CN103832262A - Rotatable engine mounting structure of overhead working vehicle - Google Patents

Rotatable engine mounting structure of overhead working vehicle Download PDF

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Publication number
CN103832262A
CN103832262A CN201410113985.9A CN201410113985A CN103832262A CN 103832262 A CN103832262 A CN 103832262A CN 201410113985 A CN201410113985 A CN 201410113985A CN 103832262 A CN103832262 A CN 103832262A
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China
Prior art keywords
mount pad
driving engine
platform
engine mount
getting
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CN201410113985.9A
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CN103832262B (en
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梁业轩
黎起富
李仕
刘文彬
黄敏
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CHTC Jove Heavy Industry Co Ltd
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CHTC Jove Heavy Industry Co Ltd
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Priority to CN201410113985.9A priority Critical patent/CN103832262B/en
Publication of CN103832262A publication Critical patent/CN103832262A/en
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Abstract

A rotatable engine mounting structure of an overhead working vehicle comprises an engine mounting base (6) rotatably connected with a get-on platform (3), the engine mounting base is a support body comprising a rectangular groove shape, an upper lug and a lower lug which are parallel to each other are arranged on the side face of the engine mounting base, a benchmark positioning hole is formed in a chassis of the get-on platform, the engine mounting base (6) is connected with the benchmark positioning hole in a pivot mode through a rotating pin shaft (4), and therefore the engine mounting base can rotate between the working position and the maintenance position. A rubber cushion block (11) is fixedly connected with the bottom of the engine mounting base (6). The structure further comprises a guide plate (15), the guide plate is fixedly connected with the chassis of the get-on platform (3), and the rubber cushion block (11) is supported on the guide plate. The mounting structure can achieve engine rotation in the narrow space, maintenance of the engine is facilitated, meanwhile, the problem of difficult screwing in and screwing out caused by large vibration between the engine and the platform and the machining error is solved, and the structure is simplified.

Description

The rotatable engine installation structure of a kind of aerial platform
Technical field
The present invention relates to a kind of mounting structure, be specifically related to a kind of mount pad technical field that can be used for the rotatable driving engine of aerial platform.
Background technology
Self-travel type aerial platform is to transport staff and use equipment to arrive the operation height of specifying, carry out the special-use vehicle of job that requires special skills, it replaces just gradually traditional scaffold and is widely used in the dressing of a surface engineering such as maintenance, repairing, welding and the paint work of boats and ships of urban construction, large-scale building site and Architectural Equipment, chemical plant, as for holding Shanghai World's Fair in 2010, just build the over one hundred seat of all kinds of venues.The internal height of these venues and constructional feature have determined that aerial platform is almost indispensable in its construction and using.
And above-mentioned aerial platform generally uses fuel power or driven by power, its working space is narrow and small, complete machine is arranged quite tightly preesed, in the time adopting fuel engines, driving engine and platform riser gap are very little, in the time that driving engine breaks down, maintainer cannot enter between driving engine and riser and keep in repair, thereby causes system maintenance difficulty.Also there is driving engine to be surrounded by protecting sheathing outward, overhauled into problem.
The publication number of ZHEJIANG DINGLI MACHINERY CO.,LTD is the patent of invention of CN102219167A, a kind of engine installation device of aerial work platform that can easy access is disclosed, its driving engine is arranged on support, guide-track groove is arranged at this support bottom, the both sides of fixed mount are provided with roller, this support is slidably mounted on fixed mount, and is locked by locking member.When maintenance, catch gear is untied, and support is pulled out from fixed mount, convenient maintenance.This formula mounting structure that skids off needs failure-free locking mechanism, and because of its intrinsic movable connection structure, engine framework and the vibrations of fuselage platform are very large, and the vibrating noise of eliminating driving engine also brings the difficulty that is difficult to overcome.
In sum, prior art exists defect as follows:
(1) the too small and maintenance difficult problem that causes in aloft work car engine and riser gap;
(2) driving engine adopts the excessive rotation after rotation is installed and damages Hydraulic Pump and engine accessory power rating;
(3), after driving engine adopts rotation to install, driving engine mount pad and platform vibrations are large;
(4) after driving engine adopts rotation to install, the engine case processing installation difficulty causing not in place.
Summary of the invention
The problem existing for above-mentioned prior art, object of the present invention provides a kind of high-altitude operation platform engine installation structure of easy access, this structure can rotate to an angle and facilitate the maintenance of driving engine, also can guarantee the fixed installation structure of driving engine, is easy to realize noise and eliminates.
The present invention realizes like this, the rotatable engine installation structure of a kind of aerial platform, comprise the driving engine seat of sitting idly, described driving engine mount pad is rotatably connected with getting-on platform, described driving engine mount pad is one to include the stake body of rectangular flute profile, side is provided with parallel upper lug and lower lug, upper lug is the extension of plane on driving engine mount pad, with upper plane in same plane, lower lug is larger than upper lug area, spill upper lug part at lower lug and be provided with pin shaft hole, being fixedly connected with at control position and getting-on platform for driving engine mount pad.One pin shaft hole is arranged between upper lug and lower lug, is installed with rotary pin shaft in pin shaft hole;
On the chassis of described getting-on platform, be provided with a baseline positioning hole, described driving engine mount pad, by rotary pin shaft and described baseline positioning hole pivot joint, can rotate driving engine mount pad between control position and maintenance position; Be fixedly connected with rubber cushion blocks in driving engine mount pad bottom;
Also comprise directing plate, described directing plate is bent into by bevel phase and planar section and forms, and described plane is fixedly connected with getting-on platform, and described rubber cushion blocks is supported on described directing plate; In the time that driving engine mount pad rotates to control position, described rubber cushion blocks is supported on the planar section of directing plate, and in the time that driving engine mount pad rotates to maintenance position, described rubber cushion blocks is supported on the bevel phase of directing plate.
Further, on the chassis of getting-on platform, be welded with anti-mistake and turn block, the lower lug of driving engine mount pad is formed to backstop.
Further, be also provided with multiple rotation knock holees on getting-on platform, described multiple rotation knock holees and anti-mistake turn block take baseline positioning hole as center of circle radial distribution, and even interval; In the time that driving engine mount pad rotates to control position or maintenance position, pass driving engine mount pad and described rotation knock hole location by rotation prevention pin shaft fixing.
Further, the inclined-plane of described directing plate and the angle of inclination of horizontal surface are 5 °~10 °.
Further, between described rotary pin shaft and baseline positioning hole, oilless metal is installed.
Further, described driving engine mount pad sidewall is provided with fixed orifice, in the time that driving engine mount pad rotates to control position, by bolt of rear end plate, captive nut connecting engine mount pad and getting-on platform.
Further, described driving engine mount pad bottom welding has rubber cushion blocks mount pad, and described rubber cushion blocks is connected with rubber cushion blocks mount pad by rubber bolt of rear end plate;
Further, on described driving engine mount pad, engine block is installed, described engine block comprises fuel engines and radiator and is installed on the Hydraulic Pump on fuel engines by coupler, and described engine block is connected on driving engine mount pad by multiple yielding rubber pads.
The invention has the beneficial effects as follows: the rotatable engine installation structure of the construction machinery and equipment that the heavy-duty low-speeds such as the applicable aerial platform of the present invention travel, can in small space, realize engine rotation, guarantee the maintainability energy of driving engine, solved the installation difficulty that vibrations are large and Mismachining tolerance causes of driving engine and platform simultaneously, this is simple in structure, economical and practical, convenient for installation and maintenance.
Accompanying drawing explanation
Fig. 1 is the front view of the driving engine installation assembly part of the embodiment of the present invention.
Fig. 2 is the birds-eye view of the driving engine installation assembly part of the embodiment of the present invention.
After Fig. 3 is the removal driving engine of the embodiment of the present invention, the birds-eye view that mount pad is connected with platform.
Fig. 4 is the enlarged drawing of the I of the driving engine seat assembly partial graph 1 of the embodiment of the present invention;
Fig. 5 is the schematic diagram that the driving engine seat assembly part mount pad side plate of the embodiment of the present invention is connected with platform.
Reference numeral in above-mentioned figure:
1 fuel engines, 2 radiator 3 getting-on platforms, 4 rotary pin shafts, 5-1 engine cushion rubber pad, 5-2 radiator yielding rubber pad, 6 driving engine mount pads, 7 rotation prevention pin shafts, 8 anti-mistakes turn block, 9 Hydraulic Pumps, 10 rubber pad tie bolts, 11 mount pad rubber shock-absorbing cushion blocks, 12 rubber cushion blocks mount pads, 13 captive nuts, 14 bolt of rear end plates, 15 directing plates
The specific embodiment
Below in conjunction with accompanying drawing, embodiments of the invention are elaborated, but be not used for limiting the scope of the invention.
As Figure 1-3, the engine installation structure of the present embodiment, comprise that high-altitude operation fuel oil starts 1 and radiator 2 and be installed on the Hydraulic Pump 9 on fuel engines 1 by coupler, above-mentioned mounting structure is respectively by multiple yielding rubber pad 5-1,5-2 is connected on driving engine mount pad 6, driving engine mount pad 6 is connected with the chassis lug of the getting-on platform 3 of aerial platform by rotary pin shaft 4, realize 6 drives of driving engine mount pad on it all parts entirety around the rotatable certain angle of S. A. 4.For reducing the make an uproar consideration of difficulty of control, between rotary pin shaft 4 and fixed mount, be provided with oilless metal, substitute antifriction-bearing box conventional in prior art, processing and install also convenient.Be welded with rubber cushion blocks mount pad 12 in driving engine mount pad 6 inside bottom, mount pad rubber shock-absorbing cushion block 11 is connected with rubber cushion blocks mount pad 12 by rubber pad tie bolt 10, plays further shock-absorbing function.
Described driving engine mount pad is one to include the stake body of rectangular flute profile, in groove, be provided with reinforced rib, side is provided with parallel upper lug and lower lug, upper lug is the extension of plane on driving engine mount pad, in same plane, lower lug is larger than upper lug area with upper plane, and lower lug and reinforced rib link into an integrated entity, spill upper lug part at lower lug and be provided with pin shaft hole, being fixedly connected with at control position and getting-on platform 3 for driving engine mount pad 6.In the upper left corner, lug place is installed with rotary pin shaft 4, and the two ends of rotary pin shaft 4 are located in the oilless metal of bearing pin mounting hole of getting-on platform 3.The sidewall on the right side of driving engine mount pad 6 is provided with fixed orifice, in the time that driving engine mount pad 6 rotates to control position, by bolt of rear end plate 14, captive nut 13 connecting engine mount pads 6 and getting-on platform 3.The chassis lug of described getting-on platform 3 is provided with the corresponding pin shaft hole of pin shaft hole with described lower lug.
In order flexibly to guide back-out and the screw-in of driving engine mount pad 6, on the chassis of getting-on platform 3, just to mount pad rubber shock-absorbing cushion block 11 place's welding directing plates 15, described directing plate 15 is bent into by bevel phase and the planar section of 5 °~10 ° and forms.In the time that driving engine mount pad 6 screws out maintenance position, rubber shock-absorbing cushion block 11 is also by being transitioned into inclined-plane and contacting with directing plate 15 plane contact, but still plays certain supporting role.In the time that driving engine mount pad 6 is screwed into control position, rubber shock-absorbing cushion block 11 also by with directing plate 15 chamfered transition to plane contact, now shock-absorbing support effect is still played on the chassis of directing plate and getting-on platform 3.
In the time of rotary engine seat 6, be welded on contact that angle that 15 bendings of directing plate on getting-on platform 3 form can effectively guide mount pad rubber shock-absorbing cushion block 11 and directing plate 15 and separate, after effectively preventing that manufacture, assembly error from causing that engine rotation out, cannot return smoothly the problem of dress, mount pad rubber shock-absorbing cushion block 11 can effectively be isolated the vibrations of engine bed 6 and getting-on platform 3 simultaneously, reaches the effect of damping.In the time that driving engine mount pad 6 rotates to control position, by bolt of rear end plate 14, captive nut 13 connecting engine mount pads 6 and getting-on platform 3, the base plate of getting-on platform 3 be provided with multiple rotation knock holees and reference for installation knock hole, rotation prevention pin shaft 7 is fixed through driving engine mount pad 6 and described mounting-positioning holes, thereby assurance driving engine and getting-on platform stable connection are reliable.In the time that driving engine needs repairing, cleans, safeguards or changes accessory, take off bolt of rear end plate 14, captive nut 13 and rotation prevention pin shaft 7, driving engine mount pad 6 is rotated to maintenance position, reconnect rotation prevention pin shaft 7 in rotation knock hole, can carry out service work.For guaranteeing only to transfer to damage Hydraulic Pump 9 when driving engine mount pad 6, on the base plate of getting-on platform 3, be welded with anti-mistake and turn block 8, it is center of circle radial distribution take origin reference location aperture that described multiple rotation knock holees and anti-mistake turn block 8.Implementation method of the present invention is simple, economical and practical, is convenient to promote.

Claims (8)

1. the rotatable engine installation structure of aerial platform, comprise the driving engine being rotatably connected with getting-on platform (3) sit idly seat (6), it is characterized in that,
Described driving engine mount pad is one to include the stake body of rectangular flute profile, side is provided with parallel upper lug and lower lug, upper lug is the extension of plane on driving engine mount pad, with upper plane in same plane, lower lug is larger than upper lug area, spill upper lug part at lower lug and be provided with pin shaft hole, being fixedly connected with in control position and getting-on platform (3) for driving engine mount pad (6).One pin shaft hole is arranged between upper lug and lower lug, is installed with rotary pin shaft (4) in pin shaft hole;
On the chassis of described getting-on platform (3), be provided with a baseline positioning hole, described driving engine mount pad (6), by rotary pin shaft (4) and described baseline positioning hole pivot joint, can rotate driving engine mount pad between control position and maintenance position; Be installed with rubber cushion blocks (11) in driving engine mount pad (6) bottom;
Also comprise directing plate (15), described directing plate is bent into by bevel phase and planar section and forms, and described plane is fixedly connected with getting-on platform (3), and described rubber cushion blocks (11) is supported on described directing plate; In the time that driving engine mount pad (6) rotates to control position, described rubber cushion blocks (11) is supported on the planar section of directing plate, and in the time that driving engine mount pad (6) rotates to maintenance position, described rubber cushion blocks (11) is supported on the bevel phase of directing plate.
2. the rotatable engine installation structure of a kind of aerial platform as claimed in claim 1, is characterized in that, is welded with anti-mistake and turns block (10) on the chassis of described getting-on platform (3), and the lower lug of driving engine mount pad (6) is formed to backstop.
3. the rotatable engine installation structure of a kind of aerial platform as claimed in claim 2, it is characterized in that, on getting-on platform (3), be also provided with multiple rotation knock holees, described multiple rotation knock hole and anti-mistake turn block (10) take baseline positioning hole as center of circle radial distribution, and even interval; In the time that driving engine mount pad (6) rotates to control position or maintenance position, fixing through driving engine mount pad (6) and described rotation knock hole location by rotation prevention pin shaft (7).
4. the rotatable engine installation structure of a kind of aerial platform as claimed in claim 1, is characterized in that, the inclined-plane of described directing plate (15) and the angle of inclination of horizontal surface are 5 °~10 °.
5. the rotatable engine installation structure of a kind of aerial platform as claimed in claim 1, is characterized in that, between described rotary pin shaft (4) and baseline positioning hole, oilless metal is installed.
6. the rotatable engine installation structure of a kind of aerial platform as claimed in claim 1, it is characterized in that, described driving engine mount pad (6) sidewall is provided with fixed orifice, in the time that driving engine mount pad (6) rotates to control position, by bolt of rear end plate (14), captive nut (13) connecting engine mount pad (6) and getting-on platform (3).
7. the rotatable engine installation structure of a kind of aerial platform as claimed in claim 1, it is characterized in that, described driving engine mount pad (6) bottom welding has rubber cushion blocks mount pad (12), and described rubber cushion blocks (11) is connected with rubber cushion blocks mount pad (12) by rubber bolt of rear end plate (10).
8. the rotatable engine installation structure of a kind of aerial platform as described in claim 1-7 any one, it is characterized in that, on described driving engine mount pad (6), engine block is installed, described engine block comprises fuel engines (1) and radiator (2) and is installed on the Hydraulic Pump (9) on fuel engines by coupler, and described engine block is connected on driving engine mount pad (6) by multiple yielding rubber pads (5).
CN201410113985.9A 2014-03-25 2014-03-25 A kind of rotatable engine installation structure of high-altitude operation vehicle Active CN103832262B (en)

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Application Number Priority Date Filing Date Title
CN201410113985.9A CN103832262B (en) 2014-03-25 2014-03-25 A kind of rotatable engine installation structure of high-altitude operation vehicle

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Application Number Priority Date Filing Date Title
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CN103832262B CN103832262B (en) 2016-06-01

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106627089A (en) * 2016-12-30 2017-05-10 徐工消防安全装备有限公司 Damping engine pallet for aerial operation platform
CN107810122A (en) * 2015-07-24 2018-03-16 标致雪铁龙汽车股份有限公司 Pivoting device
CN112406506A (en) * 2020-12-04 2021-02-26 广州电力机车有限公司 Maintenance method for diesel engine mounting seat of mining dump truck

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20020055029A (en) * 2000-12-28 2002-07-08 이계안 A Roll Rod for Engine Mount of Vehicle
JP2004176837A (en) * 2002-11-28 2004-06-24 Tokai Rubber Ind Ltd Roll mount
CN201206096Y (en) * 2008-02-26 2009-03-11 山东交通学院 Full-hydraulic crawler-type self-walking aerial working platform
CN102219167A (en) * 2011-03-29 2011-10-19 浙江鼎力机械有限公司 Engine mounting device for aerial work platform convenient for maintenance
CN203766476U (en) * 2014-03-25 2014-08-13 恒天九五重工有限公司 Rotatable engine mounting structure of hydraulic aerial cage

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20020055029A (en) * 2000-12-28 2002-07-08 이계안 A Roll Rod for Engine Mount of Vehicle
JP2004176837A (en) * 2002-11-28 2004-06-24 Tokai Rubber Ind Ltd Roll mount
CN201206096Y (en) * 2008-02-26 2009-03-11 山东交通学院 Full-hydraulic crawler-type self-walking aerial working platform
CN102219167A (en) * 2011-03-29 2011-10-19 浙江鼎力机械有限公司 Engine mounting device for aerial work platform convenient for maintenance
CN203766476U (en) * 2014-03-25 2014-08-13 恒天九五重工有限公司 Rotatable engine mounting structure of hydraulic aerial cage

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107810122A (en) * 2015-07-24 2018-03-16 标致雪铁龙汽车股份有限公司 Pivoting device
CN107810122B (en) * 2015-07-24 2020-07-28 标致雪铁龙汽车股份有限公司 Pivoting device
CN106627089A (en) * 2016-12-30 2017-05-10 徐工消防安全装备有限公司 Damping engine pallet for aerial operation platform
CN106627089B (en) * 2016-12-30 2023-09-08 徐工消防安全装备有限公司 Vibration reduction engine tray for aerial working platform
CN112406506A (en) * 2020-12-04 2021-02-26 广州电力机车有限公司 Maintenance method for diesel engine mounting seat of mining dump truck
CN112406506B (en) * 2020-12-04 2021-12-07 广州电力机车有限公司 Maintenance method for diesel engine mounting seat of mining dump truck

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