CN105414884A - Method for replacing pin roll of external adjustment sheet - Google Patents

Method for replacing pin roll of external adjustment sheet Download PDF

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Publication number
CN105414884A
CN105414884A CN201510745362.8A CN201510745362A CN105414884A CN 105414884 A CN105414884 A CN 105414884A CN 201510745362 A CN201510745362 A CN 201510745362A CN 105414884 A CN105414884 A CN 105414884A
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CN
China
Prior art keywords
locking
pin
bearing pin
support
adjustment sheet
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
CN201510745362.8A
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Chinese (zh)
Other versions
CN105414884B (en
Inventor
齐歆霞
蓝天霞
王晓梅
朱光远
孙文岩
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.)
AECC Shenyang Liming Aero Engine Co Ltd
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Shenyang Liming Aero Engine Group Co Ltd
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Publication date
Application filed by Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201510745362.8A priority Critical patent/CN105414884B/en
Publication of CN105414884A publication Critical patent/CN105414884A/en
Application granted granted Critical
Publication of CN105414884B publication Critical patent/CN105414884B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P11/00Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for 
    • B23P11/02Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for  by first expanding and then shrinking or vice versa, e.g. by using pressure fluids; by making force fits
    • B23P11/025Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for  by first expanding and then shrinking or vice versa, e.g. by using pressure fluids; by making force fits by using heat or cold

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Drilling And Boring (AREA)

Abstract

The invention discloses a method for replacing a pin roll of an external adjustment sheet. The method comprises the following specific steps: step 1, clamping the external adjustment sheet with a to-be-replaced pin roll onto a clamp, drilling off a locking pin by use of a drill bit, and taking out the pin roll with abrasion exceeding standards from the bracket; step 2, clearing an inner cavity of a mounting hole in a bracket; step 3, measuring the diameter of the mounting hole in the bracket; step 4, processing out a locking hole with a corresponding size in the pin roll; step 5, placing the processed pin roll into the mounting hole of the bracket, and aligning the locking hole in the pin roll to the locking hole in the bracket; step 6, selecting the corresponding locking pin, cooling the locking pin for 15-10 minutes in liquid-state nitrogen, then, pressing the locking pin into the locking holes of the bracket and the pin roll, and locking the pin roll on the bracket; and step 7, locking a combined part of the locking pin and the bracket. By replacing the pin roll without damaging a component main body, a using function of the component can be recovered, so that the repair problem of the external adjustment sheet is solved, scrapping of the external adjustment sheet is avoided, and the repair cost is reduced.

Description

The method of bearing pin changed by a kind of outer adjustment sheet
Technical field:
The present invention relates to technical field of engine overhaul, be specifically related to a kind of method that bearing pin changed by outer adjustment sheet.
Background technology:
The outer adjustment sheet of spout is the extension of fuselage, ensures seamlessly transitting of fuselage and jet pipe, time uniform stream flow through afterbody, reduce airplane tail group resistance.The structure of outer adjustment sheet as shown in Figure 1, Figure 2, Figure 3 shows, outer adjustment sheet 4 rear end is provided with support 3, bearing pin 2 is sleeved in the installing hole on support 3, and bearing pin 2 is locked on support 3 by locking pin 1, outer adjustment sheet is by the up and down adjustment that realize self of rear end bearing pin in the installing hole of support, due to the deviation from circular from of nozzle exit, bearing pin is is very easily worn and torn in installing hole, causes part rejection.Normal manufacturing process reinstalls outer adjustment sheet after locking pin and bearing pin are fitted into support.But finished product needs to destroy outer adjustment sheet as repaired according to process for making, and cost is too high, and repairing is worth little.
Summary of the invention:
The object of this invention is to provide a kind of method that bearing pin changed by outer adjustment sheet, the replacing that part main body just realizes wearing and tearing bearing pin can not be destroyed.
For achieving the above object, the present invention is by the following technical solutions:
The method of bearing pin changed by a kind of outer adjustment sheet provided by the invention, and concrete steps are as follows:
Step 1, by the outer adjustment sheet clamping of bearing pin to be replaced on fixture, fix the support of outer adjustment sheet rear end, adjustment drill bit, the locking hole center on alignment support, removes locking pin by bit drills, takes out from the installing hole of support the bearing pin wearing and tearing and exceed standard;
Step 2, the installing hole inner chamber on support to be cleaned out;
The diameter of installing hole on step 3, measurement support;
Step 4, choose the bearing pin of correspondingly-sized according to measurement result, simultaneously according to the size of locking hole on support, bearing pin process the locking hole of correspondingly-sized, and get rid of limit, locking hole hole on bearing pin burr and to locking hole sharp edge rounding;
Step 5, the bearing pin that processes in step 4 to be loaded in the installing hole of support, and adjust the locking hole on bearing pin and the locking hole on support aligns;
Step 6, according to the corresponding locking pin of locking hole selection of dimension, cool locking pin 15-10 minute in liquid nitrogen after, be pressed in the locking hole of support and bearing pin, make lock clasp on support;
Step 7, the junction of locking pin and support to be locked.
Adopt punching pin and compressed air to the installing hole inner chamber cleaning on support in described step 2.
The locking hole that drill bit and reamer drill and ream out on bearing pin on drilling machine is used in described step 4.
In shown step 6, rear for cooling locking pin is pressed in the locking hole of support and bearing pin by use hammer and plug.
Beat punching point with the junction of punching pin at locking pin and support or adopt the locking of " ball closing in " method with plug in described step 7.
Described drill bit drilling speed is 300 ~ 500r/min, and the amount of feeding is 0.056 ~ 0.16mm/r.
Beneficial effect of the present invention: change the using function that bearing pin can recover part by not destroying part main body, effectively can solve the problem that in part, damaged parts is changed, repairing for part provides economy, efficiently method, be applied in the processing of part, implementation result is fine, both solved the reparation problem of outer adjustment sheet, and avoided scrapping of outer adjustment sheet, reduce repair cost.
Accompanying drawing illustrates:
Fig. 1 is the structural representation of outer adjustment sheet;
Fig. 2 is the structural representation of outer adjustment sheet upper bracket;
Fig. 3 be in Fig. 1 P to schematic cross-section;
1-locking pin, 2-bearing pin, 3-support, the outer adjustment sheet of 4-.
Detailed description of the invention:
Below in conjunction with embodiment, the present invention is described in further detail.
The method of bearing pin changed by a kind of outer adjustment sheet of the present invention, and concrete steps are as follows:
Step 1, by the outer adjustment sheet clamping of bearing pin to be replaced on fixture, fix the support of outer adjustment sheet rear end, adjustment drill bit, the locking hole center on alignment support, removes locking pin by bit drills, takes out from the installing hole of support the bearing pin wearing and tearing and exceed standard;
Installing hole inner chamber on support is cleaned out by step 2, employing punching pin and compressed air;
The diameter of installing hole on step 3, measurement support;
Step 4, choose the bearing pin of correspondingly-sized according to measurement result, simultaneously according to the size of locking hole on support, bearing pin uses drill bit and reamer to drill and ream out on drilling machine the locking hole of correspondingly-sized on bearing pin, and get rid of limit, locking hole hole on bearing pin burr and to locking hole sharp edge rounding;
Step 5, the bearing pin that processes in step 4 to be loaded in the installing hole of support, and adjust the locking hole on bearing pin and the locking hole on support aligns;
Step 6, according to the corresponding locking pin of locking hole selection of dimension, be pressed in the locking hole of support and bearing pin, by lock clasp on support with hammer and plug cool locking pin 15-10 minute in liquid nitrogen after;
Step 7, to beat punching point with punching pin in the junction of locking pin and support or adopt " ball closings in " method to lock with plug;
Step 8, inspection
The mated condition of visual examination bearing pin and support, under the prerequisite do not moved axially, allows slight swing and angle to move, and checks assembling place, checks the junction of locking pin and support, do not allowed crackle with magnifying glass (10 times).
Described drill bit drilling speed is 300 ~ 500r/min, and the amount of feeding is 0.056 ~ 0.16mm/r, allows hand feed.
Finally should be noted that: above embodiment is only in order to illustrate that technical scheme of the present invention is not intended to limit, although with reference to above-described embodiment to invention has been detailed description, those of ordinary skill in the field are to be understood that: still can modify to the specific embodiment of the present invention or equivalent replacement, and not departing from any amendment of spirit and scope of the invention or equivalent replacement, it all should be encompassed in the middle of this right.

Claims (6)

1. a method for bearing pin changed by outer adjustment sheet, it is characterized in that: concrete steps are as follows:
Step 1, by the outer adjustment sheet clamping of bearing pin to be replaced on fixture, fix the support of outer adjustment sheet rear end, adjustment drill bit, the locking hole center on alignment support, removes locking pin by bit drills, takes out from the installing hole of support the bearing pin wearing and tearing and exceed standard;
Step 2, the installing hole inner chamber on support to be cleaned out;
The diameter of installing hole on step 3, measurement support;
Step 4, choose the bearing pin of correspondingly-sized according to measurement result, simultaneously according to the size of locking hole on support, bearing pin process the locking hole of correspondingly-sized, and get rid of limit, locking hole hole on bearing pin burr and to locking hole sharp edge rounding;
Step 5, the bearing pin that processes in step 4 to be loaded in the installing hole of support, and adjust the locking hole on bearing pin and the locking hole on support aligns;
Step 6, according to the corresponding locking pin of locking hole selection of dimension, cool locking pin 15-10 minute in liquid nitrogen after, be pressed in the locking hole of support and bearing pin, make lock clasp on support;
Step 7, the junction of locking pin and support to be locked.
2. the method for bearing pin changed by a kind of outer adjustment sheet according to claim 1, it is characterized in that: adopt punching pin and compressed air to the installing hole inner chamber cleaning on support in described step 2.
3. the method for bearing pin changed by a kind of outer adjustment sheet according to claim 1, it is characterized in that: use the locking hole that drill bit and reamer drill and ream out on bearing pin on drilling machine in described step 4.
4. the method for bearing pin changed by a kind of outer adjustment sheet according to claim 1, it is characterized in that: in shown step 6, use hammer and plug are by the locking hole of locking pin press-in support and bearing pin after cooling.
5. the method for bearing pin changed by a kind of outer adjustment sheet according to claim 1, it is characterized in that: beat punching point with the junction of punching pin at locking pin and support or adopt the method locking of ball closing in plug in described step 7.
6. the method for bearing pin changed by a kind of outer adjustment sheet according to claim 1 or 3, and it is characterized in that: described drill bit drilling speed is 300 ~ 500r/min, the amount of feeding is 0.056 ~ 0.16mm/r.
CN201510745362.8A 2015-11-04 2015-11-04 A kind of method that outer adjustment sheet changes bearing pin Active CN105414884B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510745362.8A CN105414884B (en) 2015-11-04 2015-11-04 A kind of method that outer adjustment sheet changes bearing pin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510745362.8A CN105414884B (en) 2015-11-04 2015-11-04 A kind of method that outer adjustment sheet changes bearing pin

Publications (2)

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CN105414884A true CN105414884A (en) 2016-03-23
CN105414884B CN105414884B (en) 2017-11-21

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111745430A (en) * 2020-06-19 2020-10-09 一飞智控(天津)科技有限公司 Rotor wing transmission mechanism assembling method, unmanned aerial vehicle and aircraft

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103157973A (en) * 2011-12-14 2013-06-19 鞍钢股份有限公司 Walking beam swinging pin shaft quick replacement method
CN103495833A (en) * 2013-09-30 2014-01-08 三一重工股份有限公司 Disassembly technology for remanufacturing deformation hinge pin of concrete pump truck
US20140007401A1 (en) * 2012-07-05 2014-01-09 Marinette Marine Corporation Apparatus and method of joining hull plates
CN203817721U (en) * 2013-12-11 2014-09-10 马钢(集团)控股有限公司 Disassembling device for heavy-load hinge pins
DE102013003274A1 (en) * 2013-02-27 2014-09-11 Wink Stanzwerkzeuge Gmbh & Co. Kg Press or punching cylinder and method for its production

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103157973A (en) * 2011-12-14 2013-06-19 鞍钢股份有限公司 Walking beam swinging pin shaft quick replacement method
US20140007401A1 (en) * 2012-07-05 2014-01-09 Marinette Marine Corporation Apparatus and method of joining hull plates
DE102013003274A1 (en) * 2013-02-27 2014-09-11 Wink Stanzwerkzeuge Gmbh & Co. Kg Press or punching cylinder and method for its production
CN103495833A (en) * 2013-09-30 2014-01-08 三一重工股份有限公司 Disassembly technology for remanufacturing deformation hinge pin of concrete pump truck
CN203817721U (en) * 2013-12-11 2014-09-10 马钢(集团)控股有限公司 Disassembling device for heavy-load hinge pins

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111745430A (en) * 2020-06-19 2020-10-09 一飞智控(天津)科技有限公司 Rotor wing transmission mechanism assembling method, unmanned aerial vehicle and aircraft

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Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company

Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City

CP01 Change in the name or title of a patent holder