CN102219167A - Engine mounting device for aerial work platform convenient for maintenance - Google Patents
Engine mounting device for aerial work platform convenient for maintenance Download PDFInfo
- Publication number
- CN102219167A CN102219167A CN2011100759954A CN201110075995A CN102219167A CN 102219167 A CN102219167 A CN 102219167A CN 2011100759954 A CN2011100759954 A CN 2011100759954A CN 201110075995 A CN201110075995 A CN 201110075995A CN 102219167 A CN102219167 A CN 102219167A
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- support
- drag chain
- engine
- operation platform
- altitude operation
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- 238000012423 maintenance Methods 0.000 title abstract description 5
- 238000009434 installation Methods 0.000 claims description 12
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 238000003466 welding Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
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- Auxiliary Drives, Propulsion Controls, And Safety Devices (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to an engine mounting device for an aerial work platform, in particular to an engine mounting device for an aerial work platform convenient for maintenance. A fixing frame of the mounting device is arranged on a chassis of the aerial work platform, guide grooves are respectively arranged at two sides of the inner side of the fixing frame, a front cover plate is arranged at the front part of an engine base, roller wheels are respectively arranged two side edges the bottom of the engine base and arranged in the guide grooves, and an engine body is mounted on the engine base; one end of a drag chain is fixedly connected with the rear part of the engine base, the other end of the drag chain is fixedly connected with the fixing frame, a mounting channel is arranged in the middle of the drag chain, a control wire and oil line pipeline of the engine body are connected with all parts of the aerial work platform by the mounting channel; a fixing-locking member arranged at the front part of the engine base, and the engine base and the fixing frame are fixed with each other by the fixing-locking member. In the invention, the engine base can be drawn out from the fixing frame, so that the engine can be overhauled conveniently, and simultaneously, the connection falling between a control wire and oil line pipeline caused by overhauling can be avoided. The engine mounting device has the advantages of simple structure and convenience in overhauling.
Description
Technical field
The present invention relates to high-altitude operation platform, relate in particular to the engine installation device of high-altitude operation platform.
Background technology
Existing aloft work all is to adopt external source or adopt storage battery power supply, adopts the high-altitude operation platform of external source to have the limitation of use, can't use in power free in the open air place.And for storage battery, because reserve of electricity is limited, the too short use that also limits high-altitude operation platform of the time of use.For the noble job platform of open-air cross-country, it need guarantee to have the power supply supply of long duration in the open air, and also bigger to the demand of power, therefore all is to adopt the diesel type driving engine that power is provided.Existing diesel type driving engine all is to be fixed on the base of high-altitude operation platform, is surrounded by protecting sheathing outward, and for this driving engine owing to be fully closed, overhauled into problem.
Summary of the invention
In order to solve the technical matters of existing high-altitude operation platform diesel type tune-up inconvenience, the high-altitude operation platform engine installation device that the purpose of this invention is to provide a kind of easy access, this device has made things convenient for the maintenance of driving engine, simultaneously again can be to not impacting with driving engine bonded assembly parts.
The engine installation device of high-altitude operation platform, this comprises the fixed mount that is arranged on the fuselage, above fixed mount, be formed with the installing port of engine block, the inboard both sides of fixed mount are respectively equipped with roller, the two bottom sides limit of support is respectively equipped with guide-track groove, described roller is arranged in the guide-track groove, and described engine block is mounted on the support; The front portion of support is provided with shroud upper panel, the rear portion of support is provided with drag chain, drag chain is hinged by the polylith connecting panel that is arranged on the drag chain both sides and constitutes, drag chain is " J " type, one end is captiveed joint with the rear portion of support, the other end is captiveed joint with fixed mount, and is provided with the installation passage at the middle part of drag chain, and the control electric wire of described engine block and oil line pipe are connected to each parts of high-altitude operation platform by passage is installed; And being provided with the fixing and locking member in the front portion of support, locking member interfixes support and fixed mount.
As further improvement, above-mentioned locking member comprises latch hook, latch hook is made of handle and buckle, handle and buckle are " L " type, the middle part of latch hook is hinged to be arranged on the support, and the below of articulated section is provided with spring, and the spring lower end is connected with support, and on fixed mount, being provided with bearing pin, buckle matches with bearing pin.
As further improvement, above-mentioned support is provided with shock-proof block, and described engine block is fixedly installed on the support by shock-proof block.The both sides of the front and back end of described engine block are respectively equipped with adapter plate, and described shock-proof block and adapter plate are bolted to connection.
As further improvement, the top of above-mentioned drag chain is provided with cover plate.Cover plate can prevent that electroslag welding drops on the drag chain owing to carry out the electric welding construction on high-altitude operation platform, burns out control electric wire or oil line pipe.
The present invention is owing to adopted above-mentioned technical scheme, support can be pulled out from fixed mount, made things convenient for the maintenance of driving engine, simultaneously owing to be provided with drag chain in the rear end of support, guaranteed the stable hauling-out of support on the one hand, one side is connected to each parts of high-altitude operation platform with the control electric wire and the oil line pipe of engine block by the installation passage in the drag chain in addition, has avoided like this because the connection that maintenance causes controlling electric wire and oil line pipe comes off.That the present invention has is simple in structure, overhaul characteristics easily.
Description of drawings
Fig. 1 is a mounting structure scheme drawing of the present invention.
Fig. 2 is the left view of Fig. 1.
Fig. 3 is a structural representation of the present invention.
Fig. 4 is the left view of Fig. 3.
Fig. 5 is the structural representation between support, drag chain and the fixed mount.
Fig. 6 is the left view of Fig. 5.
Fig. 7 is the structural representation of drag chain.
The specific embodiment
Below in conjunction with accompanying drawing the specific embodiment of the present invention is made a detailed explanation.
The cross-country fork high-altitude operation platform of cutting as shown in Figure 1 and Figure 2, this high-altitude operation platform by fuselage 1, support 2, wheel running gear 3, engine block 4,, scissor-type jacking system 5, job platform 6, platform guardrail 7, platform stop locking device 8 and body supporting apparatus 9 constitute, wheel running gear 3 is arranged on the fuselage 1, body supporting apparatus 9 is arranged on four bights of fuselage 1, job platform 6 is arranged on the scissor-type jacking system 5
As shown in Figure 3, Figure 4, fuselage 1 is provided with fixed mount 10, above fixed mount 10, be formed with the installing port of engine block 4 in the scissor-type jacking system 5, the inboard both sides of fixed mount 10 are respectively equipped with roller 12, the two bottom sides limit of support 2 is respectively equipped with guide-track groove 21, and described roller 12 is arranged in the guide-track groove 21.Support 2 is provided with shock-proof block 11, and the both sides of the front and back end of described engine block 4 are respectively equipped with adapter plate 41, and described shock-proof block 11 is bolted to connection with adapter plate 41, and the front portion of support 2 is provided with shroud upper panel 22, and the rear portion of support 2 is provided with drag chain 20.
As Fig. 5, shown in Figure 6, drag chain 20 is " J " type, and an end of drag chain 20 is captiveed joint with the rear portion of support 2, and the other end is captiveed joint with fixed mount 10.As shown in Figure 7, drag chain 20 is hinged by the polylith connecting panel 201 that is arranged on drag chain 20 both sides and constitutes, and be provided with at the middle part of drag chain 20 passage 202 is installed, the top of drag chain 20 is provided with cover plate 203, and the control electric wire of described engine block 4 and oil line pipe are connected to each parts of high-altitude operation platform by passage is installed; And being provided with the fixing and locking member in the front portion of support 2, locking member interfixes support 2 and fixed mount 10.
As shown in Figure 3, locking member comprises latch hook, latch hook is made of handle 23 and buckle 24, handle 23 and buckle 24 are " L " type, the middle part of latch hook is hinged to be arranged on the support 2, and the below of articulated section is provided with spring 25, and spring 25 lower ends are connected with support 2, and on fixed mount 10, being provided with bearing pin 13, buckle 24 matches with bearing pin 13.
Claims (5)
1. the high-altitude operation platform engine installation device of easy access, it is characterized in that: this mount pad comprises the fixed mount (10) that is arranged on the high-altitude operation platform fuselage (1), be formed with the installing port of engine block (4) in fixed mount (10) top, the inboard both sides of fixed mount (10) are respectively equipped with roller (12), the two bottom sides limit of support (2) is respectively equipped with guide-track groove (21), described roller (12) is arranged in the guide-track groove (21), and described engine block (4) is mounted on the support (2); The front portion of support (2) is provided with shroud upper panel (22), the rear portion of support (2) is provided with drag chain (20), drag chain (20) is by the polylith connecting panel (201) that is arranged on drag chain (20) the both sides formation that is hinged, drag chain (20) is " J " type, one end is captiveed joint with the rear portion of support (2), the other end is captiveed joint with fixed mount (10), and be provided with at the middle part of drag chain (20) passage (202) is installed, the control electric wire of described engine block (4) and oil line pipe are connected to each parts of high-altitude operation platform by installation passage (202); And being provided with the fixing and locking member in the front portion of support (2), locking member interfixes support (2) and fixed mount (10).
2. the high-altitude operation platform engine installation device of easy access according to claim 1, it is characterized in that: locking member comprises latch hook, latch hook is made of handle (23) and buckle (24), handle (23) and buckle (24) are " L " type, the middle part of latch hook is hinged to be arranged on the support (2), the below of articulated section is provided with spring (25), spring (25) lower end is connected with support (2), and on fixed mount (10), being provided with bearing pin (13), buckle (24) matches with bearing pin (13).
3. the high-altitude operation platform engine installation device of easy access according to claim 1, it is characterized in that: support (2) is provided with shock-proof block, and described engine block (4) is fixedly installed on the support (2) by shock-proof block (11).
4. the high-altitude operation platform engine installation device of easy access according to claim 4, it is characterized in that: the both sides of the front and back end of engine block (4) are respectively equipped with adapter plate (41), and described shock-proof block (11) is bolted to connection with adapter plate (41).
5. the high-altitude operation platform engine installation device of easy access according to claim 1, it is characterized in that: the top of drag chain (20) is provided with cover plate (203).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110075995 CN102219167B (en) | 2011-03-29 | 2011-03-29 | Engine mounting device for aerial work platform convenient for maintenance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110075995 CN102219167B (en) | 2011-03-29 | 2011-03-29 | Engine mounting device for aerial work platform convenient for maintenance |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102219167A true CN102219167A (en) | 2011-10-19 |
| CN102219167B CN102219167B (en) | 2013-01-23 |
Family
ID=44775923
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201110075995 Expired - Fee Related CN102219167B (en) | 2011-03-29 | 2011-03-29 | Engine mounting device for aerial work platform convenient for maintenance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102219167B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103832262A (en) * | 2014-03-25 | 2014-06-04 | 恒天九五重工有限公司 | Rotatable engine mounting structure of overhead working vehicle |
| CN113200475A (en) * | 2021-04-27 | 2021-08-03 | 杨春花 | Water pipeline plays to rise supplementary installation device for basement |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10277967A (en) * | 1997-04-08 | 1998-10-20 | Shiitsupu:Kk | Lift device |
| JP2001063994A (en) * | 1999-08-31 | 2001-03-13 | Aichi Corp | Safeguard for vertically elevatable high lift working vehicle |
| CN201206096Y (en) * | 2008-02-26 | 2009-03-11 | 山东交通学院 | Full-hydraulic crawler-type self-walking aerial working platform |
| CN202016839U (en) * | 2011-03-29 | 2011-10-26 | 浙江鼎力机械有限公司 | Engine installation device of aerial work platform with convenience in overhaul |
-
2011
- 2011-03-29 CN CN 201110075995 patent/CN102219167B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10277967A (en) * | 1997-04-08 | 1998-10-20 | Shiitsupu:Kk | Lift device |
| JP2001063994A (en) * | 1999-08-31 | 2001-03-13 | Aichi Corp | Safeguard for vertically elevatable high lift working vehicle |
| CN201206096Y (en) * | 2008-02-26 | 2009-03-11 | 山东交通学院 | Full-hydraulic crawler-type self-walking aerial working platform |
| CN202016839U (en) * | 2011-03-29 | 2011-10-26 | 浙江鼎力机械有限公司 | Engine installation device of aerial work platform with convenience in overhaul |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103832262A (en) * | 2014-03-25 | 2014-06-04 | 恒天九五重工有限公司 | Rotatable engine mounting structure of overhead working vehicle |
| CN113200475A (en) * | 2021-04-27 | 2021-08-03 | 杨春花 | Water pipeline plays to rise supplementary installation device for basement |
| CN113200475B (en) * | 2021-04-27 | 2023-03-28 | 湖北广盛建设集团有限责任公司 | Water pipeline plays to rise supplementary installation device for basement |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102219167B (en) | 2013-01-23 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP03 | Change of name, title or address |
Address after: 313219 Zhejiang province Deqing County leidian town of Baiyun Road No. 1255 Patentee after: ZHEJIANG DINGLI MACHINERY Co.,Ltd. Address before: 313219 Zhejiang city of Huzhou province Deqing County Lei Dian Zhen Tang Bei Cun, Zhejiang Dingli Machinery Co. Ltd. Patentee before: Zhejiang Dingli Machinery Co.,Ltd. |
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| 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: 20130123 |