CN207583497U - A kind of protective cover of aviation ground servicing equipment engine spindle - Google Patents
A kind of protective cover of aviation ground servicing equipment engine spindle Download PDFInfo
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- CN207583497U CN207583497U CN201721801769.9U CN201721801769U CN207583497U CN 207583497 U CN207583497 U CN 207583497U CN 201721801769 U CN201721801769 U CN 201721801769U CN 207583497 U CN207583497 U CN 207583497U
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- frame
- connection axis
- protective
- protective cover
- inner cavity
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Abstract
The utility model discloses a kind of protective covers of aviation ground servicing equipment engine spindle, including protective frame, protect cover main body and ventilation frame, the protective frame is mounted on protective cover body front end, protective frame inner cavity bottom end is equipped with bumper bracket, the bumper bracket is fixedly arranged at the front end with steel plate, steel plate center inner end is elasticly connected with flexible bumper frame, the ventilation is erected at protective cover main center position, the ventilation frame inner cavity is equipped with wind shield, the wind shield lower end offers connectivity slot, the wind shield side is connected with link, link inner cavity bottom end is equipped with fixed frame, the fixed frame front end is plugged with inserted link, the first connection axis is connected on the outside of the inserted link, the first connection axis side is equipped with the second connection axis, the ventilation frame side is equipped with petroleum pipeline, the oil transportation tube cavity is equipped with fastening plates.The utility model realizes the purpose of convenient oil transportation by the setting of petroleum pipeline.
Description
Technical field
The utility model is related to engine apparatus technical field, specially a kind of guarantor of aviation ground servicing equipment engine spindle
Shield.
Background technology
The protective cover of aviation ground servicing equipment engine spindle can help to carry out engine protection work, solve traditional protection
The inconvenience of cover, while can conveniently be detected, more environment are adapted to, it is time saving and energy saving to have achieved the purpose that, facilitates and is tieed up
Work is repaiied, ensures the quality of product, but the protective cover of the ground servicing equipment engine spindle of aviation at present has the following problems：
First, in the presence of the transmission work for being not easy to carry out fluid so that the phenomenon that will appear leakage during oil transportation can cause one
Fixed inconvenience second is that the protection of engine and anticollision work can not be carried out, needs to be improved.
Utility model content
It is above-mentioned to solve the purpose of this utility model is to provide a kind of protective cover of aviation ground servicing equipment engine spindle
The problem of being proposed in background technology.
To achieve the above object, the utility model provides following technical solution：A kind of aviation ground servicing equipment engine spindle
Protective cover, including protective frame, protection cover main body and ventilation frame, the protective frame is mounted on protective cover body front end, described anti-
Retaining frame inner cavity bottom end is equipped with bumper bracket, and the bumper bracket is fixedly arranged at the front end with steel plate, and steel plate center inner end is elasticly connected with
Flexible bumper frame, the ventilation are erected at protective cover main center position, and the ventilation frame inner cavity is equipped with wind shield, described to keep out the wind
Plate lower end offers connectivity slot, and the wind shield side is connected with link, and link inner cavity bottom end is equipped with fixed frame, institute
It states fixed frame front end and is plugged with inserted link, the first connection axis is connected on the outside of the inserted link, the first connection axis side is set
There is the second connection axis, the ventilation frame side is equipped with petroleum pipeline, and the oil transportation tube cavity is equipped with fastening plates, under the fastening plates
End is communicated with telescoping tube, and convex block is equipped on the outside of the telescoping tube, and the protection cover main body outer end is socketed with guard shield.
Preferably, the convex block of the petroleum pipeline inner end is mutually welded with guard shield.
Preferably, the link is mutually fixed by the first connection axis and the second connection axis with wind shield.
Preferably, the second connection axis arc diameter is less than the first connection axis arc diameter.
Preferably, the flexible bumper frame is equipped with two groups, and is symmetrical arranged by steel plate.
Preferably, the bumper bracket inner end is equipped with gap.
Compared with prior art, the beneficial effects of the utility model are：
1st, by installing ventilation frame and link, the wind shield of ventilation frame inner cavity realizes outer end connection work, and wind shield is dashed forward
Go out the surface of guard shield, and wind shield lower end offers connectivity slot, be connected by connectivity slot with inner end engine, realize wind
Cold purpose, air-flow reach the inner end of protection cover main body by connectivity slot, realize the purpose of heat dissipation, the connection of wind shield side
Frame realizes the work that is fixedly connected of wind shield, and link connects axis by the first of side and the second connection axis connects
It connects frame and realizes fixation with wind shield, by tightening the distance of the first connection axis and the second connection axis, realize fixed work, make
It obtains inner end and is convenient for ventilative work.
2nd, by installing petroleum pipeline, oil transportation tube cavity is equipped with fastening plates, and fastening plates lower end connection telescoping tube, passes through fastening
Telescoping tube can be carried out drawing work by plate user so that drive the elongation of telescoping tube, telescoping tube is set for elastic material, and bottom
End is connected with engine oil filler point, realizes the oil transportation work of inner end, and fastening plates are set using dish-type so that can be straight with oil bottle
The phenomenon that connecing in succession, preventing from spilling, telescoping tube outside are equipped with convex block, and convex block is mutually welded with guard shield, are realized by convex block outer
End protection, when not needing to oil transportation, user can realize the compression work of telescoping tube, and convex block is with stretching by pressing telescoping tube
The fastening plates on draw top are mutually clamped, and are realized that work is fixed in outer end, are convenient for the transmission work of fluid so that during oil transportation more
Safety.
3rd, by installing protective frame, the bumper bracket of protective frame inner cavity bottom end realizes protected working, prevents outer end body from occurring
The phenomenon that collision, causes the damage of inner end, and bumper bracket gap of inner end, realizes the function of isolating and protecting, realizes the buffering of inner end,
And the steel plate center inner end of bumper bracket front end is elasticly connected with flexible bumper frame, bumper frame of stretching is equipped with two groups, by flexible anti-
It hits frame and can absorb extra stress so that reduce internal damage, realize the protected working of inner end engine so that protection is more
What is added is thorough, helps to carry out the protection of engine and anticollision work.
Description of the drawings
Fig. 1 is the utility model agent structure schematic diagram；
Fig. 2 is the utility model ventilation frame structure diagram；
Fig. 3 is the utility model connecting frame structure schematic diagram；
Fig. 4 is the utility model petroleum pipeline structure diagram；
Fig. 5 is the utility model protective frame structure diagram.
In figure：1- protective frames；2- petroleum pipelines；3- guard shields；4- protects cover main body；5- ventilation frames；6- wind shields；7- connects
Straight slot；8- links；9- fixed frames；The connection axis of 10- first；The connection axis of 11- second；12- inserted links；13- fastening plates；14-
Telescoping tube；15- convex blocks；16- bumper brackets；17- stretches bumper frame；18- steel plates.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
It clearly and completely describes, it is clear that the described embodiments are only a part of the embodiments of the utility model rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are without making creative work
All other embodiments obtained shall fall within the protection scope of the present invention.
- 5 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of guarantor of aviation ground servicing equipment engine spindle
Shield, including protective frame 1, protection cover main body 4 and ventilation frame 5, protective frame 1, which is mounted on, protects 4 front end of cover main body, in protective frame 1
Bottom of chamber end is equipped with bumper bracket 16, and bumper bracket 16 is fixedly arranged at the front end with steel plate 18, and 18 center inner end of steel plate is elasticly connected with flexible anti-
Frame 17 is hit, by installing protective frame 1, the bumper bracket 16 of 1 inner cavity bottom end of protective frame realizes protected working, prevents outer end body from going out
The phenomenon that now colliding causes the damage of inner end, and 16 gap of inner end of bumper bracket, realizes the function of isolating and protecting, realize inner end
Buffering, and the 18 center inner end of steel plate of 16 front end of bumper bracket is elasticly connected with flexible bumper frame 17, bumper frame 17 of stretching is equipped with two
Group can absorb extra stress so that reduce internal damage, realize the anti-nurse of inner end engine by flexible bumper frame 17
Make so that protection it is more thorough, help to carry out the protection of engine and anticollision work, ventilation frame 5 is located at protective cover master
4 center of body, 5 inner cavity of ventilation frame are equipped with wind shield 6, and 6 lower end of wind shield offers connectivity slot 7, and 6 side of wind shield is connected with
Link 8,8 inner cavity bottom end of link are equipped with fixed frame 9, and 9 front end of fixed frame is plugged with inserted link 12, and 12 outside of inserted link is connected with the
One connection axis 10, the first 10 side of connection axis are equipped with the second connection axis 11, and 5 side of ventilation frame is equipped with petroleum pipeline 2, oil transportation
2 inner cavity of pipe is equipped with fastening plates 13, and 13 lower end of fastening plates is communicated with telescoping tube 14, and 14 outside of telescoping tube is equipped with convex block 15, passes through peace
Petroleum pipeline 2 is filled, 2 inner cavity of petroleum pipeline is equipped with fastening plates 13, and 13 lower end of fastening plates connection telescoping tube 14, is used by fastening plates 13
Telescoping tube 14 can be carried out drawing work by person so that drive the elongation of telescoping tube 14, telescoping tube 14 is set for elastic material, and bottom
End is connected with engine oil filler point, realizes the oil transportation work of inner end, and fastening plates 13 are set using dish-type so that can be with oil bottle
The phenomenon that being directly connected to, preventing from spilling, 14 outside of telescoping tube are equipped with convex block 15, and convex block 15 is welded with 3 phase of guard shield, by convex
Block 15 realizes outer end protection, and when not needing to oil transportation, user can realize the compression work of telescoping tube 14 by pressing telescoping tube 14
Make, and convex block 15 and 13 phase of fastening plates on 14 top of telescoping tube are clamped, and are realized that work is fixed in outer end, are convenient for the transmission of fluid
Work so that more safe during oil transportation, 4 outer end of protection cover main body is socketed with guard shield 3.
The convex block 15 of 2 inner end of petroleum pipeline is welded with 3 phase of guard shield, and link 8 passes through the first connection axis 10 and second
Connection axis 11 is fixed with 6 phase of wind shield, and the second 11 arc diameter of connection axis is less than the first connection 10 arc diameter of axis, bumper frame of stretching
17 are equipped with two groups, and be symmetrical arranged by steel plate 18, and 16 inner end of bumper bracket is equipped with gap.
Operation principle：When needing work, by installing ventilation frame 5 and link 8, the wind shield 6 of 5 inner cavity of ventilation frame,
Realize outer end connection work, wind shield 6 protrudes the surface of guard shield 3, and 6 lower end of wind shield offers connectivity slot 7, passes through company
Straight slot 7 is connected with inner end engine, realizes air-cooled purpose, and air-flow reaches the inner end of protection cover main body 4 by connectivity slot 7,
Realize the purpose of heat dissipation, the link 8 of 6 side of wind shield, that realizes wind shield 6 is fixedly connected with work, and link 8 passes through side
The first connection axis 10 and second connect axis 11 so that link 8 and wind shield 6 are realized fixes, by tightening the first connection
Axis 10 and second connects the distance of axis 11, realizes fixed work so that inner end is convenient for ventilative work, defeated by installing
Oil pipe 2,2 inner cavity of petroleum pipeline are equipped with fastening plates 13, and 13 lower end of fastening plates connection telescoping tube 14, and by fastening plates, 13 user can
Telescoping tube 14 is subjected to drawing work so that drive telescoping tube 14 elongation, telescoping tube 14 for elastic material set, and bottom end and
Engine oil filler point is connected, and realizes the oil transportation work of inner end, and fastening plates 13 are set using dish-type so that can be direct with oil bottle
Connection, the phenomenon that preventing from spilling, 14 outside of telescoping tube is equipped with convex block 15, and convex block 15 is welded with 3 phase of guard shield, passes through convex block 15
Realize outer end protection, when not needing to oil transportation, user can realize the compression work of telescoping tube 14 by pressing telescoping tube 14,
And convex block 15 and 13 phase of fastening plates on 14 top of telescoping tube are clamped, and are realized that work is fixed in outer end, are convenient for the transmission work of fluid
Make so that more safe during oil transportation, by installing protective frame 1, the bumper bracket 16 of 1 inner cavity bottom end of protective frame realizes anti-nurse
The phenomenon that making, preventing outer end body from colliding causes the damage of inner end, and 16 gap of inner end of bumper bracket, realizes isolating and protecting
Function, realize the buffering of inner end, and the 18 center inner end of steel plate of 16 front end of bumper bracket is elasticly connected with flexible bumper frame 17, stretches
Contracting bumper frame 17 is equipped with two groups, and extra stress is can absorb by flexible bumper frame 17 so that internal damage is reduced, in realization
Hold engine protected working so that protection it is more thorough, help carry out engine protection and anticollision work, complete
Work.
While there has been shown and described that the embodiment of the utility model, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case of the principle and spirit for not departing from the utility model, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of protective cover of aviation ground servicing equipment engine spindle, including protective frame (1), protection cover main body (4) and ventilation frame
(5), it is characterised in that：The protective frame (1) is mounted on protection cover main body (4) front end, protective frame (1) the inner cavity bottom end installation
There is bumper bracket (16), the bumper bracket (16) is fixedly arranged at the front end with steel plate (18), and steel plate (18) the center inner end is elasticly connected with
Flexible bumper frame (17), the ventilation frame (5) are located at protection cover main body (4) center, and ventilation frame (5) inner cavity is equipped with gear
Aerofoil (6), wind shield (6) lower end offer connectivity slot (7), and wind shield (6) side is connected with link (8), institute
Link (8) inner cavity bottom end is stated equipped with fixed frame (9), fixed frame (9) front end is plugged with inserted link (12), the inserted link (12)
Outside is connected with the first connection axis (10), and described first connection axis (10) side is equipped with the second connection axis (11), described
Ventilation frame (5) side is equipped with petroleum pipeline (2), and petroleum pipeline (2) inner cavity is equipped with fastening plates (13), fastening plates (13) lower end
Telescoping tube (14) is communicated with, convex block (15) is equipped on the outside of the telescoping tube (14), described protection cover main body (4) outer end is socketed with anti-
Protect shell (3).
2. a kind of protective cover of aviation ground servicing equipment engine spindle according to claim 1, it is characterised in that：It is described defeated
The convex block (15) of oil pipe (2) inner end is mutually welded with guard shield (3).
3. a kind of protective cover of aviation ground servicing equipment engine spindle according to claim 1, it is characterised in that：The company
Frame (8) is connect mutually to fix with wind shield (6) by the first connection axis (10) and the second connection axis (11).
4. a kind of protective cover of aviation ground servicing equipment engine spindle according to claim 1, it is characterised in that：Described
Two connection axis (11) arc diameters are less than first connection axis (10) arc diameter.
5. a kind of protective cover of aviation ground servicing equipment engine spindle according to claim 1, it is characterised in that：It is described to stretch
Contracting bumper frame (17) is symmetrical arranged equipped with two groups, and by steel plate (18).
6. a kind of protective cover of aviation ground servicing equipment engine spindle according to claim 1, it is characterised in that：It is described slow
Frame (16) inner end is rushed equipped with gap.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721801769.9U CN207583497U (en) | 2017-12-21 | 2017-12-21 | A kind of protective cover of aviation ground servicing equipment engine spindle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721801769.9U CN207583497U (en) | 2017-12-21 | 2017-12-21 | A kind of protective cover of aviation ground servicing equipment engine spindle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207583497U true CN207583497U (en) | 2018-07-06 |
Family
ID=62739297
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721801769.9U Active CN207583497U (en) | 2017-12-21 | 2017-12-21 | A kind of protective cover of aviation ground servicing equipment engine spindle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207583497U (en) |
-
2017
- 2017-12-21 CN CN201721801769.9U patent/CN207583497U/en active Active
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