CN205243707U - Simple to operate's hydraulic motor - Google Patents

Simple to operate's hydraulic motor Download PDF

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Publication number
CN205243707U
CN205243707U CN201521128383.7U CN201521128383U CN205243707U CN 205243707 U CN205243707 U CN 205243707U CN 201521128383 U CN201521128383 U CN 201521128383U CN 205243707 U CN205243707 U CN 205243707U
Authority
CN
China
Prior art keywords
fuselage
hydraulic motor
installation
mount pad
screw thread
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
CN201521128383.7U
Other languages
Chinese (zh)
Inventor
江海厅
郑丹
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.)
NINGBO BOCLAIN HYDRAULIC Co Ltd
Original Assignee
NINGBO BOCLAIN HYDRAULIC 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 NINGBO BOCLAIN HYDRAULIC Co Ltd filed Critical NINGBO BOCLAIN HYDRAULIC Co Ltd
Priority to CN201521128383.7U priority Critical patent/CN205243707U/en
Application granted granted Critical
Publication of CN205243707U publication Critical patent/CN205243707U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

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  • Motor Or Generator Frames (AREA)

Abstract

The utility model discloses a simple to operate's hydraulic motor, including fuselage, pivot and mount pad, the front end outer lane of fuselage is equipped with the external screw thread, the rear end of external screw thread is equipped with and keeps off the ring, the pivot is installed the front end of fuselage, be equipped with anti -skid pattern in the pivot, the mount pad with the lower extreme of fuselage links to each other, the mount pad lower extreme is equipped with a plurality of shock attenuation sponge strips. The utility model discloses a simple to operate's hydraulic motor novel structure can make things convenient for, nimble in different face -to -face mountings, satisfies the needs under the different assembly condition, and the total still has the absorbing effect in addition.

Description

A kind of hydraulic motor easy for installation
Technical field
The utility model relates to hydraulic motor field, specifically relates to a kind of hydraulic pressure easy for installationMotor.
Background technology
Hydraulic motor is a kind of executive component of hydraulic system, and the liquid that it provides hydraulic pump is pressedPower can change the mechanical energy (torque and rotational speed) of its output shaft into.
Existing hydraulic motor is all generally to install by front end or bottom surface, in useNeed to use the different hydraulic motors that end face is installed according to different installation environments, use square notJust. In addition also there is the problem that vibrations are large in existing hydraulic motor.
Utility model content
(1) technical problem that will solve
The deficiency existing for prior art, the utility model provides a kind of hydraulic pressure easy for installationMotor.
(2) technical scheme
For achieving the above object, the utility model provides a kind of hydraulic motor easy for installation,Comprise fuselage, rotating shaft and mount pad, the front end outer ring of described fuselage is provided with external screw thread, described outsideThe rear end of screw thread is provided with baffle ring, and described rotating shaft is arranged on the front end of described fuselage, in described rotating shaftBe provided with anti-skid design, described mount pad is connected with the lower end of described fuselage, described mount pad lower endBe provided with some damping sponge bars.
Further, also comprise installation end block, described installation end block comprises tube connector and connecting ring,Described tube connector is connected with described connecting ring, and described tube connector is provided with internal thread, described interior spiral shellLine matches with described external screw thread, and described connecting ring is provided with several fixing holes.
Further, described damping sponge bar has three, is evenly distributed on described mount pad lower end.
Further, described baffle ring and described fuselage are cast into one.
Further, described fuselage cover material is stainless steel.
(3) beneficial effect
The hydraulic motor structure novelty that the utility model is easy for installation, can facilitate, use flexiblyDifferent end faces is installed, and meets the needs under different assembled conditions, and total also has in additionThe effect of damping.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model hydraulic motor easy for installation;
Fig. 2 is the structural representation of base in the utility model hydraulic motor easy for installation;
Fig. 3 is the knot that a direction of end block is installed in the utility model hydraulic motor easy for installationStructure schematic diagram;
Fig. 4 installs another direction of end block in the utility model hydraulic motor easy for installationStructural representation.
Wherein, 1 is fuselage, and 2 is rotating shaft, and 3 is external screw thread, and 4 is base, and 5 is baffle ring, 6For damping sponge bar, 7 is tube connector, and 8 is connecting ring, and 9 is fixing hole.
Detailed description of the invention
Below in conjunction with drawings and Examples, detailed description of the invention of the present utility model is done furtherDescribe in detail. Following examples are used for illustrating the utility model, but it is new not to be used for limiting this practicalityThe scope of type.
The structure of a kind of hydraulic motor easy for installation of the present utility model as shown in Figure 1, Figure 2, figure3 and Fig. 4 shown in, comprise fuselage 1, rotating shaft 2 and mount pad 4, the front end of described fuselage 1Outer ring is provided with external screw thread 3, and the rear end of described external screw thread 3 is provided with baffle ring 5, and described rotating shaft 2 is pacifiedBe contained in the front end of described fuselage 1, described rotating shaft 2 is provided with anti-skid design, described mount pad 4Be connected with the lower end of described fuselage 1, described mount pad 4 lower ends are provided with some damping sponge bars 6.Mount pad 4 can be used for installing fuselage 1.
In the present embodiment, also comprise installation end block, described installation end block comprises tube connector 7 HesConnecting ring 8, described tube connector 7 is connected with described connecting ring 8, and described tube connector 7 is provided withInternal thread, described internal thread matches with described external screw thread 3, if described connecting ring 8 is provided withA dry fixing hole 9. When use, tube connector 7 is connected with fuselage 1 front end external screw thread, logicalCrossing fixing hole 9 fixedly mounts.
In the present embodiment, described damping sponge bar 6 has three, is evenly distributed on described installationSeat 4 lower ends.
In the present embodiment, described baffle ring 5 is cast into one with described fuselage 1.
In the present embodiment, described fuselage 1 enclosure material is stainless steel.
The beneficial effects of the utility model: novel structure, can facilitate, use flexibly differentEnd face is installed, and meets the needs under different assembled conditions, and total also has damping in additionEffect.
The above is only preferred embodiment of the present utility model, it should be pointed out that for this skillThe those of ordinary skill in art field, in the prerequisite that does not depart from the utility model know-whyUnder, can also make some improvements and modifications, it is new that these improvements and modifications also should be considered as this practicalityThe protection domain of type.

Claims (5)

1. a hydraulic motor easy for installation, is characterized in that, comprise fuselage (1),Rotating shaft (2) and mount pad (4), the front end outer ring of described fuselage (1) is provided with external screw thread (3),The rear end of described external screw thread (3) is provided with baffle ring (5), described in described rotating shaft (2) is arranged onThe front end of fuselage (1), described rotating shaft (2) is provided with anti-skid design, described mount pad (4)Be connected with the lower end of described fuselage (1), described mount pad (4) lower end is provided with some dampings seaContinuous bar (6).
2. hydraulic motor easy for installation as claimed in claim 1, is characterized in that, alsoComprise installation end block, described installation end block comprises tube connector (7) and connecting ring (8), described inTube connector (7) is connected with described connecting ring (8), and described tube connector (7) is provided with interior spiral shellLine, described internal thread matches with described external screw thread (3), and described connecting ring (8) is provided withSeveral fixing holes (9).
3. hydraulic motor easy for installation as claimed in claim 1, is characterized in that, instituteStating damping sponge bar (6) has three, is evenly distributed on described mount pad (4) lower end.
4. hydraulic motor easy for installation as claimed in claim 1, is characterized in that, instituteState baffle ring (5) and be cast into one with described fuselage (1).
5. hydraulic motor easy for installation as claimed in claim 1, is characterized in that, instituteStating fuselage (1) enclosure material is stainless steel.
CN201521128383.7U 2015-12-30 2015-12-30 Simple to operate's hydraulic motor Expired - Fee Related CN205243707U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201521128383.7U CN205243707U (en) 2015-12-30 2015-12-30 Simple to operate's hydraulic motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201521128383.7U CN205243707U (en) 2015-12-30 2015-12-30 Simple to operate's hydraulic motor

Publications (1)

Publication Number Publication Date
CN205243707U true CN205243707U (en) 2016-05-18

Family

ID=55942790

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201521128383.7U Expired - Fee Related CN205243707U (en) 2015-12-30 2015-12-30 Simple to operate's hydraulic motor

Country Status (1)

Country Link
CN (1) CN205243707U (en)

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
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: 20160518

Termination date: 20171230