CN201232021Y - Crankweb self-propelled high-altitude operation platform arm support capable of implementing two arms synchronous amplitude lifting - Google Patents

Crankweb self-propelled high-altitude operation platform arm support capable of implementing two arms synchronous amplitude lifting Download PDF

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Publication number
CN201232021Y
CN201232021Y CNU2008201161744U CN200820116174U CN201232021Y CN 201232021 Y CN201232021 Y CN 201232021Y CN U2008201161744 U CNU2008201161744 U CN U2008201161744U CN 200820116174 U CN200820116174 U CN 200820116174U CN 201232021 Y CN201232021 Y CN 201232021Y
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CN
China
Prior art keywords
arm
rear end
seat
hinged
underarm
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
CNU2008201161744U
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Chinese (zh)
Inventor
刘晓锋
杨昌桂
周海强
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.)
Huacheng Special Machinery Engineering Co Ltd Jiangyin City
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Huacheng Special Machinery Engineering Co Ltd Jiangyin City
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 Huacheng Special Machinery Engineering Co Ltd Jiangyin City filed Critical Huacheng Special Machinery Engineering Co Ltd Jiangyin City
Priority to CNU2008201161744U priority Critical patent/CN201232021Y/en
Application granted granted Critical
Publication of CN201232021Y publication Critical patent/CN201232021Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to an arm support of a crank arm self-propelled high altitude working platform, two arms of the arm support can be lifted with synchronous amplitude. The arm support comprises a revolving platform (1), a lower arm (2), a lower pulling rod (3), a lower linkage base (6), a connecting bar (5), an upper arm (8), an upper pulling rod (7), an upper linkage base (9) and a derricking cylinder (4); the rear end of the lower arm (2) is articulated with the lower part of a shaft seat of the revolving platform (1), the front end thereof is articulated with the lower part of the lower linkage base; the rear end of the lower pulling rod (3) is articulated with the upper part of the shaft seat of the revolving platform (1), the front end thereof is articulated with the lower and middle parts of the lower linkage base (6); the rear end of the upper arm (8) is articulated with the upper part of the lower linkage base (6), the front end thereof is articulated with the lower part of the upper linkage base (9); the rear part of the upper pulling rod (7), which is closed to the position of the rear end, is articulated with the upper and middle parts of the lower linkage base (6), the front end of the upper pulling rod (7) is articulated with the lower part of the upper linkage base (9). The two arms of the arm support can be lifted with synchronous amplitude by only single handle operation in the arm support.

Description

Can realize the self-propelled aerial working platform jib of cranking arm that two arm synchronous amplitudes hoist
Technical field
The utility model relates to a kind of self-propelled aerial working platform, especially relates to a kind of self-propelled aerial working flat-bed jib of cranking arm.Belong to technical field of engineering machinery.
Background technology
The self-propelled aerial working platform of cranking arm is mainly used in and builds the shipping agency industry, the port machine is made industry and construction trade etc.Mainly by chassis, turn table, jib, hang head, work bucket, go up control box, control box, driving engine, electro-hydraulic proportional valve and oil cylinder etc. are formed down.Before the utility model is made, traditional self-propelled aerial working platform of cranking arm all adopts electro-hydraulic proportional valve of an electric ratio handle drives, oil cylinder of electro-hydraulic proportional valve control promotes a jib amplitude-variation hoisting, and this connecting mode mainly has the following disadvantages:
Because the jib of this structure can only be controlled the luffing action of a jib with an electro-hydraulic proportional valve, amplitude oil cylinder and electric ratio handle, control two jibs, just need two electro-hydraulic proportional valves, two amplitude oil cylinder and two electric ratio handles to control the luffing action of two jibs respectively.Realize that two jib synchronous amplitudes hoist, just need both hands to operate two handles simultaneously, not only operation inconvenience, stability neither be fine, and cost is very high.
Summary of the invention
The purpose of this utility model is to overcome above-mentioned deficiency, and a kind of the self-propelled aerial working flat-bed jib of cranking arm that needs single only lever operated just energy two arm synchronous amplitudes to hoist is provided.
The purpose of this utility model is achieved in that the self-propelled aerial working flat-bed jib of cranking arm that a kind of energy two arm synchronous amplitudes hoist, comprise turn table, underarm, lower link, following interlock seat, connecting rod, upper arm, top rod, go up interlock seat and amplitude oil cylinder
The lower hinge of the axle bed on described underarm rear end and the turn table, the front end and the seat lower hinge that links down;
The upper articulation of the axle bed on described lower link rear end and the turn table, front end is with interlock seat middle and lower part is hinged down;
The described upper arm rear end and the seat upper articulation that links down, front end and last interlock seat upper articulation;
Described top rod rear portion is hinged with the seat middle and upper part of linking down near rear end, front end and last interlock seat lower hinge;
Described connecting rod lower end and underarm rear portion are hinged near rear end, and upper end and top rod rear end are hinged;
The cylinder tail and the underarm front portion of described amplitude oil cylinder are hinged, and the piston rod of amplitude oil cylinder and upper arm are hinged near rear end;
Described upper arm, top rod, go up the interlock seat and down the interlock seat constitute a parallel-crank mechanism,
Axle bed on described underarm, lower link, following interlock seat and the turn table constitutes another parallel-crank mechanism.
Principle of work
During as the amplitude-variation hoisting action, the piston rod of amplitude oil cylinder stretches out, and drives upper arm and upwards does the luffing action.Because upper arm and top rod have formed a parallel-crank mechanism by the last interlock seat and the seat that links down, so top rod and upper arm luffing abreast make progress, meanwhile, because top rod links to each other by connecting rod with underarm, underarm and lower link have also formed a parallel-crank mechanism by the axle bed on down interlock seat and the turn table, do the synchronous amplitude action that hoists so drive underarm and lower link simultaneously.
Compare with existing jib, the utlity model has following advantage:
1, generally two jibs is controlled separately owing to traditional self-propelled aerial working platform of cranking arm, so will realize that the difficulty that two arm synchronous amplitudes hoist is bigger, not only to operate two handles simultaneously with two hands, and also very high to operator's technical merit requirement, and stationarity neither be fine.The self-propelled aerial working flat-bed jib of cranking arm that the utility model adopts the energy synchronous amplitude to hoist, can hoist by two jib synchronous amplitudes of an electric ratio handle control, not only simple to operate, and luffing is steady, and normal operations workman just can operate freely.
2, traditional self-propelled aerial working platform of cranking arm just needs two apportioning valves and handle owing to the luffing to jib is control separately, and cost is quite high.The self-propelled aerial working flat-bed jib of cranking arm that the utility model adopts the energy synchronous amplitude to hoist then only needs an apportioning valve and a handle, and this just can save the 8000 yuan of left and right sides costs light.
Description of drawings
The front appearance scheme drawing of the self-propelled aerial working flat-bed jib of cranking arm that Fig. 1 hoists for the related energy two arm synchronous amplitudes of the utility model.
Fig. 2 is the birds-eye view of Fig. 1.
Fig. 3 is A-A cutaway view of Fig. 2.
Among the figure: turn table 1, underarm 2, lower link 3, amplitude oil cylinder 4, connecting rod 5, down interlock seat 6, top rod 7, upper arm 8, go up interlock seat 9.
The specific embodiment
Referring to Fig. 1~3, the utility model is the self-propelled aerial working flat-bed jib of cranking arm that a kind of energy two arm synchronous amplitudes hoist, mainly by turn table 1, underarm 2, lower link 3, down interlock seat 6, connecting rod 5, upper arm 8, top rod 7, go up interlock seat 9 and amplitude oil cylinder 4 is formed.
The lower hinge of the axle bed on described underarm 2 rear ends and the turn table 1, the front end and seat 6 lower hinge that link down;
The upper articulation of the axle bed on described lower link 3 rear ends and the turn table 1, front end is with interlock seat 6 middle and lower parts are hinged down;
Described upper arm 8 rear ends and seat 6 upper articulations that link down, front end and last interlock seat 9 upper articulations;
Described top rod 7 rear portions are hinged with seat 6 middle and upper parts of linking down near rear end, front end and last interlock seat 9 lower hinge;
Described connecting rod 5 lower ends and underarm 2 rear portions are hinged near rear end, and upper end and top rod 7 rear ends are hinged;
The cylinder tail of described amplitude oil cylinder 4 and underarm 2 are anterior hinged, and the piston rod of amplitude oil cylinder 4 and upper arm 8 are hinged near rear end;
Described upper arm 8, top rod 7, go up interlock seat 9 and down interlock seat 6 constitute a parallel-crank mechanism,
Axle bed on described underarm 2, lower link 3, following interlock seat 6 and the turn table 1 constitutes another parallel-crank mechanism.

Claims (1)

1, the self-propelled aerial working flat-bed jib of cranking arm that hoists of a kind of energy two arm synchronous amplitudes, it is characterized in that described jib comprises turn table (1), underarm (2), lower link (3), following interlock seat (6), a connecting rod (5), upper arm (8), top rod (7), goes up interlock (9) and amplitude oil cylinder (4)
The lower hinge of the axle bed on described underarm (2) rear end and the turn table (1), the front end and seat (6) lower hinge that links down;
The upper articulation of the axle bed on described lower link (3) rear end and the turn table (1), front end is with interlock seat (6) middle and lower part is hinged down;
Described upper arm (8) rear end and seat (6) upper articulation that links down, front end and last interlock seat (9) upper articulation;
Described top rod (7) rear portion is hinged with seat (6) middle and upper part of linking down near rear end, front end and last interlock seat (9) lower hinge;
Described connecting rod (5) lower end and underarm (2) rear portion are hinged near rear end, and upper end and top rod (7) rear end is hinged;
The cylinder tail of described amplitude oil cylinder (4) and underarm (2) are anterior hinged, and the piston rod of amplitude oil cylinder (4) and upper arm (8) are hinged near rear end;
Described upper arm (8), top rod (7), go up interlock seat (9) and down interlock seat (6) constitute a parallel-crank mechanism,
Axle bed on described underarm (2), lower link (3), following interlock seat (6) and the turn table (1) constitutes another parallel-crank mechanism.
CNU2008201161744U 2008-05-16 2008-05-16 Crankweb self-propelled high-altitude operation platform arm support capable of implementing two arms synchronous amplitude lifting Expired - Fee Related CN201232021Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2008201161744U CN201232021Y (en) 2008-05-16 2008-05-16 Crankweb self-propelled high-altitude operation platform arm support capable of implementing two arms synchronous amplitude lifting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2008201161744U CN201232021Y (en) 2008-05-16 2008-05-16 Crankweb self-propelled high-altitude operation platform arm support capable of implementing two arms synchronous amplitude lifting

Publications (1)

Publication Number Publication Date
CN201232021Y true CN201232021Y (en) 2009-05-06

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Application Number Title Priority Date Filing Date
CNU2008201161744U Expired - Fee Related CN201232021Y (en) 2008-05-16 2008-05-16 Crankweb self-propelled high-altitude operation platform arm support capable of implementing two arms synchronous amplitude lifting

Country Status (1)

Country Link
CN (1) CN201232021Y (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102485636A (en) * 2010-12-06 2012-06-06 上海微电子装备有限公司 Synchronous lifting component and synchronous lifting and horizontal moving mechanism
CN109665471A (en) * 2019-01-18 2019-04-23 徐州海伦哲特种车辆有限公司 A kind of variable centre of gyration turntable for high-altitude operation vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102485636A (en) * 2010-12-06 2012-06-06 上海微电子装备有限公司 Synchronous lifting component and synchronous lifting and horizontal moving mechanism
CN109665471A (en) * 2019-01-18 2019-04-23 徐州海伦哲特种车辆有限公司 A kind of variable centre of gyration turntable for high-altitude operation vehicle

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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: 20090506

Termination date: 20130516