CN215057764U - Snow removing and deicing equipment for large-scale front-mounted turbojet engine - Google Patents
Snow removing and deicing equipment for large-scale front-mounted turbojet engine Download PDFInfo
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- CN215057764U CN215057764U CN202121536645.9U CN202121536645U CN215057764U CN 215057764 U CN215057764 U CN 215057764U CN 202121536645 U CN202121536645 U CN 202121536645U CN 215057764 U CN215057764 U CN 215057764U
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Abstract
The utility model relates to a large-scale forward type turbojet engine snow removing and deicing equipment, it includes: the ground wheel is arranged at the bottom of the frame and is used for being arranged at the front end of the carrier vehicle; the suspension arm is fixedly connected with the rack; snow removing device, snow removing device are located the outside of frame, and it includes: the support is in rotary connection with the suspension arm through the rotating mechanism; the turbojet engine can be suspended on the bracket in a pitching mode through the pitching mechanism; the turbojet engine is used for removing snow and frost, the rotating mechanism is used for driving the bracket to rotate, and the bracket is used for driving the turbojet engine to rotate when rotating; the pitch mechanism is used to adjust the pitch angle of the turbojet engine. The equipment can accurately and effectively remove snow and freeze in all directions on roads, buildings, mechanical equipment, traffic equipment and engineering equipment, thereby ensuring the normal operation and safety of the facility equipment.
Description
Technical Field
The utility model relates to the technical field of mechanical device, especially, relate to a snow removing and deicing equipment of large-scale forward type turbojet engine.
Background
The low-temperature snowfall and freezing in winter in cold areas not only bring serious influence to smooth roads, but also cause the problem that large equipment (such as mechanical equipment and engineering equipment) and the like cannot be started and used under the condition of low temperature, and bring great inconvenience and danger to life and production.
At present, the ice and snow removing technology mainly comprises an artificial removing method, a mechanical snow removing method, a chemical method and the like. The manual elimination method is the most traditional snow removal method, namely, the accumulated snow and the ice are removed by using manpower, but the manpower consumption is high, and the deicing efficiency is low; the mechanical snow removing method can rapidly remove ice and snow in an open area by means of shoveling, scraping and the like, but has no capacity for special road sections, narrow areas and the like; chemical methods remove snow and ice by salt or alcohol snow-melting agents, but the efficiency is low, and the salt snow-melting agents are corrosive and have destructive influence on the removal area after long-term use.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a large-scale forward type turbojet engine snow removing deicing equipment to solve the problem that provides among the above-mentioned background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
a snow and freeze removing device for a large front-mounted turbojet engine comprises:
the ground wheel is arranged at the bottom of the frame and is used for being arranged at the front end of the carrier vehicle;
the suspension arm is fixedly connected with the rack;
snow removing device, snow removing device is located the outside of frame, it includes: the support is in rotary connection with the suspension arm through the rotating mechanism; the turbojet engine is suspended on the bracket in a pitching mode through a pitching mechanism;
the turbojet engine is used for removing snow and frost, the rotating mechanism is used for driving the bracket to rotate, and the bracket is used for driving the turbojet engine to rotate when rotating; the pitch mechanism is used to adjust the pitch angle of the turbojet engine.
As a further improvement of the present invention, the support includes a horizontal cross plate and two opposite side plates disposed below the horizontal cross plate.
As a further improvement of the present invention, the rotating mechanism includes: the device comprises a rotating shaft, a first gear and a first driving motor;
the bottom of the rotating shaft is fixedly connected with the support, the top of the rotating shaft penetrates through the suspension arm, the first gear is sleeved on the rotating shaft and located above the suspension arm, and the first driving motor is connected with the first gear;
the first driving motor is used for driving the first gear to rotate when the first driving motor is started, and the first gear is used for driving the rotating shaft to rotate when the first driving motor rotates, so that the support is driven to rotate.
As a further improvement of the present invention, the pitch mechanism includes: the hinge shaft, the second gear and the second driving motor are fixedly connected with the upper part of the turbojet engine;
the two ends of the hinge shaft are respectively fixed on the two vertical side plates, the second gear is sleeved on the hinge shaft, and the second driving motor is connected with the second gear;
the second driving motor is used for driving the second gear to rotate when the turbojet engine is started, and the second gear is used for driving the hinge shaft to rotate when the second gear rotates, so that the pitching angle of the turbojet engine is changed.
As a further improvement, the one end of davit with frame fixed connection, the other end is to keeping away from the direction of frame extends, snow removing device with the other end of davit is connected.
As a further improvement, the both ends of davit are all to keeping away from the direction of frame extends, snow removing device respectively with the both ends of davit correspond the connection.
As a further improvement of the present invention, the range of rotation angle of the turbojet engine is 0 ° -180 °.
As a further improvement, the turbojet pitch angle range is 0 DEG to 45 deg.
Adopt the produced beneficial effect of above-mentioned technical scheme to lie in:
the embodiment of the utility model provides a snow removing deicing equipment arranges carrier vehicle the place ahead in during use, and the driver can audio-visual operation condition of observing this equipment, and is simple high-efficient. The carrier vehicle can be a wheeled vehicle or a tracked vehicle, and can also be a fuel internal combustion locomotive or an electric drive vehicle.
When the device works, the turbojet engine can generate high-speed airflow at the temperature of 800 ℃ when working, the turbojet engine is driven to rotate through the rotating mechanism, the pitching angle of the turbojet engine is adjusted through the pitching mechanism, multi-angle adjustment of the upper nozzle of the turbojet engine is achieved, snow and frost can be removed from roads, buildings, mechanical equipment, traffic equipment and engineering equipment accurately and effectively in an all-dimensional manner, and therefore normal operation and safety of the equipment are guaranteed.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the technical solutions in the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is an installation front view of snow and freeze removing equipment for a large front-mounted turbojet engine provided by an embodiment of the invention.
Fig. 2 is an installation front view of the snow and ice removing device of the single-engine large-scale front-mounted turbojet engine provided by the embodiment of the invention.
Fig. 3 is an installation front view of the snow and ice removing device of the double-engine large front turbojet engine provided by the embodiment of the invention.
Fig. 4 is a display diagram of the double-engine large-scale front-mounted turbojet engine snow removing and deicing device boom extending to both sides.
Fig. 5 is a schematic structural view of a snow removing device provided by an embodiment of the present invention.
Fig. 6 is a schematic view of a turbojet pitch provided by an embodiment of the present invention.
Wherein: the snow removing device comprises a 100-carrier vehicle, a 1 frame, 101 ground wheels, 2 suspension arms, 3 snow removing devices, a 301 support, a 301-1 horizontal transverse plate, a 301-2 vertical side plate, a 302 rotating mechanism, a 302-1 rotating shaft, a 302-2 first gear, a 303 pitching mechanism, a 303-1 hinging shaft, a 303-2 second gear, a 304 turbojet engine and a 304-1 nozzle.
Detailed Description
To make the objects, aspects and advantages of the present invention clearer, and in accordance with the following detailed description of certain embodiments of the present invention, it is to be understood that the terms "center," "vertical," "horizontal," "up," "down," "front," "back," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientation or positional relationship shown in the accompanying drawings, which are used for convenience of description and simplicity of illustration, and are not intended to indicate or imply that the device or element so referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the present invention.
The embodiment of the utility model provides a large-scale forward type turbojet engine snow removing and deicing equipment, as shown in fig. 1-6, it includes:
the vehicle comprises a frame 1, wherein the bottom of the frame 1 is provided with a land wheel 101 which is used for being arranged at the front end of a carrier vehicle 100;
the suspension arm 2 is fixedly connected with the frame 1;
the turbojet engine 304 is used for snow removal and freeze removal, the rotating mechanism 302 is used for driving the support to rotate, and the support is used for driving the turbojet engine 304 to rotate when rotating; pitching mechanism 303 is used to adjust the pitch angle of turbojet engine 304.
Further, in order to ensure more effective and accurate operation of the turbine engine, as shown in fig. 6, the pitch angle range a of the turbojet engine 304 is 0 ° -45 °, that is, the maximum included angle between the axes of the turbojet engine 304 when the turbojet engine 304 is in the state of tilting down to the maximum and when the turbojet engine 304 is in the state of tilting up to the maximum is 45 °; in addition, as shown in fig. 5, the range of the rotation angle of turbojet engine 304 is 0 ° to 180 °, that is, turbojet engine 304 can rotate about the axis of rotating shaft 302-1 by 0 ° to 90 ° in the left direction and 0 ° to 90 ° in the right direction.
The embodiment of the utility model provides a snow removing deicing equipment arranges carrier vehicle 100 the place ahead in during the use, and the driver can audio-visual operation condition of observing this equipment, and is simple high-efficient. The carrier vehicle 100 may be a wheeled vehicle or a tracked vehicle, and may also be a fuel-powered diesel locomotive or an electrically driven vehicle.
When the turbojet engine 304 works, high-speed airflow up to 800 ℃ can be generated, the turbojet engine 304 is driven to rotate through the rotating mechanism 302, the pitching angle of the turbojet engine 304 is adjusted through the pitching mechanism 303, multi-angle adjustment of a nozzle 304-1 on the turbojet engine 304 is achieved, snow and frost can be accurately and effectively removed from roads, buildings, mechanical equipment, traffic equipment and engineering equipment in an all-dimensional manner, and therefore normal operation and safety of the facility equipment are guaranteed.
In one possible implementation, as shown in fig. 5, the bracket includes a horizontal cross plate 301-1 and two vertical side plates 301-2 disposed opposite to each other and located below the horizontal cross plate 301-1.
As for the structure of the rotating mechanism 302, as shown in fig. 5, the rotating mechanism 302 includes: a rotating shaft 302-1, a first gear 302-2, and a first driving motor;
wherein, the bottom of the rotating shaft 302-1 is fixedly connected with the bracket (specifically, the horizontal transverse plate 301-1), the top passes through the suspension arm 2, the first gear 302-2 is sleeved on the rotating shaft 302-1 and is located above the suspension arm 2, and the first driving motor is connected with the first gear 302-2, for example: first driving motor passes through sprocket chain structure and first gear connection, perhaps through another and first gear engagement's gear and first gear connection, the embodiment of the utility model provides a do not do specifically to this and restrict.
The first driving motor is used for driving the first gear 302-2 to rotate when being started, and the first gear 302-2 is used for driving the rotating shaft 302-1 to rotate when being rotated, so as to drive the bracket to rotate.
As for the structure of the pitching mechanism 303, as shown in fig. 5, the pitching mechanism 303 includes: a hinge shaft 303-1, a second gear 303-2 and a second driving motor, wherein the hinge shaft 303-1 is fixedly connected with the upper part of the turbojet engine 304;
wherein, the both ends of articulated shaft 303-1 are fixed respectively on two vertical curb plates 301-2, and second gear 303-2 cover is established on articulated shaft 303-1, and second driving motor is connected with second gear 303-2, for example: the second driving motor is connected to the second gear 303-2 through a chain and sprocket structure, or connected to the second gear 303-2 through another gear engaged with the second gear 303-2, which is not limited in this embodiment of the present invention.
The second driving motor is used for driving the second gear 303-2 to rotate when the turbojet engine is started, and the second gear 303-2 is used for driving the hinge shaft 303-1 to rotate when the turbojet engine is rotated, so that the pitch angle of the turbojet engine 304 is changed.
Therefore, the pitching angle of the turbojet engine 304 is changed through the second driving motor, multi-angle adjustment of the nozzle 304-1 on the turbojet engine 304 is achieved, and the support and the turbojet engine 304 are driven to integrally rotate through the first driving motor.
Note that the number of the snow removing devices 3 may be set as needed, and may be a single-hair type or a double-hair type.
As shown in fig. 2, the snow removing device 3 is a single-shot type, that is, a turbojet engine 304 is provided, one end of the boom 2 is fixedly connected to the frame 1, the other end extends in a direction away from the frame 1, and the snow removing device 3 is connected to the other end of the boom 2.
As shown in fig. 3, two snow removing devices 3, i.e., two turbojet engines 304, are provided, two ends of the boom 2 extend in a direction away from the frame 1, and the two snow removing devices 3 are respectively connected to two ends of the boom 2.
In addition, the suspension arm 2 can be arranged in a telescopic manner, and the display diagram of the double-arm suspension arm 2 after extending to two sides is shown in fig. 4.
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 it; 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: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the embodiments of the present invention.
Claims (8)
1. A snow removing and deicing equipment for a large front turbojet engine is characterized by comprising:
the device comprises a frame (1), wherein the bottom of the frame (1) is provided with a land wheel (101) which is used for being arranged at the front end of a carrier vehicle (100);
the suspension arm (2), the suspension arm (2) is fixedly connected with the frame (1);
snow removing device (3), snow removing device (3) are located the outside of frame (1), it includes: the support (301) is in rotary connection with the suspension arm (2) through the rotating mechanism (302); the turbojet engine (304) is suspended on the bracket (301) in a pitching mode through a pitching mechanism (303);
the turbojet engine (304) is used for snow removal and freeze removal, the rotating mechanism (302) is used for driving the support (301) to rotate, and the support (301) is used for driving the turbojet engine (304) to rotate when rotating; the pitching mechanism (303) is used for adjusting the pitching angle of the turbojet engine (304).
2. The snow and ice removing apparatus for the large front turbojet engine according to claim 1, wherein the bracket (301) comprises a horizontal cross plate (301-1) and two vertical side plates (301-2) which are oppositely arranged and located below the horizontal cross plate (301-1).
3. The large forward turbojet engine snow and ice removing apparatus of claim 1, wherein the rotating mechanism (302) comprises: a rotating shaft (302-1), a first gear (302-2) and a first driving motor;
the bottom of the rotating shaft (302-1) is fixedly connected with the support (301), the top of the rotating shaft penetrates through the suspension arm (2), the first gear (302-2) is sleeved on the rotating shaft (302-1) and located above the suspension arm (2), and the first driving motor is connected with the first gear (302-2);
the first driving motor is used for driving the first gear (302-2) to rotate when the first driving motor is started, and the first gear (302-2) is used for driving the rotating shaft (302-1) to rotate when the first driving motor rotates, so that the support (301) is driven to rotate.
4. The large front turbojet engine snow and ice removing apparatus of claim 2, wherein the pitching mechanism (303) comprises: a hinged shaft (303-1), a second gear (303-2) and a second driving motor, wherein the hinged shaft (303-1) is fixedly connected with the upper part of the turbojet engine (304);
two ends of the hinged shaft (303-1) are respectively fixed on the two vertical side plates (301-2), the second gear (303-2) is sleeved on the hinged shaft (303-1), and the second driving motor is connected with the second gear (303-2);
the second driving motor is used for driving the second gear (303-2) to rotate when the turbojet engine is started, and the second gear (303-2) is used for driving the hinge shaft (303-1) to rotate when the turbojet engine is rotated, so that the pitching angle of the turbojet engine (304) is changed.
5. The snow removing and deicing apparatus for the large front turbojet engine according to claim 1, wherein one end of the boom (2) is fixedly connected to the frame (1), the other end extends in a direction away from the frame (1), and the snow removing device (3) is connected to the other end of the boom (2).
6. The snow removing and deicing equipment for the large front turbojet engine according to claim 1, wherein both ends of the boom (2) extend in a direction away from the frame (1), and the snow removing devices (3) are correspondingly connected with both ends of the boom (2), respectively.
7. The snow and ice removing apparatus for a large front turbojet engine according to claim 1, wherein the turbojet engine (304) is rotated through an angle in the range of 0 ° to 180 °.
8. The large forward turbojet engine snow and ice removing apparatus of claim 1 wherein the turbojet engine (304) has a pitch angle in the range of 0 ° to 45 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121536645.9U CN215057764U (en) | 2021-07-07 | 2021-07-07 | Snow removing and deicing equipment for large-scale front-mounted turbojet engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121536645.9U CN215057764U (en) | 2021-07-07 | 2021-07-07 | Snow removing and deicing equipment for large-scale front-mounted turbojet engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215057764U true CN215057764U (en) | 2021-12-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121536645.9U Active CN215057764U (en) | 2021-07-07 | 2021-07-07 | Snow removing and deicing equipment for large-scale front-mounted turbojet engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215057764U (en) |
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2021
- 2021-07-07 CN CN202121536645.9U patent/CN215057764U/en active Active
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