CN206539390U - Disjunctor fuselage separated oil sump - Google Patents

Disjunctor fuselage separated oil sump Download PDF

Info

Publication number
CN206539390U
CN206539390U CN201720131442.9U CN201720131442U CN206539390U CN 206539390 U CN206539390 U CN 206539390U CN 201720131442 U CN201720131442 U CN 201720131442U CN 206539390 U CN206539390 U CN 206539390U
Authority
CN
China
Prior art keywords
flange face
shell body
disjunctor
oil sump
shell
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
CN201720131442.9U
Other languages
Chinese (zh)
Inventor
梁权
崔丛敏
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.)
Steyr Engine Power (changzhou) Co Ltd
Original Assignee
Steyr Engine Power (changzhou) 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 Steyr Engine Power (changzhou) Co Ltd filed Critical Steyr Engine Power (changzhou) Co Ltd
Priority to CN201720131442.9U priority Critical patent/CN206539390U/en
Application granted granted Critical
Publication of CN206539390U publication Critical patent/CN206539390U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)

Abstract

The utility model discloses a kind of disjunctor fuselage separated oil sump, including left shell and right shell body, described left shell bottom surface has left half flange face, right shell body bottom surface has right half flange face, described left half flange face and right half flange face form the oil pan that storage machine oil is sealedly connected with mounting flange face, mounting flange face after left shell and right shell body positioning mould assembling assembling.The utility model assembled by mould assembling after left shell, right shell body bottom form mounting flange face, individually it is tightly connected the oil pan acted on oil sump, when producing interference or inadequate installation gap in different vehicle, machine oil dish structure only need to be changed, because oil pan is relatively simple for structure, volume is also small compared with left and right housing, therefore can shorten the construction cycle, reduces development cost.

Description

Disjunctor fuselage separated oil sump
Technical field
The utility model is related to technical field of engines, especially a kind of disjunctor fuselage separated oil sump.
Background technology
Disjunctor fuselage oil sump used in available engine, generally by the way of middle subdivision, is connected by left and right housing and closed Into, and the left side of left and right housing bottom and right side are then integrated into the oil sump entirety for being used to store machine oil, the oily bottom Shell bottom protrudes the baseplane of left and right housing, thus when actual use is installed, and the oil sump of engine bottom is often and vehicle Vehicle frame or other parts produce interference or installation gap is inadequate, it is impossible to meet installation requirement.Convention resolution method is according to dry Relate to situation and making is re-molded at least one in left and right housing, even all two will remake sometimes, and this undoubtedly causes The part construction cycle is long, and cost is high, and the generalization degree of parts is relatively low.
Utility model content
The technical problems to be solved in the utility model is:Deficiency in the prior art is overcome simply to change i.e. there is provided a kind of The disjunctor fuselage separated oil sump of different vehicle installation requirement can be met.
The utility model solves the technical scheme that its technical problem used:A kind of disjunctor fuselage is with split type oily bottom Shell, including left shell and right shell body, described left shell bottom surface have left half flange face, and right shell body bottom surface has right half flange Face, described left half flange face and right half flange face form mounting flange face after left shell and right shell body positioning mould assembling assembling, The oil pan of storage machine oil is sealedly connected with mounting flange face.
To ensure the flatness in mounting flange face, the split surface of the described flange face of left shell bottom vertical left half is provided with Alignment pin, is accordingly provided with positioning hole on the split surface of the flange face of right shell body bottom vertical right half.
To ensure on the sealing between oil pan and mounting flange face, described left half flange face and right half flange face It is coated with fluid sealant.
The beneficial effects of the utility model are:The utility model assembled by mould assembling after left shell, right shell body bottom shape Into mounting flange face, the oil pan acted on oil sump is individually tightly connected, produces and interferes when in different vehicle Or install gap it is inadequate when, only need to change machine oil dish structure, because oil pan is relatively simple for structure, the body compared with left and right housing Product is also small, therefore can shorten the construction cycle, reduces development cost.
Brief description of the drawings
The utility model is further illustrated with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is structural representation of the present utility model.
The left right alignment pin of half flange face, 5. oil pan 6. of half flange face 4. of 1. left shell, 2. right shell body 3. in figure
Embodiment
The utility model is further described presently in connection with accompanying drawing.These accompanying drawings are simplified schematic diagram only to show Meaning mode illustrates basic structure of the present utility model, therefore it only shows the composition relevant with the utility model.
A kind of disjunctor fuselage separated oil sump as shown in Figure 1, including left shell 1 and right shell body 2, described left housing The bottom surface of body 1 has left half flange face 3, and the bottom surface of right shell body 2 has right half flange face 4, described left half flange face 3 and right half flange Face 4 forms on mounting flange face, mounting flange face after left shell 1 and the positioning mould assembling assembling of right shell body 2 and is sealedly connected with storage The oil pan 5 of machine oil.
The split surface of the described flange face 3 of 1 bottom vertical left of left shell half is provided with alignment pin 6, accordingly in right shell body 2 The split surface of the flange face 4 of bottom vertical right half is provided with positioning hole.When mould assembling is installed, first in the combination of left shell 1 and right shell body 2 Plane silica gel is applied on face, by the cooperation of alignment pin 6 and positioning hole, left shell 1 and right shell body 2 are tightened to one with bolt Body, the magnitude of misalignment that alignment pin 6 can make left shell 1 and the 2-in-1 case of right shell body relative after installing is maintained in rational scope, so as to Ensure that the flatness in mounting flange face meets the requirements.And before the installation of oil pan 5, it is same first in left half flange face 3 and right half method Applied on blue face 4 after fluid sealant, with bolt by oil pan 5 and the fixed seal connection of mounting flange face.
The utility model assembled by mould assembling after left shell 1, the bottom of right shell body 2 form mounting flange face, individually sealing The oil pan 5 that connection is acted on oil sump, when generation interferes or installed gap inadequate in different vehicle, need to only change Become the structure of oil pan 5, because oil pan 5 is relatively simple for structure, volume is also small compared with left shell 1 and right shell body 2, therefore can be with Shorten the construction cycle, reduce development cost.
Above-mentioned embodiment is only to illustrate technical concepts and features of the present utility model, and its object is to allow be familiar with this skill The personage of art can understand content of the present utility model and be carried out, and protection model of the present utility model can not be limited with this Enclose, all equivalent change or modifications made according to the utility model Spirit Essence should all cover in protection model of the present utility model In enclosing.

Claims (3)

1. a kind of disjunctor fuselage separated oil sump, including left shell (1) and right shell body (2), it is characterized in that:Described left housing Body (1) bottom surface has left half flange face (3), and right shell body (2) bottom surface has right half flange face (4), described left half flange face (3) With right half flange face (4) mounting flange face, mounting flange face are formed after left shell (1) and right shell body (2) positioning mould assembling assembling On be sealedly connected with storage machine oil oil pan (5).
2. disjunctor fuselage separated oil sump according to claim 1, it is characterized in that:Described left shell (1) bottom The split surface of the flange face of vertical left half (3) is provided with alignment pin (6), accordingly in the flange face of right shell body (2) bottom vertical right half (4) split surface is provided with positioning hole.
3. disjunctor fuselage separated oil sump according to claim 1, it is characterized in that:Described left half flange face (3) With right half flange face (4) on be coated with fluid sealant.
CN201720131442.9U 2017-02-14 2017-02-14 Disjunctor fuselage separated oil sump Expired - Fee Related CN206539390U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720131442.9U CN206539390U (en) 2017-02-14 2017-02-14 Disjunctor fuselage separated oil sump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720131442.9U CN206539390U (en) 2017-02-14 2017-02-14 Disjunctor fuselage separated oil sump

Publications (1)

Publication Number Publication Date
CN206539390U true CN206539390U (en) 2017-10-03

Family

ID=59945667

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720131442.9U Expired - Fee Related CN206539390U (en) 2017-02-14 2017-02-14 Disjunctor fuselage separated oil sump

Country Status (1)

Country Link
CN (1) CN206539390U (en)

Similar Documents

Publication Publication Date Title
CN203941956U (en) The hermetically-sealed construction of battery case
CN204344195U (en) A kind of engine sump tank
CN203742826U (en) Automobile engine timing cavity structure
CN204175757U (en) A kind of sealed self-locking nut connection part of anti-leak
CN206539390U (en) Disjunctor fuselage separated oil sump
CN204795966U (en) Engine control ware canning
CN204929480U (en) Engine control unit with seal structure
CN204586689U (en) A kind of glove box of automobile
CN208905265U (en) A kind of water-cool control lid plate
CN202080351U (en) Automobile oil filler fixing cap assembly
CN202007977U (en) Rotor oil pump with internal pump cover
CN202857194U (en) Electric vehicle controller radiating shell
CN201568710U (en) Gear type oil pump integrated with cover housing
CN202790460U (en) Integral gear reducer body
CN109210044B (en) Via hole connector plastic shell mounting structure
CN202047892U (en) Top cover structure of water tank for heat cooling of automobile engine
CN203856580U (en) Single-cylinder engine and rear cover board thereof
CN203050836U (en) Diesel engine oil sump
CN204591473U (en) Novel diesel engine pressurized machine front-end bracket
CN212839306U (en) Gear box body structure
CN220957422U (en) Combined flywheel shell
CN220828504U (en) Main reducer casing assembly that suitability is good
CN201396428Y (en) Gear case sealing structure
CN203047348U (en) Transition plug cover
CN203585361U (en) Controlling valve for automobile exhaust gas recirculation system

Legal Events

Date Code Title Description
GR01 Patent grant
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: 20171003

Termination date: 20220214