 Baoji Oilfield Machinery Co Ltd filed Critical Baoji Oilfield Machinery Co Ltd
Priority to CN201310087489.6A priority Critical patent/CN103182621B/en
Publication of CN103182621A publication Critical patent/CN103182621A/en
Application granted granted Critical
Publication of CN103182621B publication Critical patent/CN103182621B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

The invention discloses a reverse flow method for shrinkage fitting of a large sleeve type part. The reverse flow method comprises the steps as follows: step one, before the shrinkage fitting, the wind source air volume of the reverse flow method is confirmed; step two, after the sleeve type part is heated and subjected to thermal insulation according to processing requirements, the sleeve type part is taken out of a heating furnace and placed on a bracket; step three, a shaft is inserted into a sleeve type part from top to bottom, and no clearance is reserved in the shaft shoulder position; and step four, the air blowing is performed according to an air volume value confirmed in the step one, the air is forced to flow from top to bottom along the sleeve type part, so that a reverse flow is generated, the sleeve type part is cooled to be in a normal temperature state, and then the method is completed. According to the method disclosed by the invention, the air is forced to generate the reverse flow from top to bottom around the sleeve type part, so that the upper part of the sleeve type part is held firstly to form positioning, the zero clearance reserved in the shaft shoulder position is achieved, and the mounting accuracy of the sleeve type part is improved.

Description

The counter-current of large-scale cover parts hot charging
Technical field
The invention belongs to mechanical assembly technique field, relate to a kind of counter-current of large-scale cover parts hot charging.
Background technology
The accurate location of part on axle and be fixedly the key ensureing its normal work, during Model For The Bush-axle Type Parts interference fit, hot charging is common selection.In the hot charging of large-scale cover parts engineering goods, interference fit situation as shown in Figure 1, due to the impact of the free convection of surrounding air after cover parts heating, cover parts bottom first cools, thus the bottom of cover parts is first held tightly, on cover parts h direction, the thermal strain of (longitudinal direction) has just become the main source in gap, shaft shoulder place, and size h is larger, and pivot clearance is larger.
In order to eliminate and reduce gap, shaft shoulder place, the main method adopting forcing press to exert pressure from top at present.Because part is in temperature-fall period, stress is complicated, cannot accurately calculate, and the pressure of forcing press cannot complete equipilibrium power axially, causes the problem of shaft shoulder place gap overroof.And large-scale cover parts is when using forcing press to assist hot charging, be often difficult to be equipped with suitable forcing press by the appearance and size restriction of part.
Summary of the invention
The object of this invention is to provide a kind of counter-current of large-scale cover parts hot charging, large, the difficult problem being equipped with suitable forcing press and carrying out exerting pressure in gap, shaft shoulder place when solving hot charging in prior art.
The technical solution adopted in the present invention is, a kind of counter-current of large-scale cover parts hot charging, specifically implements according to following steps:
Before step 1, hot charging, determine the air force of adverse current wind regime
First determine the surface coefficient of heat transfer α of cover parts around under natural convection air state, try to achieve the heat dissipation capacity Q of the cover parts under free convection operating mode s, then obtain the size of required wind regime air quantity q;
Step 2, according to technological requirement to cover parts heating, insulation after, cover parts is taken out from heating furnace, is placed on support;
Step 3, supporting axle from up to down to be inserted in cover parts, ensure that the shaft shoulder place of cover parts is very close to each other;
Step 4, the airflow value determined according to step 1 blow, and make air from up to down flowing around cover parts produce adverse current, cooling cover parts until normal temperature state.
The invention has the beneficial effects as follows:
1) adopt counter-current assembling hot-assembling method simple.Tradition hot-assembling method needs large-tonnage forcing press to coordinate, and is subject to strict restriction, and has very high requirement of strength to the support of lower support part to the profile of part.Counter-current hot charging, owing to exerting pressure without the need to forcing press, is saved equipment, and is not also had specific intensity requirement to bottom ground and support.
2) cooling characteristics of cover parts is constant.Because the heat that wind is taken away is just close to the heat distributed of part under nature, so cooling velocity is substantially constant, ensure that the intensity of material, tenacity properties and this characteristic when traditional method hot charging are consistent substantially.
Accompanying drawing explanation
Fig. 1 is the installation site structural representation of existing assembly method;
Fig. 2 is the installation site schematic diagram of the inventive method embodiment.
In figure, 1. support, 2. cover parts, 3. axle, 4. deflector.
Detailed description of the invention
With reference to Fig. 1, existing large-scale cover parts adopts interference fit, and due to the free convection of cover parts 2 surrounding air, after heating, the flow direction of large-scale cover parts 2 surrounding air is from bottom to top.
With reference to Fig. 2, it is the counter-current of large-scale cover parts hot charging of the present invention, its operation principle is, the wind regime of an adjustable wind speed is added above large-scale cover parts 2, force air around cover parts, produce adverse current from top to bottom, the upper part of cover parts is first held tightly and forms location, thermal strain on such h direction would not have an impact to the shaft shoulder place of large-scale cover parts, also zero clearance, shaft shoulder place can just be realized, improve the installation accuracy of cover parts, this method is called the counter-current of hot charging according to operation principle, meet vertically completely, level, the various installation operating mode Lower shaft sleeve class part hot charging assemblings of tilting.
When Model For The Bush-axle Type Parts is not vertical placement but horizontal direction placement is assembled, counter-current of the present invention also can be applied, by arranging the wind regime of an adjustable wind speed above Model For The Bush-axle Type Parts shaft shoulder one end, accelerate the cooling velocity of shaft shoulder one end, shaft shoulder place is first held tightly, thus realizes the installation location of cover parts 2.
For the feature of the large-scale cover parts 2 of difference in practical operation, determining air quantity through calculating, reaching the gap of eliminating shaft shoulder place, improve the requirement of installation accuracy; And make cover parts 2 reach effect close to cooling naturally in air, improve hot charging quality.
For irregular cover parts, in order to the better side at cover parts 2 forms adverse current, as Fig. 2, the deflector 4 of bell-mouth structure of air can be increased on wind regime passage, make air fully flow to the side of cover parts 2.
The concrete implementation step of the inventive method is:
Step 1, before hot charging, determine adverse current wind regime airflow value
First determine the surface coefficient of heat transfer α of cover parts around under natural convection air state, draw the heat dissipation capacity Q of the cover parts under free convection operating mode s, then the size of wanted wind regime air quantity q value is tried to achieve according to formula (2);
Along with the temperature of cover parts reduces, heat radiation reduces thereupon, the air quantity also corresponding reduction required, calculate different grades according to formula (1), (2), in practical operation, divide several gradient successively to reduce air quantity, gradient is got more, the effect of adverse current hot-assembling method is better, utilize existing alternating frequency conversion technique effectively can regulate air quantity, realize air quantity gradient and divide
Surface coefficient of heat transfer α obtains according to existing related data, or according to free convection criteria equation, draws nusselt number, then calculates according to characteristic size, the heat dissipation capacity Q of cover parts scomputing formula is:
Q S = αS ( t 1 - t 0 ) , - - - ( 1 )
Wherein, S-cover parts area of dissipation;
α-surface coefficient of heat transfer;
T 1the temperature of-cover parts;
T 0-environment temperature,
The air quantity q computing formula of wind regime is:
q = Q s ρ c f ( θ 1 f - θ 0 ) η f (unit is m 3/ s), (2)
Wherein, C f-air specific heat capacity at constant pressure, preferred value is C f≈ 1004J/ (kg ° of C),
η fthe usage factor of-blowing, preferred value is η f≈ 0.8,
θ 1 f-blow over cover parts after discharge the temperature of air-flow, θ 1 f0+ (3 ~ 6) ° C,
ρ-dry air density.
Step 2, according to technological requirement, cover parts 2 heated, be incubated after, taken out from heating furnace by cover parts 2, be placed on support 1, support plays the effect being convenient to installation shaft;
Step 3, supporting axle 3 from up to down to be inserted in cover parts 2, ensure that the shaft shoulder place of cover parts 2 does not have assemblage gap;
Step 4, the airflow value determined according to step 1 blow, and adopt auxiliary deflector 4 as required, force air from up to down flow generation adverse current along cover parts 2, for cooling cover parts 2, until normal temperature state.
Cover parts 2 hot charging is complete, checks the installation quality of cover parts in addition according to technological requirement.

Claims (4)

1. a counter-current for large-scale cover parts hot charging, is characterized in that, specifically implement according to following steps:
Before step 1, hot charging, determine the air force of adverse current wind regime:
First determine the surface coefficient of heat transfer α of cover parts around under natural convection air state, try to achieve the heat dissipation capacity Q of the cover parts under free convection operating mode s, then obtain the size of required wind regime air quantity q;
Step 2, according to technological requirement to cover parts (2) heating, insulation after, cover parts (2) is taken out from heating furnace, is placed on support (1);
Step 3, supporting axle (3) is from up to down inserted in cover parts (2), ensure that the shaft shoulder place of cover parts (2) is very close to each other;
Step 4, the airflow value determined according to step 1 blow, and make air produce adverse current along cover parts (2) from up to down flowing around, cooling cover parts (2) until normal temperature state.
2. the counter-current of large-scale cover parts hot charging according to claim 1, it is characterized in that: in described step 1, the deterministic process of wind regime air quantity q is: calculate different air quantity grades according to formula (1), (2), and divide several gradient successively to reduce air quantity in practical operation, realize air quantity gradient to divide
Surface coefficient of heat transfer α obtains according to related data, or according to free convection criteria equation, draws nusselt number, then calculates according to characteristic size, the heat dissipation capacity Q of cover parts (2) scomputing formula is:
Q S=αS(t 1-t 0), (1)
Wherein, S-cover parts area of dissipation;
α-surface coefficient of heat transfer;
T 1the temperature of-cover parts;
T 0-environment temperature,
The computing formula of wind regime air quantity q is:
q = Q s ρ c f ( θ 1 f - θ 0 ) η f , - - - ( 2 )
Wherein, the unit of wind regime air quantity q is m 3/ s,
C f-air specific heat capacity at constant pressure,
η fthe usage factor of-blowing,
θ 1 fthe temperature that-wind is discharged after blowing over cover parts,
θ 0expression wind blows over the temperature before cover parts;
ρ-dry air density.
3. the counter-current of large-scale cover parts hot charging according to claim 2, is characterized in that: in described formula (2), parameter value selects C f≈ 1004J/ (kg DEG C), η f≈ 0.8, θ 1 f0+ (3 ~ 6) DEG C.
4. the counter-current of large-scale cover parts hot charging according to claim 1, is characterized in that: the passage at described adverse current wind regime place is provided with deflector (4).
CN201310087489.6A 2013-03-19 2013-03-19 Reverse flow method for shrinkage fitting of large sleeve type part Expired - Fee Related CN103182621B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310087489.6A CN103182621B (en) 2013-03-19 2013-03-19 Reverse flow method for shrinkage fitting of large sleeve type part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310087489.6A CN103182621B (en) 2013-03-19 2013-03-19 Reverse flow method for shrinkage fitting of large sleeve type part

Publications (2)

Publication Number Publication Date
CN103182621A CN103182621A (en) 2013-07-03
CN103182621B true CN103182621B (en) 2015-04-22

Family

ID=48674196

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310087489.6A Expired - Fee Related CN103182621B (en) 2013-03-19 2013-03-19 Reverse flow method for shrinkage fitting of large sleeve type part

Country Status (1)

Country Link
CN (1) CN103182621B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103934628B (en) * 2014-04-25 2016-06-08 南车洛阳机车有限公司 Internal combustion, continuous current locomotive wheel is to the substep compaction apparatus in axle suspension bearing box assembling

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6025620A (en) * 1983-07-22 1985-02-08 Hitachi Ltd Shrink fit method for sleeve-type reinforced roll
DE3643651A1 (en) * 1986-12-17 1988-06-30 Steuer Mess Regel Armaturen Gm Process for the production of a shrink joint between at least two workpieces comprising materials with different expansion coefficients
CN1151932A (en) * 1995-09-13 1997-06-18 出光石油化学株式会社 Multi-layer structure roller and method for producing the same
EP0830917A1 (en) * 1996-09-20 1998-03-25 Marquart, Ingeborg Chuck for clamping a tool on a machine tool and device for clamping tools by shrink fitting
WO2008047378A2 (en) * 2006-01-30 2008-04-24 Tema India Limited A process of fitting a shrink ring

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6025620A (en) * 1983-07-22 1985-02-08 Hitachi Ltd Shrink fit method for sleeve-type reinforced roll
DE3643651A1 (en) * 1986-12-17 1988-06-30 Steuer Mess Regel Armaturen Gm Process for the production of a shrink joint between at least two workpieces comprising materials with different expansion coefficients
CN1151932A (en) * 1995-09-13 1997-06-18 出光石油化学株式会社 Multi-layer structure roller and method for producing the same
EP0830917A1 (en) * 1996-09-20 1998-03-25 Marquart, Ingeborg Chuck for clamping a tool on a machine tool and device for clamping tools by shrink fitting
WO2008047378A2 (en) * 2006-01-30 2008-04-24 Tema India Limited A process of fitting a shrink ring

Also Published As

Publication number Publication date
CN103182621A (en) 2013-07-03

Similar Documents

Publication Publication Date Title
CN206339360U (en) A kind of arc tunnel treadmill test model support
CN109506876B (en) Temperature layer junction simulation device and method in atmospheric boundary layer environment wind tunnel
CN103182621B (en) Reverse flow method for shrinkage fitting of large sleeve type part
CN205255529U (en) Be applied to wind -guiding heat radiation structure of 3D printer
CN107526868A (en) A kind of Thermal design for radar electric cabinet system
CN203427246U (en) Movable type draught fan cooling device
CN205952464U (en) Automatic capper of chrysanthemum tea
Renze et al. Large-eddy simulation of film cooling flow ejected in a shallow cavity
CN102230638B (en) Hot wind convection type microwave oven
CN203817348U (en) Mold disk baking bracket
CN204749531U (en) Laser coding machine
CN203452830U (en) Tunnel natural ventilation cooling structure
CN203629782U (en) Large-power power electronic module thermal test platform
CN207113338U (en) A kind of electronic device production and processing cooling frame
CN205152283U (en) Heat treating equipment complex air adjusting device
CN205917301U (en) Novel aluminum foil annealing furnace stove bottom device
CN205074359U (en) Wire rod control cooling device that possesses online recovery function
CN204244096U (en) A kind of parallel air duct rectifier bridge
CN202030794U (en) Hot extrusion online wind cooling quenching unit
CN215601623U (en) Novel electrical component assembly with heating member
CN207585369U (en) A kind of aluminium is quickly cooled down platform
CN203550535U (en) Safe and stable trolley type resistance furnace
CN103407049A (en) Movable fan cooling device
CN202988969U (en) Novel die for machining toughened glass
CN206765400U (en) Composite core pultrusion electromagnetism solidification equipment

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150422