Snow plow for aircraft

Abstract

The present invention relates to the field of aircraft technology, and specifically to a snowplow for aircraft, comprising a vehicle body, a first driving member being arranged at the upper end of the vehicle body, a second driving member being installed at the upper end of the movable part of the first driving member, an angle adjustment member being arranged at the front end of the movable part of the second driving member, a first plate being hingedly connected to the front end of the angle adjustment member, a second plate being installed directly in front of the first plate, a first clamping member being arranged at the right end of the first plate, a second clamping member being installed at the right end of the second plate, an adjustment member being arranged between the first plate and the second plate, a main pipe being installed at the lower end of the adjustment member, two vertical portions of the main pipe being connected to the front end of the first plate and the rear end of the auxiliary plate respectively at the outward ends, a plurality of nozzles being connected to the inner wall of the main pipe at equal distances, this design enables comprehensive mechanical snow removal operations on the wing of an aircraft, effectively reduces the probability of residual ice and snow during snow removal due to factors such as icing on the side of the wing of the aircraft, effectively reduces working time, and effectively ensures snow removal effect and quality.

Description

Technical Field

[0001] The invention relates to a snowplow for aircraft, belonging to the technical field of aircraft. Background Art

[0002] Aircraft, these marvels soaring through the blue sky, soar freely through the atmosphere with their delicate wings and powerful propulsion systems. Civil airliners, as a key member of the aircraft family, not only carry the dreams and expectations of countless passengers but are also an indispensable part of the modern transportation network. However, in extreme weather conditions such as winter, when night falls and the winds are biting, the wings of these giant steel birds are often covered with a layer of frost or snow. While this natural phenomenon is beautiful, it poses a potential threat to flight safety. The presence of ice and snow can seriously interfere with the airflow characteristics of the wing surface, thereby affecting the stability and controllability of the entire aircraft.

[0003] To ensure that every takeoff is safe and smooth, effective measures must be taken to remove these obstacles. The currently commonly used method is to use specially designed snow removal vehicles for operations. This type of equipment is usually equipped with a body that stores de-icing fluid, a flexibly movable robotic arm, an operating cabin at the end of the arm, and a spraying device installed in the cabin. The specific operation process is: first, the vehicle is driven to the aircraft to be processed. Then, the staff enters the operating cabin and controls the robotic arm to move the spraying device above the target area. Finally, the nozzle is activated to release de-icing fluid to dissolve and wash away the ice and snow layer attached to the wing surface.

[0004] Although the above solution is relatively mature and widely used, it still has some shortcomings. For example, under the manual intervention mode, due to factors such as limited vision and differences in experience, it is often necessary to adjust the position multiple times to complete full coverage, which undoubtedly increases the overall operation time. In addition, ice may form on the edges of the wings, and these locations are very likely to be ignored and not properly handled, resulting in a high probability of ice and snow remaining on the aircraft wings after subsequent snow removal, which will affect the effect and quality of snow removal. Summary of the Invention

[0005] In view of the problems in the prior art, the present invention provides a snowplow for aircraft.

[0006] The technical solution adopted by the present invention to solve the technical problem is as follows: a snowplow for aircraft, comprising a vehicle body, a first driving member being provided at the upper end of the vehicle body, a second driving member being mounted at the upper end of a movable portion of the first driving member, an angle adjustment member being provided at the front end of the movable portion of the second driving member, the front end of the angle adjustment member being hinged to a first plate, a second plate being mounted directly in front of the first plate, an auxiliary plate being hinged to the lower end of the second plate, a first clamping member being provided at the right end of the first plate, a second clamping member being mounted at the right end of the second plate, and the second clamping member being located directly in front of the first clamping member;

[0007] An adjusting member is provided between the first plate and the second plate, and a main pipe is installed at the lower end of the adjusting member, and the cross-section of the main pipe is U-shaped. The two vertical parts of the main pipe are connected to the front end of the first plate and the rear end of the auxiliary plate respectively toward the outward ends. The inner wall of the main pipe is connected to multiple nozzles at equal distances. A connecting pipe is provided at the lower end of the rear of the main pipe, and the other end of the connecting pipe is connected to the box part of the vehicle body.

[0008] Furthermore, the adjusting member includes a mounting plate, the lower end of the mounting plate is rotatably connected to the gear, and the mounting plate is located between the first plate and the second plate, a turntable is provided at the lower end of the gear, a first drive device is installed in the middle of the upper end of the mounting plate, and the output shaft of the first drive device is connected to the gear, two first guide wheels are symmetrically provided at the lower end of the rear of the turntable, and the two first guide wheels are located on the left and right ends of the main pipe, two second guide wheels are symmetrically provided at the lower end of the front of the turntable, and the second guide wheels are located directly in front of the first guide wheels, and the two second guide wheels are located on the left and right ends of the main pipe;

[0009] A second rack is provided at the front end of the first plate, and the second rack is located between the lower end of the mounting plate and the upper end of the turntable, the second rack is meshed with the left end of the gear, the first rack is installed at the rear end of the second plate, and the first rack is located between the lower end of the mounting plate and the upper end of the turntable, the first rack is meshed with the right end of the gear, a plurality of second rods are equidistantly provided at the rear end of the mounting plate, the rear ends of the plurality of second rods all pass through the first plate, and the second rods are slidably connected to the first plate, a plurality of first rods are equidistantly provided at the front end of the mounting plate, the front ends of the plurality of first rods all pass through the second plate, and the first rods are slidably connected to the second plate.

[0010] Furthermore, the first clamping member includes a first mounting frame, which is arranged on the right end of the first plate, and the cross-section of the first mounting frame is L-shaped. The first clamping frame is installed at the front end of the vertical part of the first mounting frame, and the cross-section of the first clamping frame is Y-shaped. A plurality of first rolling members are equidistantly arranged at the front end of the first clamping frame.

[0011] Furthermore, the second clamping member includes a second mounting frame, which is arranged at the right end of the second plate, and the cross-section of the second mounting frame is L-shaped. The second clamping frame is installed at the rear end of the vertical part of the second mounting frame, and the second clamping frame is located directly in front of the first clamping frame. The cross-section of the second clamping frame is Y-shaped, and the second clamping frame is arranged opposite to the first clamping frame. A plurality of second rolling members are equidistantly installed at the rear end of the second clamping frame.

[0012] Furthermore, the angle adjustment member includes a frame, which is attached to the rear end of the first plate, and the cross-section of the frame is L-shaped. The lower end of the frame is hinged to the lower end of the first plate, and a lifting device is movably installed on the upper end of the transverse part of the frame, and the front end of the movable part of the lifting device is movably connected to the rear end of the first plate.

[0013] Furthermore, the second driving member includes a movable block, the lower end of the movable block is connected to the upper end of the movable part of the first driving member, a telescopic device is provided at the upper end of the movable block, a movable plate is installed at the rear end of the movable part of the telescopic device, and the movable plate is located at the rear side of the movable block, and a plurality of round rods are equidistantly provided at the front end of the movable plate, the other ends of the plurality of round rods are connected to the rear end of the vertical part of the frame, the plurality of round rods all pass through the movable block, and the round rods are slidably connected to the movable block.

[0014] Furthermore, the first driving member includes a third frame, the third frame is slidably connected to the upper end of the vehicle body, the third frame is internally rotatably connected to a bidirectional screw, the left outer end of the bidirectional screw is connected to the first movable plate via a ball nut pair, and the first movable plate is slidably connected within the third frame, the right outer end of the bidirectional screw is connected to the second movable plate via a ball nut pair, and the second movable plate is slidably connected within the third frame, a second driving device is provided at the left end of the third frame, and an output shaft of the second driving device is connected to the bidirectional screw;

[0015] The first frame is arranged directly above the third frame, and a plurality of first arms are movably installed on the upper end of the first movable plate, and the first arms are tilted with the left higher and the right lower. The other ends of the plurality of first arms are movably connected to the lower end of the first frame, and a plurality of second arms are movably provided on the upper end of the second movable plate, and the second arms are tilted with the left lower and the right higher. The other ends of the plurality of second arms are movably connected to the lower end of the first frame, and the first screw rod is rotatably connected in the first frame, the outer end of the first screw rod is connected to the nut seat through a ball nut pair, and the nut seat is slidably connected in the first frame, the upper end of the nut seat extends out of the upper side of the first frame and is connected to the lower end of the movable block, a third driving device is installed on the left end of the first frame, and the output shaft of the third driving device is connected to the first screw rod.

[0016] Furthermore, a second frame is installed on the upper end of the vehicle body, the third frame is slidably connected to the second frame, and the third frame extends out of the right side of the second frame. Moving seats are provided at both the front and rear ends of the left part of the third frame, and the moving seats are slidably connected to the second frame. Two second screw rods are symmetrically rotated in the second frame, and the two second screw rods respectively pass through the two moving seats, and the second screw rods and the moving seats are connected by a ball nut pair;

[0017] A fourth drive device is provided at the right end of the second frame, and the fourth drive device is located outside the third frame. The output shaft of the fourth drive device is connected to a second screw rod. The left end of the second frame is symmetrically rotated to connect two sprockets, and the two sprockets are connected to each other through a chain. The left ends of the two second screw rods pass through the second frame and are respectively connected to the two sprockets.

[0018] Furthermore, a first ladder frame is provided at the lower right end of the first frame, and the first ladder frame is located on the right side of the vehicle body and the right side of the third frame. The right end of the first ladder frame is slidably connected to the second ladder frame, and the second ladder frame extends out of the lower side of the first ladder frame. Two movable components are symmetrically installed at the lower end of the second ladder frame.

[0019] Beneficial effects of the present invention:

[0020] 1. Through the vehicle body, the fourth motor, the bidirectional screw rod, multiple first arms, multiple second arms, the first electric push rod, multiple round rods, the second motor, the first screw rod, the main pipe, multiple nozzles, the first plate, the second plate and the mounting plate, the nozzles installed at the vertical portion of the main pipe will spray heated deicing liquid toward the sides of the aircraft's wings, thereby achieving comprehensive mechanical snow removal operations on the aircraft's wings, effectively reducing the probability of residual ice and snow during snow removal due to factors such as ice formation on the sides of the aircraft's wings, effectively reducing working time, and effectively ensuring the snow removal effect and quality.

[0021] 2. The wing of the aircraft is clamped by the first motor, gear, turntable, two first guide wheels, two second guide wheels, first rack and second rack, and heated de-icing fluid is sprayed onto the surface of the wing of the aircraft through multiple nozzles. At the same time, the second motor, first screw rod, third motor and two second screw rods and other components are used to make the main pipe continue to move rightward along the wing of the aircraft, so as to effectively spray the heated de-icing fluid onto the surface of the wing of the aircraft, effectively reduce the probability of non-contact between the sprayed heated de-icing fluid and the surface of the wing of the aircraft, effectively reduce the probability of residual ice and snow on the surface of the wing of the aircraft, and automatically adjust the distance between the movable block and the main pipe and other components, effectively reduce the probability of interference between the nozzle on the upper side of the main pipe and the wing of the aircraft, effectively ensure that the heated de-icing fluid can be sprayed onto the surface of the wing of the aircraft normally, and effectively ensure the snow removal effect and quality.

[0022] 3. Use the second electric push rod and the frame to make the mounting plate and other components parallel to the wing of the aircraft, so as to adjust the angle of the mounting plate and other components, effectively reducing the probability of interference when the main pipe moves outward along the wing due to the tilt of the aircraft's wing, and effectively ensuring the snow removal effect and quality.

[0023] 4. Through the third bull's eye ball, the functional plate and the third arm, the nozzle direction of the corresponding nozzle is changed, and the nozzle with the changed nozzle direction sprays heated deicing fluid toward the extension of the aircraft engine part, thereby realizing snow removal operation on the extension of the aircraft engine part and ensuring that the main pipe can move normally along the aircraft wing part, effectively reducing the probability of collision between the main pipe, the second plate and other components and the aircraft wing part, effectively reducing the probability of ice and snow remaining on the aircraft wing part, and effectively ensuring the snow removal effect and quality. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Other features, objects and advantages of the present invention will become more apparent upon reading the detailed description of non-limiting embodiments with reference to the following drawings:

[0025] Figure 1 This is a schematic structural diagram of an aircraft snowplow according to the present invention;

[0026] Figure 2 A perspective view of an aircraft snowplow according to the present invention;

[0027] Figure 3 This is a perspective view of a first frame of an aircraft snowplow according to the present invention;

[0028] Figure 4 This is a perspective view of a second frame of an aircraft snowplow according to the present invention;

[0029] Figure 5 This is a perspective view of a third frame of an aircraft snowplow according to the present invention;

[0030] Figure 6 This is an assembly diagram of a first plate, a turntable, a mounting plate, a second plate, and a main pipe in an aircraft snowplow of the present invention;

[0031] Figure 7 This is a cross-sectional view of a mounting plate in an aircraft snowplow according to the present invention;

[0032] Figure 8 This is an assembly diagram of a turntable and a first motor in an aircraft snowplow according to the present invention;

[0033] Figure 9 This is a schematic diagram of another embodiment of an aircraft snowplow according to the present invention;

[0034] Figure 10 This is an assembly diagram of a turntable, a first motor, a mounting plate, and gears in an aircraft snowplow according to the present invention;

[0035] Figure 11 for Figure 10 Enlarged view of part A in the middle.

[0036] In the figure: 1, vehicle body, 2, first frame, 3, movable block, 4, first plate, 5, turntable, 6, first motor, 7, mounting plate, 8, second plate, 9, main pipe, 21, first ladder frame, 22, universal wheel, 23, second ladder frame, 24, second frame, 25, third frame, 26, nut seat, 27, first screw rod, 28, second motor, 31, round rod, 32, movable plate, 33, first electric push rod, 41, first mounting frame, 42, first clamping frame, 43, first bull's eye ball, 44, frame, 45, second electric push rod, 51, first guide wheel, 52, second guide Wheel, 61, gear, 71, first rod, 72, first rack, 73, second rod, 74, second rack, 81, second mounting bracket, 82, auxiliary plate, 83, second clamping bracket, 84, second bull's eye ball, 85, function board, 91, nozzle, 92, connecting pipe, 241, third motor, 242, second screw rod, 243, movable seat, 244, sprocket, 251, fourth motor, 252, bidirectional screw rod, 253, first movable plate, 254, first support arm, 255, second movable plate, 256, second support arm, 851, third bull's eye ball, 852, third support arm. DETAILED DESCRIPTION

[0037] In order to make the technical means, creative features, objectives and effects achieved by the present invention easier to understand, the present invention is further described below in conjunction with specific implementation methods.

[0038] Example 1: Figures 1-8 As shown, a snowplow for aircraft is provided, comprising a vehicle body 1, a first frame 2 being provided directly above the vehicle body 1, a third frame 25 being slidably connected to a second frame 24 and extending to the right side of the second frame 24, and being slidably connected to the upper end of the vehicle body 1, the third frame 25 being used to provide a mounting carrier for components such as a bidirectional screw rod 252, and the bidirectional screw rod 252 being rotatably connected to the interior of the third frame 25, and the first movable plate 253 and the second movable plate 255 being moved relative to each other by the bidirectional screw rod 252, and then the first movable plate 253 being slidably connected to the third frame 25 is moved by a ball nut pair. Connected to the left outer end of the bidirectional screw rod 252, a mounting carrier is provided for the first arm 254 through the first movable plate 253, and a second movable plate 255 slidably connected to the third frame 25 is connected to the right outer end of the bidirectional screw rod 252 through a ball nut pair, and a mounting carrier is provided for the second arm 256 through the second movable plate 255. The fixed part of the second driving device connecting the output shaft to the bidirectional screw rod 252 is set on the left end of the third frame 25, and the bidirectional screw rod 252 is driven to rotate by the second driving device. The second driving device can use the fourth motor 251;

[0039] A plurality of first arms 254 are arranged with a left higher and a right lower tilt and the other end of which is movably connected to the lower end of the first frame 2 and is movably installed on the upper end of the first movable plate 253, and a plurality of second arms 256 are arranged with a left lower and a right higher tilt and the other end of which is movably connected to the lower end of the first frame 2 and is movably arranged on the upper end of the second movable plate 255. The plurality of first arms 254 and the plurality of second arms 256 are used in conjunction with each other to make the first frame 2 move up and down, and then the first screw rod 27 is rotatably connected to the first frame 2, and the nut seat 26 is moved along the first frame 2 through the first screw rod 27, and the nut seat 26 which is slidably connected to the first frame 2 and the upper end of which extends out of the upper side of the first frame 2 and is connected to the lower end of the movable block 3 is connected to the outer end of the first screw rod 27 through a ball nut pair, and a mounting carrier is provided for the movable block 3 through the nut seat 26, and then the fixed part of the third driving device connected with the output shaft and the first screw rod 27 is installed on the left end of the first frame 2, and the first screw rod 27 is driven to rotate by the third driving device, and the third driving device can adopt a second motor 28;

[0040] The second frame 24 is mounted on the upper end of the vehicle body 1, and a mounting carrier is provided for components such as the second screw rod 242 through the second frame 24, and two movable seats 243 respectively arranged at the front and rear ends of the left part of the third frame 25 are slidably connected to the front and rear walls inside the second frame 24. The two movable seats 243 cooperate with each other to make the third frame 25 move left and right. Then, two second screw rods 242 connected to the movable seats 243 through ball nut pairs are respectively passed through the two movable seats 243 and the left ends pass through the second frame 24 and are respectively connected to the two sprockets 244, and are symmetrically rotated and connected in the second frame 24. The movable seat 243 moves left and right through the second screw rod 242, and the fixing part of the fourth driving device located outside the third frame 25 and having the output shaft connected to one of the second screw rods 242 is set on the right end of the second frame 24. The corresponding second screw rod 242 is started to rotate through the fourth driving device. The fourth driving device can adopt the third motor 241;

[0041] The two sprockets 244 connected to each other by a chain are symmetrically rotated and connected to the left end of the second frame 24. The two sprockets 244 are used in conjunction with each other to make the two second screw rods 242 rotate synchronously, and the first ladder frame 21 located on the right side of the vehicle body 1 and the right side of the third frame 25 is set on the lower end of the right part of the first frame 2, and then the second ladder frame 23 extending from the lower side of the first ladder frame 21 is slidably connected to the right end of the first ladder frame 21. The first ladder frame 21 and the second ladder frame 23 are used in conjunction with each other to lift the first frame 2 on the one hand and can be used for climbing on the other hand. The two moving components are symmetrically installed on the lower end of the second ladder frame 23. The two moving components are used in conjunction with each other to assist the left and right movement of the second ladder frame 23. The moving component can be a universal wheel 22. The fixed part of the telescopic device on which the moving plate 32 is installed at the rear end of the movable part is connected to the upper end of the movable block 3 connected at the lower end and the upper end of the movable block 3. The moving plate 32 is driven to move forward and backward through the telescopic device. The telescopic device can be a first electric push rod 33. A plurality of round rods 31 connected at the other end to the rear end of the vertical part of the frame 44, passing through the movable block 3 and slidingly connected to the movable block 3 are connected to the front end of the movable plate 32 located at the rear side of the movable block 3. The plurality of round rods 31 are moved forward and backward through the movable plate 32.

[0042] The lower end of the frame 44 having an L-shaped cross section and a vertical portion affixed to the rear end of the first plate 4 is hinged to the lower end of the first plate 4, and a mounting carrier is provided for the lifting device through the frame 44. The lifting device, whose movable front end is movably connected to the rear end of the first plate 4, is movably mounted on the upper end of the horizontal portion of the frame 44. The first plate 4 is driven to swing through the lifting device. The lifting device can use a second electric push rod 45. The lower end of the second plate 8 located directly in front of the first plate 4 is hinged to the auxiliary plate 82, and a mounting carrier is provided for the main pipe 9 through the auxiliary plate 82.

[0043] The horizontal portion of the first mounting frame 41 with an L-shaped cross section is set on the right end of the first plate 4, and the first mounting frame 41 is used to provide a mounting carrier for the first clamping frame 42. The horizontal portion of the second mounting frame 81 with an L-shaped cross section is set on the right end of the second plate 8, and the second mounting frame 81 is used to provide a mounting carrier for the second clamping frame 83. Then, the vertical portion of the first clamping frame 42 with a Y-shaped cross section is installed on the front end of the vertical portion of the first mounting frame 41, and the second clamping frame 83 located in front of the first clamping frame 42 and having a Y-shaped cross section and arranged opposite to the first clamping frame 42 is installed. The vertical portion is mounted on the rear end of the vertical portion of the second mounting frame 81. The first clamping frame 42 is used in conjunction with the second clamping frame 83 to clamp the wing portion of the aircraft. A plurality of first rolling members are equidistantly arranged on the front end of the first clamping frame 42. The first rolling members are used to assist the movement of the first clamping frame 42. The first rolling members can be first bull's eye balls 43. A plurality of second rolling members are equidistantly mounted on the rear end of the second clamping frame 83. The second rolling members are used to assist the movement of the second clamping frame 83. The second rolling members can be second bull's eye balls 84.

[0044] The gear 61 is rotatably connected to the lower end of the mounting plate 7 located between the first plate 4 and the second plate 8, and the first rack 72 and the second rack 74 are moved relative to each other through the gear 61, and the fixed part of the first driving device connected to the output shaft and the gear 61 is installed on the middle part of the upper end of the mounting plate 7, and the gear 61 is driven to rotate by the first driving device. The first driving device can adopt the first motor 6, and then the turntable 5 is set on the lower end of the gear 61, and the turntable 5 provides a mounting carrier for components such as the first guide wheel 51, and the two first guide wheels 51 located at the left and right ends of the main pipe 9 are symmetrically arranged on the rear lower end of the turntable 5, and the two first guide wheels 51 are used in conjunction to clamp the main pipe 9, and then the two second guide wheels 52 located at the left and right ends of the main pipe 9 and directly in front of the first guide wheel 51 are symmetrically mounted on the front lower end of the turntable 5, and the two second guide wheels 52 are used in conjunction to clamp the main pipe 9;

[0045] The second rack 74 located between the lower end of the mounting plate 7 and the upper end of the turntable 5 and meshed with the left end of the gear 61 is arranged on the front end of the first plate 4, and the first plate 4 is moved forward and backward through the second rack 74, and the first rack 72 located between the lower end of the mounting plate 7 and the upper end of the turntable 5 and meshed with the right end of the gear 61 is mounted on the rear end of the second plate 8, and the second plate 8 is moved forward and backward through the first rack 72, and then a plurality of second rods 73 with rear ends passing through the first plate 4 and slidably connected to the first plate 4 are equidistantly arranged on the rear end of the mounting plate 7, and the plurality of second rods 73 are used in conjunction with each other to movably connect the mounting plate 7 and the first plate 4, and a plurality of first rods 71 ​​with front ends passing through the second plate 8 and slidably connected to the second plate 8 are equidistantly mounted on the front end of the mounting plate 7, and the plurality of first rods 71 ​​are used in conjunction with each other to movably connect the mounting plate 7 and the second plate 8;

[0046] The transverse portion of a main pipe 9 having a U-shaped cross section and two vertical portions connected outwardly to the front end of the first plate 4 and the rear end of the auxiliary plate 82 respectively is installed on the lower side of the turntable 5. The main pipe 9 provides a mounting carrier for components such as the nozzles 91, and multiple nozzles 91 are connected to the inner wall of the main pipe 9 at equal distances. The multiple nozzles 91 are used in combination to spray deicing liquid onto the wing surface of the aircraft. Then, a connecting pipe 92, the other end of which is connected to the box portion of the vehicle body 1, is connected and arranged on the lower rear end of the main pipe 9. The main pipe 9 is connected to the box portion of the vehicle body 1 through the connecting pipe 92.

[0047] When in use, the vehicle body 1 is first started, thereby moving the main pipe 9 and other components to a position near the wing of the aircraft to be cleared of snow, and then the fourth motor 251 is started, thereby driving the bidirectional screw rod 252 to rotate, thereby causing the first movable plate 253 and the second movable plate 255 to move outward, thereby causing the lower parts of the multiple first support arms 254 and the lower parts of the multiple second support arms 256 to move outward, thereby causing the upper parts of the multiple first support arms 254 and the upper parts of the multiple second support arms 256 to move upward, thereby causing the first frame 2 to move upward, thereby causing the mounting plate 7, the movable block 3 and other components to move upward to the appropriate position, and then the first electric push rod 33 is started, thereby driving the movable plate 32 to move forward, thereby causing the multiple round rods 31 to move forward, thereby causing the frame 44, the first plate 4, the second plate 8 and the mounting plate 7 and other components to move forward, thereby causing the main pipe 9 to move forward to be just above the wing of the aircraft;

[0048] Then the second motor 28 is started to drive the first screw rod 27 to rotate, thereby causing the nut seat 26 to move to the left, thereby causing the movable block 3, the frame 44, the first plate 4, the second plate 8 and the mounting plate 7 to move to the left, so that the main pipe 9 is moved to the top of the connection position between the aircraft wing and the aircraft fuselage, and then the fourth motor 251, the two-way screw rod 252, the first movable plate 253, the second movable plate 255, the multiple first arms 254 and the multiple second arms 256 are used to move the main pipe 9, the first clamping The frame 42 and the second clamping frame 83 are moved down to a suitable position, and then the second electric push rod 45 is started, thereby driving the structure formed by the first plate 4, the second plate 8, the mounting plate 7 and other components to swing around the hinge portion of the first plate 4 and the frame 44, so that the mounting plate 7 and other components are parallel to the wing of the aircraft, and the angle of the mounting plate 7 and other components is adjusted, effectively reducing the probability of interference with the main pipe 9 when it moves outward along the wing due to the tilted state of the aircraft wing, and effectively ensuring the snow removal effect and quality;

[0049] Then, the first motor 6 is started, thereby driving the gear 61 and the turntable 5 to rotate, thereby rotating the two first guide wheels 51 and the two second guide wheels 52, thereby converting the middle part of the main pipe 9 into an S shape. At the same time, because the gear 61 is meshed with the first rack 72 and the second rack 74, the rotation of the gear 61 causes the first rack 72 and the second rack 74 to move inward, thereby causing the first plate 4 and the second plate 8 to move inward, thereby causing the first mounting frame 41 and the second mounting frame 81 to move inward, thereby causing the first clamping frame 42 and the second clamping frame 83 to move inward, thereby causing the multiple first bull's eye balls 43 and the multiple second bull's eye balls 84 to contact the side ends of the aircraft's wing portion, thereby clamping the aircraft's wing portion;

[0050] Then, the deicing liquid stored in the box of the vehicle body 1 is heated, and then the heated deicing liquid is transported to the main pipe 9 through the connecting pipe 92. Then, the heated deicing liquid in the main pipe 9 is sprayed onto the surface of the wing of the aircraft through multiple nozzles 91. At the same time, the second motor 28, the first screw rod 27 and the nut seat 26 and other components are used to move the mounting plate 7, the first plate 4 and other components to the right along the wing of the aircraft. When the nut seat 26 moves to the right limit position, if the main pipe 9 still does not move to the tail end of the wing of the aircraft, the third motor 24 is started again. 1, thereby driving the corresponding second screw rod 242 to rotate, and causing the corresponding sprocket 244 to rotate, and with the assistance of the chain, the two sprockets 244 rotate synchronously, thereby causing the two second screw rods 242 to rotate synchronously. Because the second screw rods 242 are connected to the movable seat 243 through a ball nut pair, the synchronous rotation of the two second screw rods 242 simultaneously causes the two movable seats 243 to move to the right synchronously, thereby causing the third frame 25, the first frame 2 and other components to move to the right, and then causing the manifold 9 to continue to move to the right along the wing of the aircraft;

[0051] At the same time, the main pipe 9 is U-shaped, so that the multiple nozzles 91 are in a U-shaped structure, and then the nozzles 91 installed at the vertical portion of the main pipe 9 will spray heated de-icing liquid toward the side of the aircraft wing, realizing a comprehensive mechanical snow removal operation on the aircraft wing, effectively reducing the probability of residual ice and snow during snow removal due to factors such as ice formation on the side of the aircraft wing, effectively reducing working time, and effectively ensuring the snow removal effect and quality;

[0052] If the wing of the aircraft is in a state of being wide inside and narrow outside, when the main pipe 9 moves outward along the wing of the aircraft, the turntable 5, the first motor 6, the gear 61, the first rack 72, the second rack 74, the two first guide wheels 51 and the two second guide wheels 52 and other components are simultaneously used to gradually reduce the distance between the first plate 4 and the second plate 8, and gradually shorten the length of the transverse portion of the main pipe 9, so that the distance between the nozzle 91 and the aircraft wing is guaranteed to be within a normal range, and the heated de-icing liquid is effectively sprayed on the surface of the aircraft wing, effectively reducing the probability of non-contact between the sprayed heated de-icing liquid and the surface of the aircraft wing, effectively reducing the probability of residual ice and snow on the surface of the aircraft wing, and effectively ensuring the snow removal effect and quality;

[0053] In addition, as the main pipe 9 moves outward along the wing of the aircraft, with the assistance of multiple first bull's eye balls 43 and multiple second bull's eye balls 84, the first clamping frame 42 and the second clamping frame 83 both move along the side of the aircraft wing, so that the aircraft wing is always in a clamping state. If the wing of the aircraft is designed to be at an angle to the fuselage of the aircraft, the clamping of the aircraft wing by the first clamping frame 42 and the second clamping frame 83 will cause the multiple round rods 31 to move evenly outward along the movable block 3 during movement, thereby automatically adjusting the distance between the movable block 3 and components such as the main pipe 9, effectively reducing the probability of interference between the nozzle 91 on the upper side of the main pipe 9 and the aircraft wing, effectively ensuring that the heated deicing fluid can be sprayed normally onto the surface of the aircraft wing, and effectively ensuring the snow removal effect and quality.

[0054] Example 2: Through the mechanical cooperation of the vehicle body 1, the fourth motor 251, the bidirectional screw rod 252, the first electric push rod 33, the second motor 28, the first screw rod 27, the fourth motor 251, the bidirectional screw rod 252, the first motor 6, the gear 61, the turntable 5, the two first guide wheels 51, the two second guide wheels 52, the first rack 72, the second rack 74, the first clamping frame 42 and the second clamping frame 83, the wing of the aircraft is effectively clamped. On this basis, the pre-sprayed material is evenly sprayed onto the surface of the wing of the aircraft through the connecting pipe 92, the main pipe 9 and the nozzle 91. The de-icing fluid is heated first, thereby achieving comprehensive and meticulous mechanical snow removal operations. However, during this process, the tail of the engine of some aircraft will extend beyond the edge of the wing. This structural layout can easily lead to accidental collisions between the moving main pipe 9 and its accessories and the extended part of the engine, thereby interfering with the smooth progress of the entire snow removal process. In addition, the upper surface of these protruding parts often becomes an ideal place for snowflakes to accumulate. Due to the existence of visual blind spots, the ice and snow in this area are difficult to be effectively removed, increasing the risk of residual ice and snow, which undoubtedly poses a hidden danger to subsequent flight safety.

[0055] In order to solve the above problems, Figures 9-11As shown, the third arm 852, which is arranged to be higher in the front and lower in the back and is located on the lower side of the main pipe 9, is installed on the rear end of the lower part of the auxiliary plate 82, and the upper end of the function plate 85 with an arc-shaped cross section is movably connected to the other end of the third arm 852. The function plate 85 and the auxiliary plate 82 are movably connected through the third arm 852, and then a plurality of third bull's eye balls 851 with an arc-shaped structure are equidistantly installed on the lower end of the function plate 85. The plurality of third bull's eye balls 851 are used in combination to enable the function plate 85 to move along the upper surface of the aircraft engine part.

[0056] During use, the vehicle body 1, the fourth motor 251, the bidirectional screw rod 252, the first movable plate 253, the second movable plate 255, the plurality of first arms 254, the plurality of second arms 256, the first electric push rod 33, the movable plate 32, the plurality of round rods 31, the second motor 28, the first screw rod 27 and the nut seat 26 are first used to move the manifold 9 to the position just above the connection position between the wing portion of the aircraft and the fuselage of the aircraft. Then, the fourth motor 251, the bidirectional screw rod 252, the first movable plate 253, the second movable plate 255, the plurality of first arms 254 and the plurality of second arms 256 and other components are used to move the manifold 9, the first clamping frame 42 and the second clamping frame 83 downward to a suitable position. Then, the second electric push rod 45 and the frame 44 are used to make the mounting plate 7 and other components parallel to the wing portion of the aircraft.

[0057] The first motor 6, gear 61, turntable 5, two first guide wheels 51, two second guide wheels 52, first rack 72, second rack 74, first plate 4, second plate 8, first clamping frame 42, and second clamping frame 83 are then used to clamp the wing of the aircraft. Then, heated deicing fluid is sprayed onto the surface of the wing of the aircraft through connecting pipe 92, main pipe 9, and nozzle 91. Simultaneously, the second motor 28, first screw rod 27, nut seat 26, third motor 241, two second screw rods 242, and two moving seats 243 are used to move the mounting plate 7, first plate 4, and other components to the right along the wing of the aircraft, thereby performing a comprehensive mechanical snow removal operation on the wing of the aircraft.

[0058] If the tail side of the aircraft's engine section extends outward from the aircraft's wing section, when the main pipe 9 moves outward along the aircraft's wing section, the third bull's eye ball 851 first contacts the aircraft's engine section extension, thereby lifting the third bull's eye ball 851 upward, causing the functional panel 85 to move upward, and with the assistance of the third arm 852, the auxiliary panel 82 swings around the hinged portion between the auxiliary panel 82 and the second panel 8, thereby causing the main pipe 9 and the auxiliary panel 82 connection portion to move outward, thereby causing the nozzle direction of the corresponding nozzle 91 to change and face the aircraft's engine section extension. At this time, the corresponding nozzle 91 sprays heated de-icing fluid onto the aircraft's engine section extension, thereby performing snow removal operations on the aircraft's engine section extension and ensuring that the main pipe 9 can move normally along the aircraft's wing section, effectively reducing the probability of collisions between the main pipe 9, the second panel 8 and other components and the aircraft's wing section, effectively reducing the probability of ice and snow remaining on the aircraft's wing section, and effectively ensuring the snow removal effect and quality.

[0059] Although this specification is described according to implementation methods, not every implementation method contains only one independent technical solution. This narrative method of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment can also be appropriately combined to form other implementation methods that can be understood by those skilled in the art.

Claims

1. An aircraft snowplow, characterized in that: The vehicle comprises a vehicle body (1), wherein a first driving member is provided at the upper end of the vehicle body (1), a second driving member is installed at the upper end of the movable portion of the first driving member, an angle adjustment member is provided at the front end of the movable portion of the second driving member, the front end of the angle adjustment member is hinged to a first plate (4), a second plate (8) is installed in front of the first plate (4), the lower end of the second plate (8) is hinged to an auxiliary plate (82), a first clamping member is provided at the right end of the first plate (4), a second clamping member is installed at the right end of the second plate (8), and the second clamping member is located in front of the first clamping member; An adjusting member is provided between the first plate (4) and the second plate (8), a main pipe (9) is installed at the lower end of the adjusting member, and the cross section of the main pipe (9) is U-shaped. The two vertical portions of the main pipe (9) are connected to the front end of the first plate (4) and the rear end of the auxiliary plate (82) toward the outer ends, respectively. The inner wall of the main pipe (9) is connected to a plurality of nozzles (91) at equal intervals. A connecting pipe (92) is provided at the lower end toward the rear of the main pipe (9), and the other end of the connecting pipe (92) is connected to the box portion of the vehicle body (1).

2. The aircraft snow removal vehicle according to claim 1, characterized in that: The regulating member comprises a mounting plate (7), the lower end of the mounting plate (7) is rotatably connected to a gear (61), and the mounting plate (7) is located between the first plate (4) and the second plate (8), a turntable (5) is provided at the lower end of the gear (61), a first driving device is installed at the middle of the upper end of the mounting plate (7), and the output shaft of the first driving device is connected to the gear (61), two first guide wheels (51) are symmetrically provided at the lower end of the rear portion of the turntable (5), and the two first guide wheels (51) are located on the left and right ends of the main pipe (9), two second guide wheels (52) are symmetrically provided at the lower end of the front portion of the turntable (5), and the second guide wheels (52) are located directly in front of the first guide wheels (51), and the two second guide wheels (52) are located on the left and right ends of the main pipe (9); A second rack (74) is provided at the front end of the first plate (4), and the second rack (74) is located between the lower end of the mounting plate (7) and the upper end of the turntable (5), and the second rack (74) is engaged with the left end of the gear (61). A first rack (72) is provided at the rear end of the second plate (8), and the first rack (72) is located between the lower end of the mounting plate (7) and the upper end of the turntable (5), and the first rack (72) is engaged with the right end of the gear (61). A plurality of second rods (73) are equidistantly provided at the rear end of the mounting plate (7), and the rear ends of the plurality of second rods (73) all pass through the first plate (4), and the second rods (73) are slidably connected to the first plate (4). A plurality of first rods (71) are equidistantly provided at the front end of the mounting plate (7), and the front ends of the plurality of first rods (71) all pass through the second plate (8), and the first rods (71) are slidably connected to the second plate (8).

3. The aircraft snow removal vehicle according to claim 1, characterized in that: The first clamping member comprises a first mounting frame (41), the first mounting frame (41) being arranged on the right end of the first plate (4), and the cross section of the first mounting frame (41) being L-shaped, a first clamping frame (42) being installed at the front end of the vertical portion of the first mounting frame (41), and the cross section of the first clamping frame (42) being Y-shaped, and a plurality of first rolling members being equidistantly arranged at the front end of the first clamping frame (42).

4. The aircraft snow removal vehicle according to claim 3, characterized in that: The second clamping member includes a second mounting frame (81), the second mounting frame (81) is arranged at the right end of the second plate (8), and the cross section of the second mounting frame (81) is L-shaped. The second clamping frame (83) is installed at the rear end of the vertical portion of the second mounting frame (81), and the second clamping frame (83) is located directly in front of the first clamping frame (42). The cross section of the second clamping frame (83) is Y-shaped, and the second clamping frame (83) is arranged opposite to the first clamping frame (42). A plurality of second rolling members are equidistantly installed at the rear end of the second clamping frame (83).

5. The aircraft snow removal vehicle according to claim 1, wherein: The angle adjustment member comprises a frame (44), the frame (44) is fitted on the rear end of the first plate (4), and the cross section of the frame (44) is L-shaped. The lower end of the frame (44) is hinged to the lower end of the first plate (4), and a lifting device is movably mounted on the upper end of the transverse portion of the frame (44), and the front end of the movable portion of the lifting device is movably connected to the rear end of the first plate (4).

6. The aircraft snow removal vehicle according to claim 5, characterized in that: The second driving member comprises a movable block (3), the lower end of the movable block (3) is connected to the upper end of the movable part of the first driving member, a telescopic device is provided at the upper end of the movable block (3), a movable plate (32) is installed at the rear end of the movable part of the telescopic device, and the movable plate (32) is located at the rear side of the movable block (3), a plurality of round rods (31) are equidistantly provided at the front end of the movable plate (32), the other ends of the plurality of round rods (31) are all connected to the rear end of the vertical part of the frame (44), the plurality of round rods (31) all penetrate the movable block (3), and the round rods (31) are slidably connected to the movable block (3).

7. The aircraft snow removal vehicle according to claim 6, characterized in that: The first driving member includes a third frame (25), the third frame (25) is slidably connected to the upper end of the vehicle body (1), the third frame (25) is internally rotatably connected to a bidirectional screw rod (252), the left outer end of the bidirectional screw rod (252) is connected to a first movable plate (253) through a ball nut pair, and the first movable plate (253) is slidably connected in the third frame (25), the right outer end of the bidirectional screw rod (252) is connected to a second movable plate (255) through a ball nut pair, and the second movable plate (255) is slidably connected in the third frame (25), a second driving device is provided at the left end of the third frame (25), and an output shaft of the second driving device is connected to the bidirectional screw rod (252); A first frame (2) is arranged directly above the third frame (25); a plurality of first arms (254) are movably mounted on the upper end of the first movable plate (253); and the first arms (254) are arranged in an inclined manner with the left side higher and the right side lower; the other ends of the plurality of first arms (254) are movably connected to the lower end of the first frame (2); a plurality of second arms (256) are movably mounted on the upper end of the second movable plate (255); and the second arms (256) are arranged in an inclined manner with the left side lower and the right side higher; the other ends of the plurality of second arms (256) are movably connected to the lower end of the first frame (2); a first screw rod (27) is rotatably connected in the first frame (2); the outer end of the first screw rod (27) is connected to the nut seat (26) through a ball nut pair, and the nut seat (26) is slidably connected in the first frame (2); the upper end of the nut seat (26) extends out of the upper side of the first frame (2) and is connected to the lower end of the movable block (3); a third driving device is mounted on the left end of the first frame (2), and the output shaft of the third driving device is connected to the first screw rod (27).

8. The aircraft snow removal vehicle according to claim 7, characterized in that: The second frame (24) is installed on the upper end of the vehicle body (1), the third frame (25) is slidably connected in the second frame (24), and the third frame (25) extends out of the right side of the second frame (24), and a movable seat (243) is provided at both the front and rear ends of the left part of the third frame (25), and the movable seat (243) is slidably connected in the second frame (24), and two second screw rods (242) are symmetrically rotated and connected in the second frame (24), and the two second screw rods (242) respectively pass through the two movable seats (243), and the second screw rod (242) and the movable seat (243) are connected through a ball nut pair; A fourth drive device is provided at the right end of the second frame (24), and the fourth drive device is located outside the third frame (25). The output shaft of the fourth drive device is connected to a second screw rod (242). The left end of the second frame (24) is symmetrically rotated and connected to two sprockets (244), and the two sprockets (244) are connected to each other through a chain. The left ends of the two second screw rods (242) pass through the second frame (24) and are respectively connected to the two sprockets (244).

9. The aircraft snow removal vehicle according to claim 8, characterized in that: A first ladder frame (21) is provided at the lower right end of the first frame (2), and the first ladder frame (21) is located on the right side of the vehicle body (1) and the right side of the third frame (25). The right end of the first ladder frame (21) is slidably connected to the second ladder frame (23), and the second ladder frame (23) extends from the lower side of the first ladder frame (21). Two movable components are symmetrically installed at the lower end of the second ladder frame (23).

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