CN202016839U - Engine installation device of aerial work platform with convenience in overhaul - Google Patents
Engine installation device of aerial work platform with convenience in overhaul Download PDFInfo
- Publication number
- CN202016839U CN202016839U CN 201120086036 CN201120086036U CN202016839U CN 202016839 U CN202016839 U CN 202016839U CN 201120086036 CN201120086036 CN 201120086036 CN 201120086036 U CN201120086036 U CN 201120086036U CN 202016839 U CN202016839 U CN 202016839U
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- China
- Prior art keywords
- support
- fixed mount
- drag chain
- engine
- operation platform
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- Expired - Lifetime
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Abstract
The utility model relates to an engine installation device of an aerial work platform. In the engine installation device of an aerial work platform with convenience in overhaul, a fixed mount of the installation device is arranged on a chassis of the aerial work platform, the two sides of the inner side of the fixed mount are respectively provided with a guide groove, a front shield plate is arranged at the front part of an engine base, the two sides of the bottom of the engine base are respectively provided with an idler wheel, the idler wheels are arranged in the guide grooves, and an engine body is installed 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 fixed mount, an installation passage is arranged in the middle of the drag chain, and a control cable and an oil-way pipeline of the engine body are connected to all the parts of the aerial work platform through the installation passage; and a fixed locking component is arranged at the front part of the engine base, and the locking component fixes the engine base with the fixed mount. The engine can be dragged out from the fixed mount, so the engine is convenient to overhaul, and the phenomenon that the connection of the control cable and the oil-way pipeline falls off due to overhaul is avoided. The utility model has the characteristics of simple structure and convenience in overhaul.
Description
Technical field
The utility model relates to high-altitude operation platform, relates 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 purpose of this utility model provides a kind of high-altitude operation platform engine installation device 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 utility model 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.The utlity model has simple in structure, overhaul characteristics easily.
Description of drawings
Fig. 1 is a mounting structure scheme drawing of the present utility model.
Fig. 2 is the left view of Fig. 1.
Fig. 3 is a structural representation of the present utility model.
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 utility model 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 201120086036 CN202016839U (en) | 2011-03-29 | 2011-03-29 | Engine installation device of aerial work platform with convenience in overhaul |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120086036 CN202016839U (en) | 2011-03-29 | 2011-03-29 | Engine installation device of aerial work platform with convenience in overhaul |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202016839U true CN202016839U (en) | 2011-10-26 |
Family
ID=44810513
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120086036 Expired - Lifetime CN202016839U (en) | 2011-03-29 | 2011-03-29 | Engine installation device of aerial work platform with convenience in overhaul |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202016839U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
-
2011
- 2011-03-29 CN CN 201120086036 patent/CN202016839U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN102219167B (en) * | 2011-03-29 | 2013-01-23 | 浙江鼎力机械有限公司 | Engine mounting device for aerial work platform convenient for maintenance |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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 city of Huzhou province Deqing County leidian town 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. |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20111026 Effective date of abandoning: 20130227 |
|
| RGAV | Abandon patent right to avoid regrant |