CN102829691A - Checking method for three-dimensional combined sample plate of cavity machining part - Google Patents

Checking method for three-dimensional combined sample plate of cavity machining part Download PDF

Info

Publication number
CN102829691A
CN102829691A CN2012103361661A CN201210336166A CN102829691A CN 102829691 A CN102829691 A CN 102829691A CN 2012103361661 A CN2012103361661 A CN 2012103361661A CN 201210336166 A CN201210336166 A CN 201210336166A CN 102829691 A CN102829691 A CN 102829691A
Authority
CN
China
Prior art keywords
model
tangent plane
class machine
sample plate
cavity class
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
CN2012103361661A
Other languages
Chinese (zh)
Other versions
CN102829691B (en
Inventor
张云鹏
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.)
Shenyang Aircraft Industry Group Co Ltd
Original Assignee
Shenyang Aircraft 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 Shenyang Aircraft Industry Group Co Ltd filed Critical Shenyang Aircraft Industry Group Co Ltd
Priority to CN201210336166.1A priority Critical patent/CN102829691B/en
Publication of CN102829691A publication Critical patent/CN102829691A/en
Application granted granted Critical
Publication of CN102829691B publication Critical patent/CN102829691B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention provides a checking method for a three-dimensional combined sample plate of a cavity machining part. A profile sample plate is improved; an integrated sample plate which is composed of the profile sample plate and a reverse sample plate of the profile sample plate is taken; a suitable section sample plate is taken according to the conditions of the change in lateral angles of the part and the structure of the part, so as to form the three-dimensional combined sample plate; and by using the sample plate for checking, the angle can be quickly checked, the thickness of a lateral margin bar and the thickness and position of a rib of the part can be checked together, and the use is more convenient.

Description

The stereo assembled model method of inspection of cavity class machine-made spares
Technical field
The present invention relates to a kind of stereo assembled model method of inspection of cavity class machine-made spares, be used for machinery, aviation, automobile etc. are related to the check of cavity class machine-made spares.
Background technology
In the airplane parts process of manufacture; Can run into a lot of cavity class machine-made spares, they mostly side and bottom surface all have angle, and the part side wall thickness that has neither be uniform; So just give check, the check of especially producing aircraft in batches brings many troubles.
Traditional method of inspection of cavity class machine-made spares is that (web face) got exterior template in this type of part bottom surface, and then chooses suitable angle line by side curved transition situation.Though this method model design and use simply relatively when the check part, need be checked by aids such as bevel protractor and slide calliper rule, if check in enormous quantities, efficient is not high, and is easy to generate and thinks the check mistake.
In addition, utilize laser measuring apparatus to carry out component test in addition, though precision is high, checkability is not high equally.
To think that a kind of method of inspection is more efficiently sought in the check of producing aircraft cavity class machine-made spares in batches imperative to improve check speed and quality inspection.
Summary of the invention
The stereo assembled model method of inspection that the purpose of this invention is to provide a kind of cavity class machine-made spares; It is simple, convenient, fast to operate; Need not use other subsidiary instruments of inspections except that model, still can guarantee quality inspection, and improve efficiency of test.
Technical scheme of the present invention: the stereo assembled model method of inspection of cavity class machine-made spares comprises the steps:
1) gets standard cavity class machine-made spares, get exterior template and anti-model thereof in the bottom surface, constitute the one model by exterior template and anti-model thereof;
2) on the one model, mark part trim line, aperture and rib line, standard cavity class machine-made spares is positioned with trim line;
3) according to part side angle situation of change, get the tangent plane model, the tangent plane model is inserted sidewall;
4) below the tangent plane model, set up inserted sheet, on the one model, set up slot, pegging graft through inserted sheet and slot is fixed on the tangent plane model on the one model;
5) according to the quantity of tangent plane model at the enterprising line number of tangent plane model, and on the one model, make the numbering mark corresponding with the tangent plane model;
6) take off all tangent plane models and standard cavity class machine-made spares, part to be detected is placed on the one model, part to be detected is positioned, test one by one with the tangent plane model then with trim line.
The tangent plane of step 4) The midsagittal plane model will wrap up sidewall fully, and tangent plane model and sidewall stay the technology gap of 0.05mm-0.15mm.
Described tangent plane model adopts the mode of two parts butt joint to combine.
All tangent plane models and one model all have additional lifting hole(eyelet).
Beneficial effect of the present invention: the present invention adopts the stereo assembled model method of inspection can save the auxiliary instruments of inspections such as bevel protractor, slide calliper rule on the one hand; Make check more convenient; Traditional simple exterior template check and the laser measuring apparatus of relying on of checkability improved a lot, can detect part angle, lateral margin thickness, rib thickness and position etc. intuitively in addition; The tangent plane of tangent plane model will wrap up sidewall fully, and tangent plane model and sidewall stay the technology gap of 0.05mm-0.15mm, extracts so that can normally insert; Under the situation that if sidewall thickness is wide at the top and narrow at the bottom or other tangent planes can't insert, the tangent plane model adopts the mode of two parts butt joint to combine; In all models, increase the brill lifting hole(eyelet), can conveniently preserve.
Description of drawings
Fig. 1 is the structural representation of cavity class machine-made spares.
Fig. 2 is the cavity class machine-made spares exterior template by the classic method design.
Fig. 3 is the structural representation of one model.
Fig. 4 follows the example of synoptic diagram for the tangent plane model.
Fig. 5 is for adopting the tangent plane model of docking mode.
Fig. 6 is the checkout procedure synoptic diagram of part to be detected.
Embodiment
The stereo assembled model method of inspection of cavity class machine-made spares comprises the steps:
1) as shown in Figure 1, get standard cavity class machine-made spares, as shown in Figure 3, get exterior template 4 and anti-model 6 thereof in the bottom surface, constitute one model 9 by exterior template 4 and anti-model 6 thereof;
2) continuation is as shown in Figure 3, on one model 9, marks part trim line, aperture and rib line, with trim line standard cavity class machine-made spares is positioned;
3) as shown in Figure 4, according to part side angle situation of change, get tangent plane model 8, tangent plane model 8 is inserted sidewall;
4) below tangent plane model 8, set up inserted sheet 1, on one model 9, set up slot 5, pegging graft with slot 5 through inserted sheet 1 is fixed on tangent plane model 8 on the one model 9;
5) according to the quantity of tangent plane model 8 at tangent plane model 8 enterprising line numbers, and on one model 9, make the numbering mark corresponding with tangent plane model 8;
6) take off all tangent plane models 8 and standard cavity class machine-made spares, as shown in Figure 6, part 10 to be detected is placed on the one model 9, with trim line part 10 to be detected is positioned, test one by one with tangent plane model 8 then.
The tangent plane of step 4) The midsagittal plane model 8 will wrap up sidewall fully, and tangent plane model 8 and sidewall stay the technology gap of 0.1mm.
As shown in Figure 5, described tangent plane model 8 adopts the mode of two parts butt joint to combine.
All tangent plane models 8 all have additional lifting hole(eyelet) 7 with one model 9.
The present invention improves exterior template 4, gets the one model 9 that exterior template 4 and anti-model 6 thereof are formed, and changes and the structure situation of part own according to part side angle simultaneously; Get suitable tangent plane model 8; The stereo assembled model of so just forming, with this model check, not only angle can be come out in quick test; And can also check out part lateral margin bar thickness and rib thickness and position together, use more convenient.

Claims (4)

1. the stereo assembled model method of inspection of cavity class machine-made spares is characterized in that comprising the steps:
1) gets standard cavity class machine-made spares, get exterior template (4) and anti-model (6) thereof in the bottom surface, constitute one model (9) by exterior template (4) and anti-model (6) thereof;
2) on one model (9), mark part trim line, aperture and rib line, standard cavity class machine-made spares is positioned with trim line;
3) according to part side angle situation of change, get tangent plane model (8), tangent plane model (8) is inserted sidewall;
4) set up inserted sheet (1) in the below of tangent plane model (8), on one model (9), set up slot (5), pegging graft with slot (5) through inserted sheet (1) is fixed on tangent plane model (8) on the one model (9);
5) according to the quantity of tangent plane model (8) at the enterprising line number of tangent plane model (8), and on one model (9), make the numbering mark corresponding with tangent plane model (8);
6) take off all tangent plane models (8) and standard cavity class machine-made spares, part to be detected (10) is placed on the one model (9), part to be detected (10) is positioned, use tangent plane model (8) to test one by one then with trim line.
2. the stereo assembled model method of inspection of cavity class machine-made spares as claimed in claim 1 is characterized in that: the tangent plane of step 4) The midsagittal plane model (8) will wrap up sidewall fully, and tangent plane model (8) and sidewall stay the technology gap of 0.05mm-0.15mm.
3. according to claim 1 or claim 2 the stereo assembled model method of inspection of cavity class machine-made spares, it is characterized in that: described tangent plane model (8) adopts the mode of two parts butt joint to combine.
4. the stereo assembled model method of inspection of cavity class machine-made spares as claimed in claim 3 is characterized in that: all tangent plane models (8) and one model (9) all have additional lifting hole(eyelet) (7).
CN201210336166.1A 2012-09-13 2012-09-13 Checking method for three-dimensional combined sample plate of cavity machining part Active CN102829691B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210336166.1A CN102829691B (en) 2012-09-13 2012-09-13 Checking method for three-dimensional combined sample plate of cavity machining part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210336166.1A CN102829691B (en) 2012-09-13 2012-09-13 Checking method for three-dimensional combined sample plate of cavity machining part

Publications (2)

Publication Number Publication Date
CN102829691A true CN102829691A (en) 2012-12-19
CN102829691B CN102829691B (en) 2014-10-29

Family

ID=47332913

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210336166.1A Active CN102829691B (en) 2012-09-13 2012-09-13 Checking method for three-dimensional combined sample plate of cavity machining part

Country Status (1)

Country Link
CN (1) CN102829691B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103203732A (en) * 2013-03-20 2013-07-17 沈阳飞机工业(集团)有限公司 Method for designing slender part sample plate

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3115777A1 (en) * 1980-10-10 1982-05-27 Ibrahim 95126 San Jose Calif. Ibrahimpasic Edge or surface template
CN202350700U (en) * 2011-11-17 2012-07-25 天津欧波精密仪器股份有限公司 Inner bore annular groove sample plate

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3115777A1 (en) * 1980-10-10 1982-05-27 Ibrahim 95126 San Jose Calif. Ibrahimpasic Edge or surface template
CN202350700U (en) * 2011-11-17 2012-07-25 天津欧波精密仪器股份有限公司 Inner bore annular groove sample plate

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
蒋兆宏: "提高样板线切割表面质量的措施", 《煤矿机械》, vol. 27, no. 06, 30 June 2006 (2006-06-30), pages 1056 - 1057 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103203732A (en) * 2013-03-20 2013-07-17 沈阳飞机工业(集团)有限公司 Method for designing slender part sample plate
CN103203732B (en) * 2013-03-20 2015-07-22 沈阳飞机工业(集团)有限公司 Method for designing slender part sample plate

Also Published As

Publication number Publication date
CN102829691B (en) 2014-10-29

Similar Documents

Publication Publication Date Title
CN103847981B (en) A kind of assembling of Double curve degree covering class part and the method for inspection
CN103453851B (en) The detection method of part outline line on a kind of mould tire
CN102954750B (en) Gauge for indirectly measuring inner hole spigot angle of differential bevel gear
CN205664756U (en) Multifunctional checking tool
CN102829691B (en) Checking method for three-dimensional combined sample plate of cavity machining part
CN102109338A (en) Testing method for radian of end cover
CN203053376U (en) Tool for detecting arcs of blade root bosses of gas turbine blade
CN204154246U (en) A kind of taper hole Quick checking tool for depth
CN203964815U (en) A kind of fast detecting hole site cubing
CN202885746U (en) Inner hole seam allowance angle detector for bevel gear
CN201348489Y (en) Tool for detecting shape and positional tolerance of spherical end surface
CN204255257U (en) A kind of rapid measurement device of the small stair degree of depth
CN108917687B (en) Method for detecting tiny cambered surfaces of front edge and rear edge of blade of aero-engine
CN103411495B (en) A kind of method of inspection for ledge and combination model
CN102997809A (en) Device for measuring thicknesses of air inlet and outlet sides of turbine blade
CN206420406U (en) A kind of battery size detects tool
CN204404928U (en) Envelope cubing in the side plate of center
CN205718712U (en) A kind of inlet flange four hole cubing
CN102967210B (en) Crankshaft end-face detecting tool for position degree of connection hole
CN206709754U (en) A kind of verifying attachment of 3D printing accessory size
CN206670536U (en) A kind of detection means of the blade of THR REV leaf grating
CN206638134U (en) A kind of air bag cubing and vehicle steering cubing
CN202304676U (en) Whole set of measuring apparatus for measuring complicated shape and size of a cast
CN204043555U (en) Trim testing tool under vehicle steering
CN203479212U (en) Auxiliary detection tool of resonator shape and dimension

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