CN207431775U - A kind of positioning of cylinder body and machining benchmark structure - Google Patents

A kind of positioning of cylinder body and machining benchmark structure Download PDF

Info

Publication number
CN207431775U
CN207431775U CN201721351501.XU CN201721351501U CN207431775U CN 207431775 U CN207431775 U CN 207431775U CN 201721351501 U CN201721351501 U CN 201721351501U CN 207431775 U CN207431775 U CN 207431775U
Authority
CN
China
Prior art keywords
benchmark
reference plane
cylinder body
cylinder
architecture
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
CN201721351501.XU
Other languages
Chinese (zh)
Inventor
赵礼飞
胡必谦
郑久林
高巧
喻昆
兰剑
林欣欣
李贺柱
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.)
Anhui Jianghuai Automobile Group Corp
Original Assignee
Anhui Jianghuai Automobile Group Corp
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 Anhui Jianghuai Automobile Group Corp filed Critical Anhui Jianghuai Automobile Group Corp
Priority to CN201721351501.XU priority Critical patent/CN207431775U/en
Application granted granted Critical
Publication of CN207431775U publication Critical patent/CN207431775U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

The utility model discloses a kind of positioning of cylinder body and machining benchmark structures, Z-direction benchmark architectures of the X to benchmark architecture, for the Y-direction benchmark architecture that defines the Y direction benchmark of cylinder body and for defining the Z-direction benchmark of cylinder body including the X-direction benchmark for being used to define cylinder body, the X are respectively formed at least two reference planes to benchmark architecture, Y-direction benchmark architecture and Z-direction benchmark architecture.Compared with prior art, the utility model by simultaneously set X-direction, three directions of Y direction and Z-direction benchmark architecture, so that benchmark influenced be subject to single rough-cast precision it is smaller, the benchmark architecture in each direction is equipped at least two reference planes, complete the function of clamping and positioning, make machining benchmark unified with positioning datum, effectively increase roughing precision, reduce mismachining tolerance.

Description

A kind of positioning of cylinder body and machining benchmark structure
Technical field
The utility model is related to technical field of engines, the particularly a kind of positioning of cylinder body and machining benchmark structure.
Background technology
Cylinder body is one of engine main parts size, and peripheral bolt hole is mainly used to support, installs engine correlation zero Component, cylinder body cylinder holes are used for providing stroke for piston, and bolt hole and cylinder holes need to machine.Cylinder body processing is divided into roughing and essence Processing, when roughing, need to select rough benchmark, can process finishing benchmark after selecting suitable rough benchmark, ensure cylinder The each mounting surface of body, bolt hole, the position dimension of cylinder holes and precision are correct.
Existing cylinder blank machining benchmark is single, inaccurate, is influenced be subject to cylinder blank casting accuracy big.
Utility model content
The purpose of this utility model is to provide a kind of positioning of cylinder body and machining benchmark structure, to solve prior art middle cylinder The technical issues of chaeta base machining benchmark is single ensures machining accuracy.
The utility model provides a kind of positioning of cylinder body and machining benchmark structure, the X-axis side including being used to define cylinder body Z axis to the X of benchmark to benchmark architecture, for the Y-direction benchmark architecture that defines the Y direction benchmark of cylinder body and for defining cylinder body The Z-direction benchmark architecture of directional reference, the X are respectively formed at least two to benchmark architecture, Y-direction benchmark architecture and Z-direction benchmark architecture Reference plane.
The positioning of cylinder body as described above and machining benchmark structure, these, it is preferred to, the X includes to benchmark architecture First reference plane and the second reference plane, on the outer circumference surface of the cylinder sleeve of the first cylinder of cylinder body outwards projection formation face away from it is described First reference block of the direction extension of first cylinder, it is described that first reference plane is formed at deviating from for first reference block The end face of first cylinder, outwards projection formation faces away from the last position cylinder on the outer circumference surface of the cylinder sleeve of the last position cylinder of the cylinder body Direction extension second reference block, second reference plane be formed at second reference block away from the last position cylinder End face.
The positioning of cylinder body as described above and machining benchmark structure, these, it is preferred to, with the first reference plane phase The first sand cleaning hole is provided at adjacent cylinder upper end face, first reference plane outer surface opposite with first sand cleaning hole is A part for the hole wall of first sand cleaning hole;The second sand removal is provided at the cylinder upper end face adjacent with second reference plane Hole, second reference plane outer surface opposite with second sand cleaning hole are a part for the hole wall of the second sand cleaning hole.
The positioning of cylinder body as described above and machining benchmark structure, these, it is preferred to, first reference plane and second Reference plane is rectangle vertical plane, and length and width are not less than 25mm.
The positioning of cylinder body as described above and machining benchmark structure, these, it is preferred to, the Y-direction benchmark architecture includes 3rd reference plane, the 4th reference plane and the 5th reference plane, the top plate of the cylinder body are equipped with the 3rd reference block in exhaust side convex With the 4th reference block, the 3rd reference plane be formed at the 3rd reference block away from the end face of the top plate, the described 4th Reference plane be formed at the 4th reference block away from the end face of the top plate, the exhaust side of the cylinder body is convexly equipped with the 5th benchmark Block, the 5th reference plane be formed at the 5th reference block away from the end face of the cylinder body.
The positioning of cylinder body as described above and machining benchmark structure, these, it is preferred to, the 3rd reference plane and the 4th Reference plane is rectangular planes, and length is not less than 25mm.
The positioning of cylinder body as described above and machining benchmark structure, these, it is preferred to, the Z-direction benchmark architecture includes 6th reference plane and the 7th reference plane, the bottom plate of the cylinder body are equipped with the 6th reference block and the 7th benchmark in exhaust side convex Block, the 6th reference plane are formed at the top surface of the 6th reference block, and the 7th reference plane is formed at the 7th benchmark The top surface of block.
Compared with prior art, the utility model by setting three X-direction, Y direction and Z-direction directions simultaneously Benchmark architecture so that benchmark influenced be subject to single rough-cast precision it is smaller, the benchmark architecture in each direction be equipped with to Few two reference planes complete the function of clamping and positioning, make machining benchmark unified with positioning datum, effectively increase roughing essence Degree, reduces mismachining tolerance.
Description of the drawings
Fig. 1 is the axonometric drawing of the utility model;
Fig. 2 is the side view of the utility model;
Fig. 3 is the top view of the utility model;
Fig. 4 is the left view of the utility model;
Fig. 5 is the right view of the utility model;
Fig. 6 is the structure diagram of the first reference block;
Fig. 7 is the structure diagram of the second reference block.
Reference sign:1- cylinder bodies, the first reference planes of 2-, the second reference planes of 3-, the first reference blocks of 4-, the second benchmark of 5- Block, the first cylinders of 6-, 7- ends position cylinder, 8- cylinder sleeves, the first sand cleaning holes of 9-, the second sand cleaning holes of 10-, the 3rd reference planes of 11-, 12- the 4th Reference plane, the 5th reference planes of 13-, the 3rd reference blocks of 14-, the 4th reference blocks of 15-, the 5th reference blocks of 16-, the 6th reference planes of 17-, The 7th reference planes of 18-, the 6th reference blocks of 19-, the 7th reference blocks of 20-, 21- top plates, 22- bottom plates.
Specific embodiment
The embodiment of the utility model is described below in detail, the example of the embodiment is shown in the drawings, wherein from beginning Same or similar element is represented to same or similar label eventually or there is same or like element.Below by ginseng The embodiment for examining attached drawing description is exemplary, and is only used for explaining the utility model, and cannot be construed to the utility model Limitation.
Engine in the present embodiment is inline four-cylinder engine, in the other embodiment of the application, engine Cylinder number is changed as needed, has no effect on the realization of the technical solution of the application.
Refer in first cylinder 6 of the present embodiment when in face of attached drawing 1, the cylinder of left end is the first cylinder 6, the gas of right end Cylinder is last position cylinder 7.
As shown in Figure 1, the embodiment of the utility model provides a kind of positioning of cylinder body and machining benchmark structure, including with In Y-direction benchmark architectures of the X to benchmark architecture, for defining the Y direction benchmark of cylinder body 1 for the X-direction benchmark for defining cylinder body 1 With for defining the Z-direction benchmark architecture of the Z-direction benchmark of cylinder body 1, the X is to benchmark architecture, Y-direction benchmark architecture and Z-direction base Quasi- structure is respectively formed at least two reference planes.
X-direction, the benchmark architecture in three directions of Y direction and Z-direction are set simultaneously so that benchmark is subject to single hair The influence of base casting accuracy is smaller, ensure that machining accuracy, the benchmark architecture in each direction is equipped at least two reference planes, complete Into the function of clamping and positioning, make machining benchmark unified with positioning datum, while there is positioning, two kinds of processing, it is fixed clamping Roughing benchmark, 1 blank of roughing cylinder body can be used as while position.
In order to avoid the interference of frock clamp, the roughing of 1 outer end face of cylinder body is influenced, reference plane is arranged in 1 edge of cylinder body Position.
With reference to shown in Fig. 6 and Fig. 7, the X includes the first reference plane 2 and the second reference plane 3 to benchmark architecture, cylinder body 1 Outside projection formation faces away from described the first of the direction extension of first cylinder 6 on the outer circumference surface of the cylinder sleeve 8 of first cylinder 6 Reference block 4, first reference plane 2 be formed at first reference block 4 away from the end face of first cylinder 6, the cylinder body 1 Last position cylinder 7 cylinder sleeve 8 outer circumference surface on outwards projection formation face away from the last position cylinder 7 direction extension described the Two reference blocks 5, second reference plane 3 are formed at the end face for deviating from the last position cylinder 7 of second reference block 5.
First reference plane 2 and the second reference plane 3 are mutually parallel;The center of the cylinder sleeve 8 of first cylinder 6 and the last position cylinder The line of centres of 7 cylinder sleeve 8 is perpendicular to first reference plane 2 and second reference plane 3.
By fixture while the stationary housing 1 on the basis of first reference plane 2 and second reference plane 3, no matter cast When 1 water jacket of cylinder body whether moved compared with cylinder body 1, can ensure processing after cylinder holes uniform wall thickness.
As shown in Figure 4 and Figure 5, the first reference plane 2 and the second reference plane 3 are clamped in order to facilitate fixture, with described first Adjacent 1 upper end surface of cylinder body of reference plane 2 is provided with the first sand cleaning hole 9, first reference plane 2 and first sand cleaning hole 9 Opposite outer surface is a part for the hole wall of the first sand cleaning hole 9;In cylinder body 1 upper surface adjacent with second reference plane 3 Place is provided with the second sand cleaning hole 10, and second reference plane 3 outer surface opposite with second sand cleaning hole 10 is the second sand removal A part for the hole wall in hole 10.
Further, 2 and second reference plane 3 of the first reference plane is rectangle vertical plane, and length and width are not less than 25mm, so as to ensure that frock is clamped using space, front and rear clamping and positioning fixes X-direction.
As depicted in figs. 1 and 2, the Y-direction benchmark architecture includes the 3rd reference plane 11, the 4th reference plane 12 and the 5th benchmark Face 13, the top plate 21 of the cylinder body 1 are equipped with the 3rd reference block 14 and the 4th reference block 15, the 3rd base in exhaust side convex Quasi- face 11 be formed at the 3rd reference block 14 away from the end face of the top plate 21, the 4th reference plane 12 is formed at described 4th reference block 15 away from the end face of the top plate 21, the exhaust side of the cylinder body 1 is convexly equipped with the 5th reference block 16, described Five reference planes 13 be formed at the 5th reference block 16 away from the end face of the cylinder body 1.
3rd reference plane 11, the 4th reference plane 12 and the 5th reference plane 13 are cylinder body 1 exhaust side, 3 vertical blanks respectively Face, 3 reference planes are triangularly arranged, and cylinder body 1 is supported by 3 reference planes, and limit Y direction movement.
For the ease of the clamping and positioning of frock clamp, the 3rd reference plane 11 and the 4th reference plane 12 are put down for rectangle Face, length are not less than 25mm.
With reference to shown in Fig. 1 and Fig. 3, the Z-direction benchmark architecture includes the 6th reference plane 17 and the 7th reference plane 18, the cylinder The bottom plate 22 of body 1 is equipped with the 6th reference block 19 and the 7th reference block 20 in exhaust side convex, and the 6th reference plane 17 is formed In the top surface of the 6th reference block 19, the 7th reference plane 18 is formed at the top surface of the 7th reference block 20.
6th reference plane 17 and the 7th reference plane 18 stretch out cylinder body 1, clamp and position convenient for frock, with the 6th reference plane 17 It is that machining benchmark, the 6th reference plane 17 and the 7th reference plane 18 process Z-direction size for same plane with the 7th reference plane 18, 6th reference plane 17 and 18 line of the 7th reference plane are as X-direction and Y direction blank machining benchmark.
The structure, feature and effect of the utility model are described in detail based on the embodiments shown in the drawings, with Upper described is only the preferred embodiment of the utility model, but the utility model is to limit practical range shown in drawing, it is every according to Change that conception according to the utility model is made or the equivalent embodiment for being revised as equivalent variations, still without departing from specification and figure When showing covered spirit, it should be within the protection scope of the present utility model.

Claims (4)

1. a kind of positioning of cylinder body and machining benchmark structure, it is characterised in that:X-direction base including being used to define cylinder body (1) Zs of the accurate X to benchmark architecture, for the Y-direction benchmark architecture that defines the Y direction benchmark of cylinder body (1) and for defining cylinder body (1) The Z-direction benchmark architecture of direction of principal axis benchmark, the X are respectively formed at least two to benchmark architecture, Y-direction benchmark architecture and Z-direction benchmark architecture A reference plane;The X includes the first reference plane (2) and the second reference plane (3) to benchmark architecture, the first cylinder (6) of cylinder body (1) Outside projection formation faces away from first benchmark of the direction extension of first cylinder (6) on the outer circumference surface of cylinder sleeve (8) Block (4), first reference plane (2) be formed at first reference block (4) away from the end face of first cylinder (6), it is described Outside projection formation faces away from the side of the last position cylinder (7) on the outer circumference surface of the cylinder sleeve (8) of the last position cylinder (7) of cylinder body (1) To second reference block (5) of extension, it is described that second reference plane (3) is formed at deviating from for second reference block (5) The end face of last position cylinder (7);The Y-direction benchmark architecture includes the 3rd reference plane (11), the 4th reference plane (12) and the 5th reference plane (13), the top plate (21) of the cylinder body (1) is equipped with the 3rd reference block (14) and the 4th reference block (15), institute in exhaust side convex State the 3rd reference plane (11) be formed at the 3rd reference block (14) away from the end face of the top plate (21), the 4th benchmark Face (12) be formed at the 4th reference block (15) away from the end face of the top plate (21), the exhaust side of the cylinder body (1) is convex Equipped with the 5th reference block (16), the 5th reference plane (13) be formed at the 5th reference block (16) away from the cylinder body (1) end face;The Z-direction benchmark architecture includes the 6th reference plane (17) and the 7th reference plane (18), the bottom plate of the cylinder body (1) (22) the 6th reference block (19) and the 7th reference block (20) are equipped in exhaust side convex, the 6th reference plane (17) is formed at The top surface of 6th reference block (19), the 7th reference plane (18) are formed at the top surface of the 7th reference block (20).
2. the positioning of cylinder body according to claim 1 and machining benchmark structure, it is characterised in that:With first benchmark Adjacent cylinder body (1) upper end surface in face (2) is provided with the first sand cleaning hole (9), first reference plane (2) and first sand removal The opposite outer surface in hole (9) is a part for the hole wall of the first sand cleaning hole (9);In the cylinder adjacent with second reference plane (3) Body (1) upper end surface is provided with the second sand cleaning hole (10), and second reference plane (3) is opposite with second sand cleaning hole (10) Outer surface is a part for the hole wall of the second sand cleaning hole (10).
3. the positioning of cylinder body according to claim 1 and machining benchmark structure, it is characterised in that:First reference plane (2) and the second reference plane (3) is rectangle vertical plane, and length and width are not less than 25mm.
4. the positioning of cylinder body according to claim 1 and machining benchmark structure, it is characterised in that:3rd reference plane (11) and the 4th reference plane (12) is rectangular planes, and length is not less than 25mm.
CN201721351501.XU 2017-10-19 2017-10-19 A kind of positioning of cylinder body and machining benchmark structure Expired - Fee Related CN207431775U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721351501.XU CN207431775U (en) 2017-10-19 2017-10-19 A kind of positioning of cylinder body and machining benchmark structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721351501.XU CN207431775U (en) 2017-10-19 2017-10-19 A kind of positioning of cylinder body and machining benchmark structure

Publications (1)

Publication Number Publication Date
CN207431775U true CN207431775U (en) 2018-06-01

Family

ID=62292576

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721351501.XU Expired - Fee Related CN207431775U (en) 2017-10-19 2017-10-19 A kind of positioning of cylinder body and machining benchmark structure

Country Status (1)

Country Link
CN (1) CN207431775U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109014788A (en) * 2018-08-30 2018-12-18 安徽江淮汽车集团股份有限公司 A kind of cylinder body processing method
CN111609827A (en) * 2019-02-26 2020-09-01 上汽通用汽车有限公司 Construction method of theoretical precise datum plane of engine cylinder block and engine cylinder block

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109014788A (en) * 2018-08-30 2018-12-18 安徽江淮汽车集团股份有限公司 A kind of cylinder body processing method
CN111609827A (en) * 2019-02-26 2020-09-01 上汽通用汽车有限公司 Construction method of theoretical precise datum plane of engine cylinder block and engine cylinder block
CN111609827B (en) * 2019-02-26 2022-01-11 上汽通用汽车有限公司 Construction method of theoretical precise datum plane of engine cylinder block and engine cylinder block

Similar Documents

Publication Publication Date Title
CN207431775U (en) A kind of positioning of cylinder body and machining benchmark structure
CN105798673A (en) Lathe tool clamp suitable for workpieces of multiple sizes
CN203045361U (en) Spring supporting rotation-clamping floating fixture
CN202780557U (en) Combined fixture for bearing hole in die casting piece
CN204868242U (en) A fixture assembly for engine cylinder block processes location
CN109249069B (en) Step cylinder milling fixture
CN205703322U (en) The hydraulically operated fixture of compatible multi items knuckle processing
CN104196644B (en) A kind of cylinder holes processing positioning method of engine block structure and cylinder body
CN204565714U (en) The location clamping tool of cylinder block end face processing
CN207415127U (en) A kind of grinding machine cylindrical component clamping jig
CN103170904A (en) Cylinder hole center alignment device of honing machine
CN206123247U (en) Pneumatic location frock of housing part machine tooling
CN202008331U (en) Check fixture for three-dimensional bending workpiece
CN211824323U (en) Three-coordinate measuring platform with positioning fixture
CN203018612U (en) Appliance for determining scanning center in mold scanning
CN204694185U (en) A kind of shock insulation rubber bearing position degree detection apparatus
CN203185124U (en) Cylinder hole centering device for honing machine
CN206177161U (en) Detection frock of orthostichous internal -combustion engine organism cylinder spot facing work precision
CN206425851U (en) A kind of three station frock clamps
CN204988095U (en) Oil pump bracket examine utensil
CN204976410U (en) Measure anchor clamps structure
CN105953757B (en) A kind of measurement machine clamp for measure batch
CN205520507U (en) Turbomachinery digital control processing multiple operation anchor clamps
CN103506973A (en) Multi-position clamp for three-coordinate measurement of compressor air cylinder block
CN211728359U (en) Special clamp for machining aero-engine parts

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180601

Termination date: 20201019

CF01 Termination of patent right due to non-payment of annual fee