CN203161989U - Two-stage cylindrical bevel gear reducer with high-speed tail mechanism - Google Patents

Two-stage cylindrical bevel gear reducer with high-speed tail mechanism Download PDF

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Publication number
CN203161989U
CN203161989U CN 201320077474 CN201320077474U CN203161989U CN 203161989 U CN203161989 U CN 203161989U CN 201320077474 CN201320077474 CN 201320077474 CN 201320077474 U CN201320077474 U CN 201320077474U CN 203161989 U CN203161989 U CN 203161989U
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CN
China
Prior art keywords
speed shaft
high speed
bevel gear
gear reducer
stage cylindrical
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
CN 201320077474
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Chinese (zh)
Inventor
陈惠娜
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Individual
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Individual
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Filing date
Publication date
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Priority to CN 201320077474 priority Critical patent/CN203161989U/en
Application granted granted Critical
Publication of CN203161989U publication Critical patent/CN203161989U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to a reducer, in particular to a two-stage cylindrical bevel gear reducer with a high-speed tail mechanism. The two-stage cylindrical bevel gear reducer comprises a gearbox, a high-speed shaft is arranged in the gearbox, a bevel pinion is arranged at the tail of the high-speed shaft, an oil baffle plate is arranged between the bevel pinion and the high-speed shaft, a cup is sleeved between the high-speed shaft and the gearbox, and bearings are arranged between the two ends of the high-speed shaft and the cup. The two-stage cylindrical bevel gear reducer with the high-speed tail mechanism is simple in structure, and operation efficiency is improved.

Description

The two-stage awl stud wheel retarder of band high speed shaft tail structure
Technical field
The utility model is a kind of retarder, particularly a kind of two-stage awl stud wheel retarder with the high speed shaft tail structure.
Background technique
Reducer structure complexity of the prior art, inefficiency.
Summary of the invention
The utility model mainly is to solve the deficiencies in the prior art, provides a kind of simple in structure, promotes the two-stage awl stud wheel retarder of the band high speed shaft tail structure of working efficiency.
Above-mentioned technical problem of the present utility model is mainly solved by following technical proposals:
A kind of two-stage awl stud wheel retarder with the high speed shaft tail structure, comprise casing, be provided with high speed shaft in the described casing, the afterbody of described high speed shaft is provided with bevel pinion, be provided with oil baffle disc between described bevel pinion and high speed shaft, be provided with a set of cups between described high speed shaft and casing, be respectively equipped with bearing between the two ends of described high speed shaft and a set of cups.
As preferably, described oil baffle disc keeps off mutually with bearing and connecing, and the outer rim of described a set of cups and oil baffle disc distributes separately, and described bevel pinion is located by shaft end ring mutually with high speed shaft.
Therefore, the two-stage of the band high speed shaft tail structure that the utility model provides awl stud wheel retarder, simple in structure, promote working efficiency.
Description of drawings
Fig. 1 is structural representation of the present utility model.
Embodiment
Below by embodiment, and by reference to the accompanying drawings, the technical solution of the utility model is described in further detail.
Embodiment: as shown in Figure 1, a kind of two-stage awl stud wheel retarder with the high speed shaft tail structure, comprise casing 1, be provided with high speed shaft 2 in the described casing 1, the afterbody of described high speed shaft 2 is provided with bevel pinion 3,2 of described bevel pinion 3 and high speed shafts are provided with oil baffle disc 4, and 1 of described high speed shaft 2 and casing are provided with a set of cups 5, and 5 of the two ends of described high speed shaft 2 and a set of cups are respectively equipped with bearing 6.Described oil baffle disc 4 keeps off mutually with bearing 6 and connecing, and described a set of cups 5 distributes separately with the outer rim of oil baffle disc 4, and described bevel pinion 3 is located by shaft end ring 7 mutually with high speed shaft 2.

Claims (2)

1. the two-stage with the high speed shaft tail structure is bored the stud wheel retarder, it is characterized in that: comprise casing (1), be provided with high speed shaft (2) in the described casing (1), the afterbody of described high speed shaft (2) is provided with bevel pinion (3), be provided with oil baffle disc (4) between described bevel pinion (3) and high speed shaft (2), be provided with a set of cups (5) between described high speed shaft (2) and casing (1), be respectively equipped with bearing (6) between the two ends of described high speed shaft (2) and a set of cups (5).
2. the two-stage of band high speed shaft tail structure according to claim 1 is bored the stud wheel retarder, it is characterized in that: described oil baffle disc (4) keeps off mutually with bearing (6) and connecing, described a set of cups (5) distributes separately with the outer rim of oil baffle disc (4), and described bevel pinion (3) is located by shaft end ring (7) mutually with high speed shaft (2).
CN 201320077474 2013-02-19 2013-02-19 Two-stage cylindrical bevel gear reducer with high-speed tail mechanism Expired - Fee Related CN203161989U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201320077474 CN203161989U (en) 2013-02-19 2013-02-19 Two-stage cylindrical bevel gear reducer with high-speed tail mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201320077474 CN203161989U (en) 2013-02-19 2013-02-19 Two-stage cylindrical bevel gear reducer with high-speed tail mechanism

Publications (1)

Publication Number Publication Date
CN203161989U true CN203161989U (en) 2013-08-28

Family

ID=49023175

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201320077474 Expired - Fee Related CN203161989U (en) 2013-02-19 2013-02-19 Two-stage cylindrical bevel gear reducer with high-speed tail mechanism

Country Status (1)

Country Link
CN (1) CN203161989U (en)

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130828

Termination date: 20140219