CN214242411U - Storage and transportation vehicle for aircraft engine - Google Patents
Storage and transportation vehicle for aircraft engine Download PDFInfo
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- CN214242411U CN214242411U CN202023108035.7U CN202023108035U CN214242411U CN 214242411 U CN214242411 U CN 214242411U CN 202023108035 U CN202023108035 U CN 202023108035U CN 214242411 U CN214242411 U CN 214242411U
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Abstract
The utility model relates to a store fortune equipment technical field, provide an aeroengine and store car, include: a main body frame; the front end of the main body frame is provided with a front supporting plate, and the rear end of the main body frame is provided with a rear supporting plate; the front support plate is arranged on the front support through the front support base plate; the rear support plate is provided with a rear support through a rear support bottom plate; hollow damping rubber blocks are respectively arranged in the front supporting plate and the rear supporting plate; and hollow damping rubber blocks are respectively arranged between the front support base plate and the front support plate and between the rear support base plate and the rear support plate. The utility model discloses can satisfy sealed nitrogen-filled packing box internal volume and install fixedly, promote the security of aeroengine in the transportation.
Description
Technical Field
The utility model relates to a store fortune equipment technical field, especially relate to an aeroengine stores car.
Background
The aeroengine is in the transportation, need to be equipped with sealed packing box of filling nitrogen, makes the engine not damaged in the transportation.
At present, a special rack is used for transferring an aviation engine, and the size of the rack is too large to meet the requirements of internal storage of a sealed nitrogen-filled packing box and external storage and transportation.
SUMMERY OF THE UTILITY MODEL
The utility model discloses mainly solve the technical problem that prior art's special rack volume of aircraft engine is too big can't satisfy sealed nitrogen-filled packing box inside storage and the technical problem that the outfield stored and transported and use, provide an aeroengine and store the car to it is fixed to satisfy sealed inside volume of nitrogen-filled packing box and installation, promotes the security of aeroengine in the transportation.
The utility model provides an aeroengine storage vehicle, include: a main body frame;
the front end of the main body frame is provided with a front supporting plate, and the rear end of the main body frame is provided with a rear supporting plate;
the front support plate is arranged on the front support through the front support base plate;
the rear support plate is provided with a rear support through a rear support bottom plate;
hollow damping rubber blocks are respectively arranged in the front supporting plate and the rear supporting plate;
and hollow damping rubber blocks are respectively arranged between the front support base plate and the front support plate and between the rear support base plate and the rear support plate.
Preferably, the front supporter includes two supporting units;
each of the supporting units includes: two support rods and a connecting column; the support rod is connected with the connecting column through a reinforcing rod;
the supporting rod is provided with a guide post in threaded connection, and a guide post handle is arranged on the guide post;
the support rods of the two support units are in a straight line.
Preferably, the rear mount includes: the locking device comprises a locking device seat, a supporting block, a locking bolt, a positioning block, a first wedge-shaped locking block and a second wedge-shaped locking block;
the locking device seat is arranged on the rear support base plate, and a supporting block is arranged on the locking device seat;
a positioning block is arranged at the center of the supporting block;
a first wedge-shaped locking block and a second wedge-shaped locking block are respectively arranged at two ends of the supporting block;
the locking bolt sequentially penetrates through the first wedge-shaped locking block, the positioning block and the second wedge-shaped locking block.
Preferably, the front end of the bottom surface of the main body frame is provided with two directional polyurethane casters, and the rear end of the bottom surface of the main body frame is provided with two universal polyurethane casters.
Preferably, the hollow damping rubber block is olive-shaped.
The utility model provides a pair of aeroengine storage vehicle has following advantage compared with prior art:
1. the engine is mainly installed and fixed on a pivot and combined with the storage and transportation vehicle, and the size is reduced, so that the internal storage of the sealed nitrogen-filled packaging box and the flexible movement of the short-distance engine in the field can be met, and the limit of the field is avoided.
2. The hollow damping rubber block is arranged at the main fulcrum, the damping effect is achieved by utilizing the cavity damping principle, the vibration generated in the moving process of the storage vehicle is effectively filtered, and the engine is not damaged.
Drawings
FIG. 1 is a schematic view of the structure of an aircraft engine storage vehicle provided by the present invention;
FIG. 2 is a top view of an aircraft engine storage vehicle provided by the present invention;
FIG. 3 is a top view of a main body frame of the storage and transportation vehicle provided by the present invention;
fig. 4 is a schematic structural view of a front support provided by the present invention;
FIG. 5 is a cross-sectional view of the rear mount provided by the present invention along an axis;
fig. 6 is a cross-sectional view of the hollow cushion rubber block along the axis.
Reference numerals: 1. a main body frame of the storage and transportation vehicle; 2. a front support; 3. a rear support; 4. a hollow damping rubber block; 5. universal polyurethane casters; 6. a directional polyurethane caster; 7. a rear support base plate; 8. a rear support plate; 9. a front support base plate; 10. a front support plate; 201. a support bar; 202. a reinforcing bar; 203. a guide post; 204. a guide post handle; 205. a reinforcing rod connecting column; 301. locking the bolt; 302. a wedge-shaped locking block; 303. a locking device seat; 304. a support block; 305. and (5) positioning the blocks.
Detailed Description
In order to make the technical problem solved by the present invention, the technical solution adopted by the present invention and the technical effect achieved by the present invention clearer, the present invention will be further described in detail with reference to the accompanying drawings and the embodiments. It is to be understood that the specific embodiments described herein are merely illustrative of the invention and are not limiting of the invention. It should be further noted that, for the convenience of description, only some but not all of the relevant portions of the present invention are shown in the drawings.
As shown in fig. 1-2, the embodiment of the present invention provides an aircraft engine storage vehicle, including: a storage vehicle main body frame 1;
as shown in fig. 3, the main body frame 1 has a front support plate 10 at the front end and a rear support plate 8 at the rear end. The bottom surface front end of main body frame 1 sets up two directional polyurethane truckles 6, the bottom surface rear end of main body frame 1 sets up two universal polyurethane truckles 5.
The front support plate 10 is arranged on the front support 2 through a front support bottom plate 9; the rear support plate 8 is provided with a rear support 3 through a rear support bottom plate 7; the inside cavity of preceding backup pad 10, back backup pad 8, set up cavity cushion rubber 4 in preceding backup pad 10, the back backup pad 8 respectively. And hollow damping rubber blocks 4 are respectively arranged between the front support base plate 9 and the front support plate 10 and between the rear support base plate 7 and the rear support plate 8. As shown in fig. 6, the hollow cushion rubber block 4 is olive-shaped. In the embodiment, the hollow damping rubber block 4 is arranged at the main fulcrum, and the hollow damping rubber block plays a role in damping by utilizing a cavity damping principle, so that the vibration generated in the moving process of the storage vehicle is effectively filtered.
As shown in fig. 4, the front mount 2 includes two support units; each of the supporting units includes: two support rods 201 and a connecting column 205; the supporting rod 201 is connected with the connecting column 205 through a reinforcing rod 202; two support rods 201 and a connecting column 205 are distributed in a triangular shape. The support bars 201 of the two support units are in a straight line. A guide post 203 connected with the support rod 201 through threads is arranged on the support rod, and a guide post handle 204 is arranged on the guide post 203; when the engine is not being transported, the guide posts 203 can be removed. The guide posts 203 can facilitate positioning during engine installation.
As shown in fig. 5, the rear mount 3 includes: a locking device base 303, a support block 304, a locking bolt 301, a positioning block 305, a first wedge-shaped locking block 302 and a second wedge-shaped locking block 306; the locking device base 303 is arranged on the rear support base plate 7, and the locking device base 303 is provided with a supporting block 304; a positioning block 305 is arranged at the center of the supporting block 304; the positioning block 305 can position the rear of the engine. A first wedge-shaped locking block 302 and a second wedge-shaped locking block 306 are respectively arranged at two ends of the supporting block 304; the locking bolt 301 passes through a first wedge-shaped locking block 302, a positioning block 305 and a second wedge-shaped locking block 306 in sequence. Tightening of the locking bolt 301 locks the first and second wedge lock blocks 302 and 306 to the support block 304. The wedge-shaped design of the rear support 3 can realize automatic clamping of the rear mounting point of the engine when the fixing bolt is locked.
The working process of the aircraft engine storage vehicle of the embodiment is as follows: an engine is placed on a main body frame, the front end of the engine is placed on the front support 2, the rear end of the engine is placed on the rear support 3, and the guide pillar 203 penetrates through a front mounting point of the engine and extends into the support rod 201 to be screwed down, so that the front end of the engine is locked; tightening the locking bolt 301 locks the rear end of the engine by means of the first and second wedge-shaped locking blocks 302, 306.
The aero-engine storage and transportation vehicle of the embodiment combines the main fixed pivot of the engine with the storage and transportation vehicle, reduces the volume, and can meet the requirements of the internal storage of a sealed nitrogen-filled packing box and the flexible movement of a short-distance engine in a field, wherein four polyurethane trundles are arranged at the bottom of the storage and transportation vehicle, and two universal polyurethane trundles are arranged at the rear pivot, so that the turning of the storage and transportation vehicle in the moving process can be realized, and the movement is more flexible. The hollow shock-absorbing rubber blocks 4 are arranged at main fulcrum positions such as among the front support plate 10, the rear support plate 8, the front support base plate 9 and the front support plate 10, and between the rear support base plate 7 and the rear support plate 8 to play a shock-absorbing role, so that the shock generated in the moving process of the storage vehicle is effectively filtered to play a role in protecting an engine. In the embodiment, each component is fixedly connected with the main body frame 1 by using the bolt, so that the components are convenient to maintain and repair in the future.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: it is to be understood that modifications may be made to the technical solutions described in the foregoing embodiments, or some or all of the technical features may be equivalently replaced, without substantially departing from the scope of the technical solutions of the embodiments of the present invention.
Claims (5)
1. An aircraft engine storage vehicle, comprising: a main body frame (1);
the front end of the main body frame (1) is provided with a front supporting plate (10), and the rear end is provided with a rear supporting plate (8);
the front support plate (10) is provided with a front support (2) through a front support bottom plate (9);
the rear support plate (8) is provided with a rear support (3) through a rear support bottom plate (7);
the front support plate (10) and the rear support plate (8) are respectively provided with a hollow damping rubber block (4);
and hollow damping rubber blocks (4) are respectively arranged between the front support base plate (9) and the front support plate (10) and between the rear support base plate (7) and the rear support plate (8).
2. The aircraft engine storage trolley according to claim 1, characterized in that said front seat (2) comprises two support units;
each of the supporting units includes: two support rods (201) and a connecting column (205); the supporting rod (201) is connected with the connecting column (205) through a reinforcing rod (202);
a guide post (203) in threaded connection is arranged on the supporting rod (201), and a guide post handle (204) is arranged on the guide post (203);
the support rods (201) of the two support units are in a straight line.
3. The aircraft engine storage trolley according to claim 1 or 2, characterized in that said rear support (3) comprises: the locking device comprises a locking device base (303), a supporting block (304), a locking bolt (301), a positioning block (305), a first wedge-shaped locking block (302) and a second wedge-shaped locking block (306);
the locking device base (303) is arranged on the rear support base plate (7), and the locking device base (303) is provided with a supporting block (304);
a positioning block (305) is arranged at the central position of the supporting block (304);
a first wedge-shaped locking block (302) and a second wedge-shaped locking block (306) are respectively arranged at two ends of the supporting block (304);
the locking bolt (301) sequentially penetrates through the first wedge-shaped locking block (302), the positioning block (305) and the second wedge-shaped locking block (306).
4. The aircraft engine storage trolley according to claim 1 or 2, wherein the front end of the bottom surface of the main body frame (1) is provided with two directional polyurethane casters (6), and the rear end of the bottom surface of the main body frame (1) is provided with two universal polyurethane casters (5).
5. The aircraft engine storage trolley according to claim 1 or 2, characterized in that said hollow shock-absorbing rubber block (4) is olive-shaped.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023108035.7U CN214242411U (en) | 2020-12-22 | 2020-12-22 | Storage and transportation vehicle for aircraft engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023108035.7U CN214242411U (en) | 2020-12-22 | 2020-12-22 | Storage and transportation vehicle for aircraft engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214242411U true CN214242411U (en) | 2021-09-21 |
Family
ID=77740582
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023108035.7U Active CN214242411U (en) | 2020-12-22 | 2020-12-22 | Storage and transportation vehicle for aircraft engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214242411U (en) |
-
2020
- 2020-12-22 CN CN202023108035.7U patent/CN214242411U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Aeroengine storage and transportation vehicle Effective date of registration: 20220615 Granted publication date: 20210921 Pledgee: Industrial and Commercial Bank of China Limited Dalian Lvshunkou sub branch Pledgor: Dalian Shunjin FRP Products Co.,Ltd. Registration number: Y2022980007787 |