CN209274345U - A kind of new engine installation system - Google Patents
A kind of new engine installation system Download PDFInfo
- Publication number
- CN209274345U CN209274345U CN201822042696.0U CN201822042696U CN209274345U CN 209274345 U CN209274345 U CN 209274345U CN 201822042696 U CN201822042696 U CN 201822042696U CN 209274345 U CN209274345 U CN 209274345U
- Authority
- CN
- China
- Prior art keywords
- pallet
- fuselage
- engine
- installation system
- engine installation
- 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.)
- Active
Links
Abstract
A kind of new engine installation system, for engine to be installed on fuselage, including pallet, the pallet is connected by revolving part thereon with fuselage rotation, the pallet has the first station and second station with respect to fuselage by revolving part, when in the first station, the pallet and the engine being mounted on pallet are located at the top of fuselage, when in second station, the pallet and the engine being mounted on pallet are located at the side of fuselage, it has easy to maintenance, and maintenance efficiency is high, and engine stabilization gets well and has the advantages that better damping effect.
Description
Technical field
The utility model relates to technical field of automobile manufacture more particularly to a kind of new engine installation systems.
Background technique
The connection of the power part engine and vehicle body of automobile must be by mounting structure come damping vibration.Currently on the market
And traditional engine installation structure mostly mainly includes motor support mechanism, damping, engine tray mechanism etc.
Composition.The engine of this form is simple with structure, can satisfy the basic installation requirement of engine, therefore, this to start
Machine mounting structure is a kind of engine installation structure that is more typical in industry and being widely used.
Although engine installation structure described above can satisfy the basic installation requirement of engine, but its there is also
Maintenance is than convenient defect.It is mainly reflected in, since above-mentioned engine mounting is mainly connected with fuselage, the complete machine of engine
Space is small, and when engine failure repairs, the personnel of needing repairing squeeze into engine mounting positions and repair to it.It is this
Mode creates great difficulties and inconvenience to maintenance work.In addition, increasing the operation of maintenance personal due to inconvenient maintenance
Time reduces the efficiency of maintenance.It is above-mentioned scarce to overcome therefore, it is necessary to design a kind of engine installation structure easy to maintenance
It falls into.
It should be noted that above content belongs to the technology category of cognition of inventor, the prior art is not necessarily constituted.
Utility model content
The utility model provides a kind of new engine installation system, it has easy to maintenance, and stability is good, has more
The advantages of damping effect got well, solve the problems of the prior art.
Used technical solution is the utility model to solve above-mentioned technical problem:
A kind of new engine installation system, for engine to be installed on fuselage, including pallet, the pallet passes through it
On revolving part and fuselage rotation connect, the pallet by revolving part with respect to fuselage have the first station and second station, locate
When the first station, the pallet is located at the top of fuselage with the engine being mounted on pallet, described when being in second station
Pallet and the engine being mounted on pallet are located at the side of fuselage.
At least two supports are additionally provided on the pallet, the support passes through shock absorber part respectively and is connected with connector, described
Connector is connect with engine.
Locking hole is additionally provided on the pallet, the locking hole is when pallet and fuselage are in the first station, by pallet
It is locked with fuselage by bolt.
The revolving part includes the rotating cylinder being arranged on the inside of pallet, and pallet is connect by the rotating cylinder by pin shaft with fuselage.
The support is set as 4 and is symmetricly set on the upper of pallet.
The shock absorber part is to consolidate with the same number of rubber block damper of support, the rubber block damper difference support
Even.
The connector is to be connected with the same number of stabilizer blade of support, the stabilizer blade and rubber block damper.
Handle is additionally provided on the outside of the pallet.
The utility model prevents pallet far from rotation center by the way that revolving part is being arranged on pallet and is increasing locking hole
Place lower hectare, when failure, can by pallet and thereon engine back-out, raising servicing ease, save a large amount of working hour；Separately
Outside, four supports are set on pallet, engine uniform force can on the one hand be distributed, on the other hand can shorten engine branch
The jib-length of leg mitigates shaking when engine operation, promotes the reliability machine comfort of engine system；Simultaneously in support
On also set up rubber block damper and be able to ascend damping performance.
Detailed description of the invention
Fig. 1 is the perspective view of the utility model；
Fig. 2 is the perspective view of another angle of the utility model；
Fig. 3 is that engine is mounted on the structural schematic diagram on the utility model.
In figure, 1, pallet, 2, support, 3, damper, 4, stabilizer blade, 5, rotating cylinder, 6, handle, 7, locking hole, 8, engine, 9,
Radiator.
Specific embodiment
In order to clarify the technical characteristics of the invention, below by specific embodiment and in conjunction with attached drawing, it is practical to this
It is novel to be described in detail.
In addition, in the description of the present invention, term " center ", "upper", "lower", "front", "rear", "left", "right",
" vertical ", " inside ", " outside ", waiting the orientation or positional relationship of instructions is to be based on the orientation or positional relationship shown in the drawings, only
It is that for the convenience of describing the present invention and simplifying the description, rather than signified device or element must have a particular orientation, therefore
It should not be understood as limiting the present invention.
As shown in Figure 1-3, a kind of new engine installation system, including pallet 1, it is equipped in the middle position of pallet 1
Four supports 2, four supports 2 are symmetrical arranged, and being symmetrical arranged is to reduce the unstable of engine to make uniform force
Property；Four shock absorber parts will be bolted respectively on aforementioned four support 2, when which makes 8 stress of engine
It can be buffered, improve the damping effect of engine 8；Four shock absorber parts are connected by bolt with connector, the connector
It is connected with engine 8, therefore, entire engine 8 is fixed on pallet 1 by connector through shock absorber part and support 2.In pallet 1
Edge is equipped with revolving part, which is a rotating cylinder 5, which is vertically provided on the inside edge of pallet 1, the pallet
It is connected by rotating cylinder 5 thereon with fuselage rotation, pallet 1 is by rotating cylinder 5 with respect to fuselage with the first station and second station, place
When the first station, which is located at the top of fuselage with engine 8 thereon, when in second station, the pallet 1 and its
On engine 8 be located at the side of fuselage, when rotating cylinder 5 is rotated around pin shaft, pallet 1 and engine 8 thereon are from the first station
Second station is turned to, maintenance is facilitated.
Further, it is additionally provided with locking hole 7 far from the side of rotating cylinder 5 in pallet 1, the locking hole 7 and setting are in fuselage position
The hole at place is set to just, when pallet and fuselage are in the first station, pallet 1 is connected using bolt with fuselage, reaches locking support
In addition the purpose of disk 1 is arranged locking hole 7 and is further supported to pallet 1, avoids the position at far from rotating cylinder 5 on pallet 1
It has a down dip.
Pallet 1 and the hinged mode of fuselage can also be used in above-mentioned revolving part, and pallet is hinged with fuselage, using pallet 1 with
It is rotated between fuselage, engine rotation by pallet and thereon achievees the purpose that facilitate maintenance to the outside of fuselage.
Further, above-mentioned shock absorber part is used into rubber material damper 3, the damper of rubber material in the present embodiment
3 can be with damping vibration, and anti-vibration effect is more prominent, but the damper 3 of rubber material can not be directly connected to engine, therefore
In 3 upper end of damper of rubber material, setting stabilizer blade can support engine and solve can not be direct between engine and shock absorber part
The problem of connection.
Further, in the present embodiment by connector be with the same number of stabilizer blade 4 of support 2, and by stabilizer blade 4 with start
Machine 8 is bolted, and since stabilizer blade 4 is connected by the damper 3 of rubber material with support 4, is on the one hand shortened by support 4
The jib-length of 8 supporting leg of engine can mitigate the shaking of engine 8, improve stationarity；On the other hand it is arranged on support 2 and subtracts
Shake device 3 is simultaneously connected by stabilizer blade 4 with engine 8, and the damping effect of engine 8 is further improved.
Further, it is also additionally provided with to facilitate on pallet 1 in the present embodiment and pallet 1 is turned into the second work from the first station
Position when handle 6, handle 6 can easier engine 8 by pallet 1 and thereon be pulled to the one of fuselage from the top of fuselage
Side, more saving physical strength；In addition, also installing radiator 9 on pallet 1 at handle 6, corresponding 6 position of handle is taken full advantage of
Space on the pallet 1 at place, the layout of reasonable Arrangement engine 8 and radiator, structure are more compact.
The use process of the utility model are as follows:
When original state, engine passes through stabilizer blade 4 and connect with the damper of rubber material 3, the damper 3 of rubber material
It is connected with the support 2 on pallet 1, engine 8 and pallet 1 are located at the top of fuselage and by the bolt and fuselage in locking hole 7
It is connected up to the purpose of locking.When the failure of engine 8 needs repairing, the bolt in locking hole 7 is unloaded, handle 6 is caught,
Pallet 1 and engine 8 thereon are rotated by rotating cylinder 5 around pin shaft so that pallet 1 and engine 8 thereon are turned by the top of fuselage
To the outside of fuselage, so that maintenance personal facilitates maintenance；When maintenance finishes, handle 6 is caught, pallet 1 and engine thereon
8 are rotated by rotating cylinder 5 around pin shaft so that top by going to fuselage on the outside of fuselage, then by bolt pass through locking hole 7 with
Fuselage, which is connected, is locked.
The utility model prevents pallet 1 in far from rotation by the way that rotating cylinder 5 is being arranged on pallet 1 and is increasing locking hole 7
Lower hectare at the heart, when failure, can engine 8 by pallet 1 and thereon screw out, improve maintenance, operation convenience, save a large amount of
Working hour；In addition, four supports 2 are arranged on pallet 1,8 uniform force of engine can on the one hand be distributed, on the other hand can
The jib-length of 8 supporting leg of engine is shortened, shaking when engine 8 works is mitigated, the reliability machine for promoting 8 system of engine relaxes
Adaptive；Meanwhile the damper 3 that rubber material is arranged on support 2 is able to ascend damping performance.
Above-mentioned specific embodiment cannot function as the limitation to scope of protection of the utility model, for the skill of the art
For art personnel, any alternate modification or transformation made to the utility model embodiment all fall within the guarantor of the utility model
It protects in range.
Place is not described in detail for the utility model, is the well-known technique of those skilled in the art of the present technique.
Claims (8)
1. a kind of new engine installation system, for engine to be installed on fuselage, it is characterised in that: described including pallet
Pallet is connected by revolving part thereon and fuselage rotation, and the pallet is by revolving part with respect to fuselage with the first station and the
Two stations, when being in the first station, the pallet is located at the top of fuselage with the engine being mounted on pallet, is in the second work
When position, the pallet is located at the side of fuselage with the engine being mounted on pallet.
2. a kind of new engine installation system according to claim 1, it is characterised in that: be additionally provided on the pallet to
Few two supports, the support pass through shock absorber part respectively and are connected with connector, and the connector is connect with engine.
3. a kind of new engine installation system according to claim 1, it is characterised in that: be additionally provided with lock on the pallet
Tieholen, the locking hole are to lock pallet and fuselage by bolt when pallet and fuselage are in the first station.
4. a kind of new engine installation system according to claim 1, it is characterised in that: the revolving part includes setting
Pallet is connect by the rotating cylinder on the inside of pallet, the rotating cylinder by pin shaft with fuselage.
5. a kind of new engine installation system according to claim 2, it is characterised in that: the support is set as 4
And it is symmetricly set on the upper of pallet.
6. a kind of new engine installation system according to claim 2, it is characterised in that: the shock absorber part is and support
The same number of rubber block damper, the rubber block damper difference support are connected.
7. a kind of new engine installation system according to claim 2, it is characterised in that: the connector is and support
The same number of stabilizer blade, the stabilizer blade and rubber block damper are connected.
8. a kind of new engine installation system according to claim 1, it is characterised in that: be additionally provided on the outside of the pallet
Handle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822042696.0U CN209274345U (en) | 2018-12-06 | 2018-12-06 | A kind of new engine installation system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822042696.0U CN209274345U (en) | 2018-12-06 | 2018-12-06 | A kind of new engine installation system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209274345U true CN209274345U (en) | 2019-08-20 |
Family
ID=67609874
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822042696.0U Active CN209274345U (en) | 2018-12-06 | 2018-12-06 | A kind of new engine installation system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209274345U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111379623A (en) * | 2020-03-29 | 2020-07-07 | 安徽天沃重工机械有限公司 | Fixed protection frame capable of conveniently dissipating heat and adjusting position in sliding manner for diesel engine |
-
2018
- 2018-12-06 CN CN201822042696.0U patent/CN209274345U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111379623A (en) * | 2020-03-29 | 2020-07-07 | 安徽天沃重工机械有限公司 | Fixed protection frame capable of conveniently dissipating heat and adjusting position in sliding manner for diesel engine |
| CN111379623B (en) * | 2020-03-29 | 2021-01-15 | 安徽天沃重工机械有限公司 | Fixed protection frame capable of conveniently dissipating heat and adjusting position in sliding manner for diesel engine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209274345U (en) | A kind of new engine installation system | |
| CN204367864U (en) | A kind of engine mounting crossbeam assembly | |
| CN203511293U (en) | Gearbox suspension structure | |
| CN212889829U (en) | Battery bracket for new energy vehicle | |
| CN207450034U (en) | Combined type front-end module and apply its automobile | |
| CN201694255U (en) | Installation structure of front fender of automobile | |
| CN201484118U (en) | Installation auxiliary structure of automobile overhead evaporator | |
| CN203544142U (en) | Engine cover structure | |
| CN109050678B (en) | Shock attenuation tower assembly of vehicle and vehicle that has it | |
| CN204249770U (en) | Spring fixed support before a kind of | |
| CN103538636A (en) | Engine hood structure | |
| CN104369654A (en) | Multifunctional front suspension support for engine | |
| CN204296440U (en) | A kind of multifunctional engine front-suspension bracket | |
| CN206124723U (en) | Storage battery installing support | |
| CN202656972U (en) | Vehicle electronic control unit installation bracket and vehicle | |
| CN202783494U (en) | Rear suspension static load device of automobile | |
| CN205059128U (en) | A support for supporting engine air condition compressor | |
| CN204196642U (en) | A kind of integrated support structure | |
| CN205468379U (en) | Support assembly on shock absorber | |
| CN206012263U (en) | A kind of automotive air-conditioning condenser support | |
| CN214930550U (en) | Rotorcraft framework | |
| CN205930233U (en) | Rearmounted passenger car motor front end installation mechanism | |
| CN205365750U (en) | Enclose linking bridge assembly before car | |
| CN207712142U (en) | A kind of bracket of stop block | |
| CN218141791U (en) | Enclose upper portion assembly before strenghthened type car |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: No.2676 Kejia Road, high tech Zone, Jinan City, Shandong Province, 250104 Patentee after: Lingong Heavy Machinery Co.,Ltd. Address before: 250101 no.2676 Kejia Road, high tech Zone, Jinan City, Shandong Province Patentee before: LINGONG GROUP JINAN HEAVY MACHINERY Co.,Ltd. |