CN111331167B - Hole machining method based on virtual size of reverse side and special drill jig - Google Patents

Hole machining method based on virtual size of reverse side and special drill jig Download PDF

Info

Publication number
CN111331167B
CN111331167B CN201911299672.6A CN201911299672A CN111331167B CN 111331167 B CN111331167 B CN 111331167B CN 201911299672 A CN201911299672 A CN 201911299672A CN 111331167 B CN111331167 B CN 111331167B
Authority
CN
China
Prior art keywords
positioning
hole
machined
jig
machining
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.)
Active
Application number
CN201911299672.6A
Other languages
Chinese (zh)
Other versions
CN111331167A (en
Inventor
王丙杰
刘平
肖羽丰
万丹
邹雪花
张冬兵
乐美
束飞
拓建峰
万宇
李小游
惠怀龙
姜超
李韶晶
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.)
Jiangxi Hongdu Aviation Industry Group Co Ltd
Original Assignee
Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Jiangxi Hongdu Aviation Industry Group Co Ltd filed Critical Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority to CN201911299672.6A priority Critical patent/CN111331167B/en
Publication of CN111331167A publication Critical patent/CN111331167A/en
Application granted granted Critical
Publication of CN111331167B publication Critical patent/CN111331167B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B35/00Methods for boring or drilling, or for working essentially requiring the use of boring or drilling machines; Use of auxiliary equipment in connection with such methods
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B47/00Constructional features of components specially designed for boring or drilling machines; Accessories therefor
    • B23B47/28Drill jigs for workpieces

Landscapes

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

Abstract

The invention provides a hole processing method taking a virtual size of a back surface as a reference and a special drill jig. According to the hole machining method, a design reference surface (a slide block position surface) and other characteristics of a hole are machined through a numerical control machine tool, a process reference hole is machined on the reverse side of the same positioning reference, after a patch is cut off, the process reference hole is used as a first reference in the horizontal direction, the sizes of two large holes are used as a second positioning reference, a drilling jig is fixed and drilled in the vertical direction by using the design reference surface as a reference, and meanwhile, in order to avoid over-positioning, a fixed pin contact surface of the second positioning reference adopts a diamond structure; aiming at the method, a special drilling jig is designed, and the special drilling jig consists of a bottom plate (1), a positioning pin (2) with a diamond structure, a drilling template (3) and a positioning pin (4). The designed drill jig and the proposed high-precision hole machining method can effectively ensure the positioning precision of the hole, and the production efficiency can be ensured because the drill jig is selected for final forming.

Description

Hole machining method based on virtual size of reverse side and special drill jig
Technical Field
The invention belongs to the field of machining, and particularly relates to a hole machining method taking a virtual size of a reverse side as a reference and a special drill jig.
Background
As a method for machining a high-precision hole part, there are generally the following two methods: firstly, a numerical control machine tool is used and holes are directly formed by depending on the precision of the machine tool, but the method easily causes part deformation, and after a process patch is cut off, the position precision of a part hole can not meet the requirement due to the part deformation; secondly, a process patch is cut off after the part is subjected to finish machining, the hole after numerical control machining is used for positioning, and a drilling template is used for making the hole, but the method can only ensure the position of the hole relative to a reference hole, cannot correspond to the design reference size, and has an out-of-tolerance imagination in the actual use process.
Disclosure of Invention
In order to solve the defects of the prior art, the invention provides a hole machining method and a special drill jig by taking the virtual size of the reverse side as a reference, which are suitable for hole making with a reverse reference, so as to ensure the hole position machining precision and improve the machining efficiency.
In order to solve the technical problem, the invention provides a hole processing method taking the virtual size of the back surface as a reference, which comprises the following steps:
step 1: fixing and positioning the parts by adopting a process patch method, and roughly machining the front, back and side surfaces of the parts by using a numerical control machine;
step 2: correcting the positioning reference after heat treatment, and finely machining the front surface, the back surface and the side surfaces of the part by adopting a numerical control machine tool, wherein the stress after the fine machining cannot be completely released due to the existence of a process patch, so that in order to prevent the part from being scrapped due to deformation after the process patch is cut off, the machining parameters during the fine machining are required to be noticed, only a process reference hole is machined on the back surface, and the rest holes are not machined;
step 3: cutting off the patch, and performing stress relief heat treatment to fully eliminate the processing stress and release stress deformation;
step 4: positioning by using a special drill jig and taking the back surface of the part and the process reference holes as references, inserting the diamond-structure positioning pins into the two second reference positioning hole size holes for fixing, and when the diamond-structure positioning pins cannot be inserted at one time, properly rotating and slowly inserting the diamond-structure positioning pins;
step 5: and drilling by using the designed special drill jig.
The special drill jig designed aiming at the method comprises a positioning pin with a diamond structure, a drill plate, a positioning pin and a bottom plate; the bottom plate is horizontally laid and used for placing and fixing parts to be processed; the two positioning pins with the rhombus structures are symmetrically arranged on the left side and the right side of the drill plate and are used for being butted with the two second reference positioning holes of the machined part to fix the machined part; the positioning pin is fixed on the drill plate and used for determining a process reference hole of the machined part.
In the technical scheme, the designed drilling jig and the high-precision hole machining method can effectively guarantee the positioning precision of the holes, the second reference is provided with the two diamond-shaped pins, the second reference can also be used for detecting the deformation of parts, and the drilling jig is selected for final forming, so that the production efficiency can be guaranteed.
Drawings
FIG. 1 is a schematic view of the structure of the drill jig of the present invention.
FIG. 2 is a schematic diagram of a design reference, a process reference hole, a second reference positioning hole and a hole to be made of a machined part according to the present invention.
In FIGS. 1-2: 1. the drilling jig comprises a bottom plate, 2 positioning pins with diamond structures, 3 drilling jig plates, 4 positioning pins.
Detailed Description
The technical solution in the embodiment of the present invention will be clearly and completely described below with reference to fig. 1 and 2.
The invention relates to a hole processing method taking the virtual size of the back surface as a reference and a special drill jig. As shown in figure 1, the designed special jig consists of a bottom plate 1, a positioning pin 2 with a diamond structure, a jig plate 3 and a positioning pin 4.
As shown in figure 2, the design reference surface and other characteristics of the numerical control machine tool machining hole are adopted, the process reference hole is machined on the reverse side of the same positioning reference, and the selected process reference hole is in the positive and negative directions of the design reference, so that the reference deviation caused by part deformation in the rough machining and heat treatment processes can be obviously reduced, and the deviation of selecting the size of the second reference positioning hole or other sizes as the drilling positioning reference is reduced. If the numerical control machine tool is directly adopted for machining, in order to ensure the consistency of the size, the hole needs to be drilled under the condition of keeping the process patch, and the final position precision of the hole is influenced by the deformation caused by machining stress after the patch is cut off.
And after the patch is cut off, fixing the drill jig and drilling holes in the horizontal direction by taking the process reference hole as a first reference and taking the two second reference positioning holes with the large hole size as a second positioning reference and taking the design reference surface as a reference in the vertical direction. In order to avoid over-positioning, the contact surface of the fixing pin of the second reference positioning hole with the large hole size adopts a diamond structure.

Claims (2)

1. A hole machining method based on a virtual size of a reverse side is characterized by comprising the following steps of: the hole machining method comprises the following steps:
step 1: fixing and positioning the parts by adopting a process patch method, and roughly machining the front, back and side surfaces of the parts by using a numerical control machine;
step 2: correcting the positioning reference after heat treatment, adopting a numerical control machine to finish machining the front surface, the back surface and the side surfaces of the part, wherein the slide block surface of the part is the front surface and contains a design reference, the surface of the part needing to be machined is the back surface and contains process reference holes, attention is paid to machining parameters in finish machining, only the process reference holes are machined in the back surface, and the rest holes are not machined;
step 3: cutting off the patch, and performing stress relief heat treatment to fully eliminate the processing stress and release stress deformation;
step 4: positioning by using a special drill jig and taking the back surface of the part and the process reference holes as references, inserting the diamond-structure positioning pins into the two second reference positioning hole size holes for fixing, and when the diamond-structure positioning pins cannot be inserted at one time, properly rotating and slowly inserting the diamond-structure positioning pins;
step 5: and drilling by using the designed special drill jig.
2. A special jig for realizing the hole processing method based on the virtual size of the reverse surface as claimed in claim 1, characterized in that: the special drill jig consists of a bottom plate (1), a positioning pin (2) with a diamond structure, a drill plate (3) and a positioning pin (4); the bottom plate (1) is horizontally laid and used for placing and fixing parts to be processed; the two positioning pins (2) with the rhombus structures are symmetrically arranged on the left side and the right side of the drill plate (3) and are used for being butted with two second reference positioning holes of the machined part to fix the machined part; and the positioning pin (4) is fixed on the drill plate (3) and used for determining a process reference hole of the processed part.
CN201911299672.6A 2019-12-17 2019-12-17 Hole machining method based on virtual size of reverse side and special drill jig Active CN111331167B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911299672.6A CN111331167B (en) 2019-12-17 2019-12-17 Hole machining method based on virtual size of reverse side and special drill jig

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911299672.6A CN111331167B (en) 2019-12-17 2019-12-17 Hole machining method based on virtual size of reverse side and special drill jig

Publications (2)

Publication Number Publication Date
CN111331167A CN111331167A (en) 2020-06-26
CN111331167B true CN111331167B (en) 2021-06-04

Family

ID=71173812

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911299672.6A Active CN111331167B (en) 2019-12-17 2019-12-17 Hole machining method based on virtual size of reverse side and special drill jig

Country Status (1)

Country Link
CN (1) CN111331167B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111958020B (en) * 2020-07-24 2022-11-22 中国航空工业集团公司济南特种结构研究所 Hole making process method combining pre-positioning and secondary accurate positioning
CN114102068B (en) * 2021-12-17 2023-10-03 江西洪都航空工业集团有限责任公司 Processing method and die for support arm part with special-shaped structure

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201446412U (en) * 2009-07-30 2010-05-05 宝鸡石油机械有限责任公司 Novel arc-surface drilling jig
CN102581549A (en) * 2012-03-21 2012-07-18 无锡圣贝尔机电有限公司 Process for fabricating wind-driven generator base
CN103008975A (en) * 2012-11-27 2013-04-03 天长缸盖有限公司 Processing method for fabrication holes in bottom surface and top surface of cylinder cover
CN104384320A (en) * 2014-11-29 2015-03-04 江西洪都航空工业集团有限责任公司 Method for locating connector mould with double curved surfaces
CN204565219U (en) * 2015-04-01 2015-08-19 南车石家庄车辆有限公司 Couple yoke fabrication hole drilling tool
CN104972281A (en) * 2015-07-15 2015-10-14 江西洪都航空工业集团有限责任公司 Machining technology of open structure part
CN205165985U (en) * 2015-12-11 2016-04-20 陈巨根 Jig anchor clamps of processing box part

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2506508B (en) * 2013-08-07 2014-09-10 Rolls Royce Plc A method of forming a perforated composite panel
CN206326095U (en) * 2016-12-20 2017-07-14 内蒙古北方重工业集团有限公司 Thin-walled arc class casting anti-deformation processing model
CN109570924A (en) * 2018-12-03 2019-04-05 江西洪都航空工业集团有限责任公司 A kind of technique patch cutting method of covering class part
CN109866055B (en) * 2019-04-03 2020-12-29 西安飞机工业(集团)有限责任公司 Wing rib positioning and drilling clamp and positioning method
CN110561048A (en) * 2019-09-17 2019-12-13 沃热精密机械(上海)有限公司 auxiliary process-added boss and boss forming process method thereof

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201446412U (en) * 2009-07-30 2010-05-05 宝鸡石油机械有限责任公司 Novel arc-surface drilling jig
CN102581549A (en) * 2012-03-21 2012-07-18 无锡圣贝尔机电有限公司 Process for fabricating wind-driven generator base
CN103008975A (en) * 2012-11-27 2013-04-03 天长缸盖有限公司 Processing method for fabrication holes in bottom surface and top surface of cylinder cover
CN104384320A (en) * 2014-11-29 2015-03-04 江西洪都航空工业集团有限责任公司 Method for locating connector mould with double curved surfaces
CN204565219U (en) * 2015-04-01 2015-08-19 南车石家庄车辆有限公司 Couple yoke fabrication hole drilling tool
CN104972281A (en) * 2015-07-15 2015-10-14 江西洪都航空工业集团有限责任公司 Machining technology of open structure part
CN205165985U (en) * 2015-12-11 2016-04-20 陈巨根 Jig anchor clamps of processing box part

Also Published As

Publication number Publication date
CN111331167A (en) 2020-06-26

Similar Documents

Publication Publication Date Title
CN111331167B (en) Hole machining method based on virtual size of reverse side and special drill jig
CN110605538B (en) Anti-side bending method in long beam part machining process
CN109551178B (en) Method for controlling machining deformation of split case
CN110293252B (en) Machining method for stable closed-angle structure
CN112222497B (en) Method for processing large conical adapter space curved surface on three-axis linkage milling machine
CN103949704B (en) The method for milling of rounding inside and outside the aperture of a kind of conical shell profiled holes on the surface
CN109531158B (en) Integrated machining method for special-shaped joint of aircraft engine boosting fuel main pipe
CN104955613A (en) Method for grinding drill bit
CN105196009A (en) Machining method of bottom surface and positioning hole of bottom surface of engine body of multi-cylinder engine
CN112171198B (en) Machining method of grid structure part
CN103978105A (en) Coverage piece female mold and machining and assembling method thereof
CN110877119A (en) Machining method for sealing groove on aircraft fuel tank part
CN112658720A (en) Positioning tool and positioning method for quickly clamping inner cavities of left and right side beams
CN103753141A (en) Method and special fixture for glass mould cylindrical machining
CN203621976U (en) Auxiliary device for water pump blade numerical control machining
CN105312645A (en) Method for machining thin web titanium alloy edge strip
CN104588983A (en) Machining method for mold with protrusion
CN108723723A (en) A kind of laser-beam drilling machine vaccum bench production method and vaccum bench
CN110977070B (en) Fixing device and method for blade tenon in linear cutting
CN204366565U (en) Oblique adjusting v block
CN111496481A (en) Precision machining method for thrust surface of crankshaft hole of high-power high-speed diesel engine body
CN105081709A (en) Machining method for large bent top tool rest part
CN110877188A (en) Machining method for airplane box part
CN117182215B (en) Electrode assembly and processing method and using method thereof
CN113199220B (en) Mold core machining method

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