CN102848871A - Self-propelled aerial working platform chassis - Google Patents

Self-propelled aerial working platform chassis Download PDF

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Publication number
CN102848871A
CN102848871A CN2012103471746A CN201210347174A CN102848871A CN 102848871 A CN102848871 A CN 102848871A CN 2012103471746 A CN2012103471746 A CN 2012103471746A CN 201210347174 A CN201210347174 A CN 201210347174A CN 102848871 A CN102848871 A CN 102848871A
Authority
CN
China
Prior art keywords
bridge
pontic
locating dowel
oil cylinder
dowel pin
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.)
Pending
Application number
CN2012103471746A
Other languages
Chinese (zh)
Inventor
谢观生
韦家义
黄禄辉
曹洲
李才斌
徐涛
李泽
陆声凯
唐恒
蒙学刘
陈昭军
苏宏武
王勇
黄井泉
李春辉
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.)
Guangxi Yuchai Heavy Industry Co Ltd
Original Assignee
Guangxi Yuchai Heavy Industry 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 Guangxi Yuchai Heavy Industry Co Ltd filed Critical Guangxi Yuchai Heavy Industry Co Ltd
Priority to CN2012103471746A priority Critical patent/CN102848871A/en
Publication of CN102848871A publication Critical patent/CN102848871A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a self-propelled aerial working platform chassis, which is characterized in that a half-bridge optimized design, a common cylinder and an electric element proximity switch are adopted, so that variable control of a wheel track is realized, electric control and mechanical double locking of a half-bridge position are realized, and stability and safety of an aerial working platform are improved.

Description

A kind of self-propelled aloft working platform chassis
Technical field
The present invention relates to the self-propelled aloft working platform chassis.
Technical background
Self-propelled aloft working platform is widely used in the industries such as Ship Building and Repairing, engineering construction, industry installation, overhaul of the equipments.In order to improve the working stability of self-propelled aloft working platform, generally need to strengthen the wheel gauge, but wheelspan is fixed and larger high-altitude operation platform transport performance is poor.Therefore, the wheel gauge on chassis needs scalable, improves the stability of operation and the comfort feature of transportation.
Patent No. ZL200720177872.0 provides a kind of underpan traveling system for altitude operation vehicle, be the four wheel drive mode, it takes turns the gauge telescoping mechanism, and can automatically to finish the wheel gauge in the process of travelling flexible, its telescopic oil cylinder is the double piston-rod structure, the telescopic oil cylinder cylinder barrel is fixed on the chassis, and oil cylinder is made and install complicated.
Patent No. ZL200820035630.2 and 200810025198.3 provides a kind of chassis that can automatically keep the self-propelled aloft working platform of turn table balance, adopt the moving bridge construction of double pendulum, to be articulated on the vehicle frame, three six logical control cock are installed on its back axle, and the control lever of control cock and rear-axle hinging, be difficult to form feedback, action response accuracy and runtime aspect Shortcomings, and it takes turns the flexible of gauge also is to have adopted jacking cylinder system, complex structure, inefficiency.
Summary of the invention
The problem of solution required for the present invention is, overcomes now technical deficiency, and a kind of self-propelled aloft working platform chassis is provided, and can realize in the process of moving taking turns the flexible, reliable and stable of gauge.
In order to solve the problems of the technologies described above, the technical solution used in the present invention is: high-altitude operation platform adopts the four wheel drive mode, is divided into four half-bridges all around; The front left half-bridge all is to be connected by a common oil cylinder with front right half-bridge, rear left half-bridge with the rear right half-bridge; Half-bridge is equipped with slide block all around and slides in vehicle frame smoothly; Be welded with the annular stop piece on the half-bridge, the stroke that slides by the restriction half-bridge that is fixed on the bearing pin machinery on the vehicle frame; On the vehicle frame four half-bridges are equipped with four approach switchs, detect the situation that slides of half-bridge, behind the flexible Overstroke of half-bridge, also keep locking by electric-control system cut-out oil circuit, thereby reach the purpose of the automatically controlled and mechanical double-locking of wheel gauge variation.
Advantage of the present invention is simple in structure, with low cost, successful, safe.
Description of drawings
Accompanying drawing 1 is that chassis assembly of the present invention is stretched the status architecture scheme drawing entirely
Accompanying drawing 2 is that chassis assembly of the present invention is stretched the left TV structure scheme drawing of state entirely
Accompanying drawing 3 is the present invention's half crossstructure scheme drawings
Accompanying drawing 4 is that A-A of the present invention analyses and observe (spacing half pontic of the spacing bearing pin of half-bridge) structural representation
Accompanying drawing 5 is A of the present invention to view (approach switch detect half pontic put in place situation) structural representation
Accompanying drawing 6 is chassis assembly fully compensated state structural representations of the present invention
The specific embodiment
The present invention includes: half pontic (1), half-bridge locating dowel pin (2), half-bridge locating dowel pin adapter plate (3), frame assembly (4), oil cylinder (5), support (6), approach switch (7), proximity test plate (8), annular stop piece (9), slide block (10).
Referring to accompanying drawing 1, the front left half-bridge is connected by a common oil cylinder (5) with the rear right half-bridge with front right half-bridge, rear left half-bridge;
Referring to accompanying drawing 3, annular stop piece (9) is welded on half pontic (1); Proximity test plate (8) is installed on half pontic (1), and the distance of two blocks of proximity test plates is oil cylinder stroke; Slide block (10) is installed on the face on four limits of half pontic (1), adjusts gap between half-bridge and frame assembly (4) contact surface by increasing or reduce the quantity of adjusting pad (11);
Referring to accompanying drawing 4, half-bridge locating dowel pin (2) inserts in the pin-and-hole of frame assembly (4), half-bridge locating dowel pin adapter plate (3) is bolted on the frame assembly (4), and inserts the displacement of the groove interior restriction half-bridge locating dowel pin (2) of half-bridge locating dowel pin (2);
Referring to accompanying drawing 5, approach switch (7) is installed in frame assembly (4) by support (6), and four half-bridges have four approach switchs to detect respectively;
Referring to accompanying drawing 2, about oil cylinder (5) directly is connected on the pin-and-hole of half pontic (1), oil cylinder (5) stretches out drive half pontic (1) beginning and stretches out toward both sides, until approach switch (7) is when detecting proximity test plate (8), half-bridge is in maximum and stretches out state, half-bridge locating dowel pin this moment (2) blocks the annular stop piece (9) on half pontic (1), when treating that four approach switchs (7) all detect proximity test plate (8), electric-control system cuts off the fuel feeding of oil cylinder (5) and keeps locking, and the chassis of self-propelled aloft working platform namely reaches maximum deployed condition;
Referring to accompanying drawing 6, oil cylinder (5) is retracted and is driven past middle contraction of half pontic (1) beginning, until approach switch (7) is when detecting proximity test plate (8), half-bridge is in the minimum retracted state, half-bridge locating dowel pin this moment (2) blocks the annular stop piece (9) on half pontic (1), when treating that four approach switchs (7) all detect proximity test plate (8), electric-control system cuts off the fuel feeding of oil cylinder (5) and keeps locking, and the chassis of self-propelled aloft working platform namely reaches the minimum retracted state.

Claims (5)

1. the chassis of a self-propelled aloft working platform, comprise half pontic (1), half-bridge locating dowel pin (2), half-bridge locating dowel pin adapter plate (3), frame assembly (4), oil cylinder (5), support (6), approach switch (7), proximity test plate (8), annular stop piece (9), slide block (10), adjust pad (11), it is characterized in that: half pontic (1) is inserted in the frame assembly (4), oil cylinder (5) connects respectively the front and back half-bridge of the right and left, flexible interlock half-bridge by oil cylinder flexible, half-bridge the flexible situation that puts in place realizes machinery and electric limitation locking by the detection signal of half-bridge locating dowel pin (2) and approach switch (7).
2. half pontic as claimed in claim 1 (1), it is characterized in that: annular stop piece (9) is welded on half pontic (1); Proximity test plate (8) is installed on half pontic (1), and the distance of two blocks of proximity test plates is oil cylinder stroke; Slide block (10) is installed on the face on four limits of half pontic (1), adjusts gap between half-bridge and frame assembly (4) contact surface by increasing or reduce the quantity of adjusting pad (11).
3. half-bridge locating dowel pin as claimed in claim 1 (2) is characterized in that: be milled with groove on the bearing pin, prevent that by half-bridge locating dowel pin adapter plate (3) it from deviating from.
4. mechanical position limitation locking as claimed in claim 1, it is characterized in that: half pontic (1) is in when stretching out maximum rating or retraction minimum rating, blocks annular stop piece (9) by half-bridge locating dowel pin (2) and realizes.
5. electric limiting locking as claimed in claim 1, it is characterized in that: when approach switch (7) detects proximity test plate (8), half-bridge is in maximum and stretches out state or minimum retracted state, when treating that four approach switchs (7) all detect proximity test plate (8), electric-control system cuts off the fuel feeding of oil cylinder (5) and keeps locking, and the chassis of self-propelled aloft working platform namely reaches the operating condition that needs.
CN2012103471746A 2012-09-19 2012-09-19 Self-propelled aerial working platform chassis Pending CN102848871A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2012103471746A CN102848871A (en) 2012-09-19 2012-09-19 Self-propelled aerial working platform chassis

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2012103471746A CN102848871A (en) 2012-09-19 2012-09-19 Self-propelled aerial working platform chassis

Publications (1)

Publication Number Publication Date
CN102848871A true CN102848871A (en) 2013-01-02

Family

ID=47396006

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2012103471746A Pending CN102848871A (en) 2012-09-19 2012-09-19 Self-propelled aerial working platform chassis

Country Status (1)

Country Link
CN (1) CN102848871A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050027421A1 (en) * 2003-07-31 2005-02-03 Humpal Richard Allen Adjustable axle control
CN101311010A (en) * 2008-04-30 2008-11-26 江阴市华澄特种机械工程有限公司 Self-propelled aloft work platform base capable of automatically keeping rotary platform balance
CN201161629Y (en) * 2007-10-16 2008-12-10 北京京城重工机械有限责任公司 Underpan traveling system
CN201501250U (en) * 2009-09-29 2010-06-09 武小玉 Wheel tread adjusting mechanism for automobile
CN101934682A (en) * 2010-09-21 2011-01-05 浙江鼎力机械有限公司 Self-propelled platform base
CN102658842A (en) * 2012-04-13 2012-09-12 领新(南通)重工有限公司 Compact type high-altitude-vehicle chassis axle extending system
CN202952776U (en) * 2012-09-19 2013-05-29 广西玉柴重工有限公司 Self-propelled aerial work platform chassis

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050027421A1 (en) * 2003-07-31 2005-02-03 Humpal Richard Allen Adjustable axle control
CN201161629Y (en) * 2007-10-16 2008-12-10 北京京城重工机械有限责任公司 Underpan traveling system
CN101311010A (en) * 2008-04-30 2008-11-26 江阴市华澄特种机械工程有限公司 Self-propelled aloft work platform base capable of automatically keeping rotary platform balance
CN201501250U (en) * 2009-09-29 2010-06-09 武小玉 Wheel tread adjusting mechanism for automobile
CN101934682A (en) * 2010-09-21 2011-01-05 浙江鼎力机械有限公司 Self-propelled platform base
CN102658842A (en) * 2012-04-13 2012-09-12 领新(南通)重工有限公司 Compact type high-altitude-vehicle chassis axle extending system
CN202952776U (en) * 2012-09-19 2013-05-29 广西玉柴重工有限公司 Self-propelled aerial work platform chassis

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C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20130102