CN210566042U - Integrated power takeoff - Google Patents

Integrated power takeoff Download PDF

Info

Publication number
CN210566042U
CN210566042U CN201920817633.XU CN201920817633U CN210566042U CN 210566042 U CN210566042 U CN 210566042U CN 201920817633 U CN201920817633 U CN 201920817633U CN 210566042 U CN210566042 U CN 210566042U
Authority
CN
China
Prior art keywords
power takeoff
output
rear bearing
gear
bearing cover
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
CN201920817633.XU
Other languages
Chinese (zh)
Inventor
王建峰
孟娜
王文瑄
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.)
Shaanxi Fast Auto Drive Group Co Ltd
Original Assignee
Shaanxi Fast Auto Drive 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 Shaanxi Fast Auto Drive Group Co Ltd filed Critical Shaanxi Fast Auto Drive Group Co Ltd
Priority to CN201920817633.XU priority Critical patent/CN210566042U/en
Application granted granted Critical
Publication of CN210566042U publication Critical patent/CN210566042U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • General Details Of Gearings (AREA)

Abstract

The utility model relates to a power takeoff, concretely relates to integrated form power takeoff. The utility model aims at solving the spline power takeoff mode assembly part of current power takeoff output structure more, it is with high costs, have oil leak risk and the difficult technical problem of scene transformation, provide an integrated form power takeoff. The integrated power takeoff comprises a power takeoff shell, a transmission gear, a driving gear, an output shaft, an output bearing and a rear bearing cover, wherein the transmission gear is arranged in the power takeoff shell and meshed with an intermediate gear of an external transmission; the rear bearing cover and the power takeoff shell are integrally processed and formed. The output part of this integrated form power takeoff has reduced the assembly part of power takeoff assembly, practices thrift the cost, and simple structure is convenient for produce, avoids the risk of combining the face oil leak, and the scene is reformed transform easily.

Description

Integrated power takeoff
Technical Field
The utility model relates to a power takeoff, concretely relates to integrated form power takeoff.
Background
The traditional power takeoff output structure provides spline power takeoff and flange power takeoff, wherein the spline power takeoff mode needs to be installed on power takeoff casing 01 and can be used after parts such as rear bearing cap 02, gasket and bolt of output shaft, as shown in fig. 1, rear bearing cap 02 and power takeoff casing 01 of output shaft are fixed through bolted connection, and adopt the gasket to seal on power takeoff casing 01 and the rear bearing cap 02 contact end face of output shaft, the assembly parts are more, the cost is high, and the risk of oil leakage still exists between the rear bearing cap 02 and the power takeoff casing 01 junction surface. When the flange plate output structure (flange plate power take-off) needs to be modified into the spline output structure (spline power take-off) on site, various parts need to be replaced, and the modification on site is difficult.
Disclosure of Invention
The utility model aims at solving the spline power takeoff mode assembly part of current power takeoff output structure more, it is with high costs, have oil leak risk and the difficult technical problem of scene transformation, provide an integrated form power takeoff.
In order to solve the technical problem, the utility model provides a technical solution as follows:
an integrated power takeoff is characterized in that: the transmission gear is arranged in the power takeoff shell and meshed with an intermediate gear of an external transmission, a driving gear coaxially arranged with the driving gear, an output gear meshed with the driving gear, an output shaft in interference fit with an inner ring of the output gear, an output bearing arranged at a shaft shoulder on the right side of the output shaft, and a rear bearing cover arranged on the right side of the output bearing; the rear bearing cover and the power takeoff shell are integrally processed and formed; the output shaft extends out of the rear bearing cover.
Further, the output shaft extends out of the rear bearing cover part to form a spline structure.
Furthermore, an elastic retainer ring is arranged between the output bearing and the rear bearing cover.
The utility model discloses compare the beneficial effect that prior art has:
1. the utility model provides an integrated form power takeoff output structure, it is integrated with the power takeoff casing with the back bearing cap of output shaft, from the power takeoff output structure of taking the back bearing cap interface. The output part of the integrated power takeoff reduces the assembly parts of the power takeoff assembly, saves cost, has a simple structure, is convenient to produce, saves the assembly of a liner and a rear bearing cover of an output shaft in the assembly process, and is convenient to install; the risk of oil leakage at the joint surface of the rear bearing cover and the power takeoff shell is avoided;
2. the utility model provides an integrated form power takeoff output structure switches the in-process at ring flange output structure and spline output structure, only need install additional or dismantle the ring flange can, greatly made things convenient for the on-the-spot transformation of ring flange power take-off and spline power take-off output structure.
Drawings
FIG. 1 is a schematic diagram of a conventional power takeoff;
fig. 2 is a schematic diagram of the integrated power takeoff structure of the present invention;
description of the reference numerals
In fig. 1:
01-power takeoff casing; 02-rear bearing cap;
in fig. 2:
1-power takeoff shell; 2-a transmission gear; 3-a drive gear; 4-an output gear; 5-an output shaft; 6-output bearing; 7-rear bearing cap; 8-elastic retainer ring.
Detailed Description
The invention will be further described with reference to the accompanying drawings and specific embodiments.
As shown in fig. 2, the integrated power takeoff of the present invention includes a power takeoff housing 1, a transmission gear 2 disposed inside the power takeoff housing 1 and engaged with an intermediate gear of an external transmission, a driving gear 3 disposed coaxially with the transmission gear 2, an output gear 4 engaged with the driving gear 3, an output shaft 5 in interference fit with an inner ring of the output gear 4, an output bearing 6 disposed at a right shoulder of the output shaft 5, and a rear bearing cover 7 disposed at a right side of the output bearing 6; the rear bearing cover 7 and the power takeoff housing 1 are integrally processed and formed; the output shaft 5 extends out of the rear bearing cover 7, and the extending part is of a spline structure. And an elastic retainer ring 8 is arranged between the output bearing 6 and the rear bearing cover 7.
The utility model discloses with the rear bearing cap 7 of output shaft 5 and power takeoff casing 1 integration, from the power takeoff output structure of taking the 7 interfaces of rear bearing cap. The integrated rear power takeoff output structure can effectively reduce power takeoff assembly assembling parts, saves cost, and can avoid the risk of oil leakage of the joint surface of the rear bearing cover 7 and the power takeoff shell 1. The assembly of the gasket and the output shaft rear bearing cap 7 is omitted in the assembly process. In the process of switching the flange and the spline output structure, only the flange plate needs to be additionally installed or detached.
Finally, it should be noted that: the above embodiments are only used for illustrating the technical solutions of the present invention, and not for limiting the same, and it is obvious for a person skilled in the art to modify the specific technical solutions described in the foregoing embodiments or to equally replace some technical features of the embodiments, and these modifications or replacements do not make the essence of the corresponding technical solutions depart from the scope of the technical solutions protected by the present invention.

Claims (3)

1. An integrated form power takeoff which characterized in that: the transmission device comprises a power takeoff shell (1), a transmission gear (2) which is arranged in the power takeoff shell (1) and is meshed with a middle gear of an external transmission, a driving gear (3) which is coaxially arranged with the transmission gear (2), an output gear (4) which is meshed with the driving gear (3), an output shaft (5) which is in interference fit with an inner ring of the output gear (4), an output bearing (6) which is arranged at a shaft shoulder at the right side of the output shaft (5), and a rear bearing cover (7) which is arranged at the right side of the output bearing (6); the rear bearing cover (7) and the power takeoff shell (1) are integrally processed and formed; the output shaft (5) extends out of the rear bearing cover (7).
2. The integrated power take-off of claim 1, wherein: the part of the output shaft (5) extending out of the rear bearing cover (7) is in a spline structure.
3. The integrated power take-off of any one of claims 1 or 2, wherein: and an elastic retainer ring (8) is arranged between the output bearing (6) and the rear bearing cover (7).
CN201920817633.XU 2019-05-31 2019-05-31 Integrated power takeoff Active CN210566042U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920817633.XU CN210566042U (en) 2019-05-31 2019-05-31 Integrated power takeoff

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920817633.XU CN210566042U (en) 2019-05-31 2019-05-31 Integrated power takeoff

Publications (1)

Publication Number Publication Date
CN210566042U true CN210566042U (en) 2020-05-19

Family

ID=70641235

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920817633.XU Active CN210566042U (en) 2019-05-31 2019-05-31 Integrated power takeoff

Country Status (1)

Country Link
CN (1) CN210566042U (en)

Similar Documents

Publication Publication Date Title
CN210566042U (en) Integrated power takeoff
CN204175757U (en) A kind of sealed self-locking nut connection part of anti-leak
CN201240419Y (en) Key tooth type elastic coupling
CN101986518A (en) Sealing and connecting structure for permanent magnet synchronous motor and decelerator of pure electric automobile
CN203272745U (en) Upper transmission case
CN208571129U (en) One kind wearing cylinder connector
CN205036843U (en) Gear box input shaft's seal structure
CN205503925U (en) Wind -powered electricity generation gearbox output shaft seal structure
CN209277997U (en) A kind of high-power internal spline power takeoff assembly of engine
CN210371899U (en) Differential mechanism and drive shaft cooperation oil blanket structure and car
CN211778900U (en) Sealing structure of speed reducer
CN203554145U (en) Water-wading power-taking generator
CN207393467U (en) A kind of gear pump front support drive assembly
CN218267154U (en) Sealed dustproof construction of transfer case output shaft
CN205315664U (en) Integral leading gear reduction unit
CN220204600U (en) Power transmission conversion device with shaft seal
CN214699193U (en) Anti-freezing oil seal
CN213776053U (en) Thrust damping bearing easy to disassemble and assemble
CN213899872U (en) Novel perpendicular cantilever seal structure
CN219796102U (en) Single static ring type mechanical oil seal
CN210153182U (en) Flange mounting clamping structure suitable for pure electric gearbox
CN217824521U (en) Marine motor that waterproof performance is good
CN214661910U (en) Reduction gears for chemical industry stirring
CN219082248U (en) Static ring group structure of water seal of internal combustion engine
CN215267885U (en) Increase journey ware ISG generator seal structure

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant