Airplane deicing device

Abstract

The invention belongs to the technical field of aircraft deicing devices, and discloses an aircraft deicing device which comprises a mounting plate, and a fixing plate is fixedly mounted at the bottom of the right side of the mounting plate. According to the deicing device, a rotating rod, a spring, a flexible sponge and a tooth plate are arranged, an operator can start a first motor to enable a rotating shaft to drive a first gear to rotate when deicing is carried out on wings of an airplane, and due to the fact that the outer surface of the first gear is meshed with the outer surface of a second gear, the second gear can rotate; then, a first gear and a second gear can drive a tooth plate to move rightwards, so that a round rod moves rightwards, the round rod extrudes and pushes the inner surface of a sliding groove, rotating rods rotate with a round shaft as the axis, the two rotating rods get close gradually, a flexible sponge can make contact with the outer surface of the wing, and the wing is protected from being damaged. And when the mechanical arm moves, the flexible sponge is driven to move, so that loose ice on the surface of the wing is pushed away and scraped off.

Description

Technical Field

[0001] The invention belongs to the technical field of aircraft deicing devices, in particular to an aircraft deicing device. Background Art

[0002] When the temperature in winter drops below 5℃ and is accompanied by humid cold air, ice, snow and frost will form, especially at airports in the extremely cold northern regions, where ice, snow and frost are more likely to form on the surface of aircraft at the airport.

[0003] To ensure the normal operation of the aircraft, the ice on its surface must be cleared before takeoff to prevent the ice from affecting the airflow passing through the fuselage. At present, aircraft de-icing usually uses large de-icing equipment such as de-icing vehicles to de-ice the aircraft. This de-icing device has a complex structure and is relatively bulky. Especially when de-icing raised positions such as wings and tail vertebrae, it is impossible to de-ice both sides of the wing or tail vertebrae at the same time, so the operator needs to adjust the position of the nozzle back and forth, which is not only time-consuming and labor-intensive, but also has low de-icing efficiency, so it needs to be improved. Summary of the invention

[0004] The object of the present invention is to provide an aircraft deicing device to solve the problems raised in the above background technology.

[0005] In order to achieve the above object, the present invention provides the following technical solution: an aircraft deicing device, comprising:

[0006] A mounting plate, a fixing plate being fixedly mounted on the bottom of the right side of the mounting plate;

[0007] A deicing mechanism, wherein the deicing mechanism is arranged on the right side of the mounting plate;

[0008] A driving mechanism, wherein the driving mechanism is arranged inside the mounting plate;

[0009] In which, the de-icing mechanism includes a round shaft, the outer surface of the round shaft is fixedly sleeved with the inner wall of the fixed plate, the outer surface of the round shaft is movably sleeved with a rotating rod, a sliding groove is opened inside the rotating rod, an installation box is fixedly installed on the inner side of the rotating rod, a movable block is movably sleeved inside the installation box, a spring is fixedly installed on the inner surface of the movable block, the other end of the spring is fixedly connected to the outer surface of the rotating rod, a flexible sponge is fixedly installed on the outer surface of the movable block, the front and rear sides of the interior of the installation plate are movably sleeved with toothed plates, the right end of the toothed plate is fixedly connected with a connecting plate, a round rod is fixedly sleeved inside the connecting plate, the top end of the round rod penetrates the connecting plate and extends to the interior of the sliding groove and is movably connected to the inner surface of the sliding groove, and the movement of the connecting plate will cause the round rod to squeeze and push the inner surface of the sliding groove.

[0010] Preferably, the driving mechanism comprises:

[0011] A first motor, wherein the top of the first motor is fixedly connected to the bottom of the mounting plate, the other end of the output shaft of the first motor is fixedly connected to a rotating shaft, the top end of the rotating shaft passes through the mounting plate and extends to the inside of the mounting plate and is movably sleeved with the inner wall of the mounting plate, and the outer surface of the rotating shaft is fixedly sleeved with a first gear located inside the mounting plate;

[0012] A fixed shaft, the outer surface of which is fixedly sleeved with the inner wall of the mounting plate, the outer surface of which is movably sleeved with a second gear, the outer surface of the second gear is meshingly connected with the outer surface of the first gear, and the outer surfaces of the first gear and the second gear are both meshingly connected with the inner surface of the tooth plate.

[0013] Preferably, a rotating plate is fixedly mounted on the left side of the mounting plate, a fixing block is movably sleeved on the outer surface of the rotating plate, and a mechanical arm is fixedly connected to the left side of the fixing block.

[0014] Preferably, a second motor is fixedly sleeved inside the right end of the robotic arm, and the other end of the output shaft of the second motor is fixedly connected to a rotating shaft, the other end of the rotating shaft passes through the fixed block and extends to the interior of the rotating plate and is movably sleeved with the inner wall of the fixed block, and the outer surface of the rotating shaft is fixedly sleeved with the inner wall of the rotating plate.

[0015] Preferably, a mounting block is fixedly mounted on the top of the robotic arm, and a conveying pipe is fixedly sleeved inside the mounting block.

[0016] Preferably, a steam diverter valve is fixedly connected to the right end of the delivery pipe, and both ends of the steam diverter valve are fixedly connected to a heat-resistant hose.

[0017] Preferably, a top plate is fixedly installed on the top of the rotating rod, a clamping ring is fixedly installed on the top of the top plate, a fixed tube is fixedly sleeved inside the clamping ring, the clamping ring fixes the fixed tube, the left end of the fixed tube is fixedly connected to the right end of the heat-resistant hose, and a nozzle is fixedly connected to the outer surface of the fixed tube.

[0018] Preferably, a support plate is fixedly mounted on the top of the mounting plate, a cylinder is fixedly sleeved between the support plates, and a lighting lamp is movably sleeved on the outer surface of the cylinder.

[0019] Preferably, a fixing rod is fixedly connected between the support plates, a rotating block is movably sleeved on the outer surface of the fixing rod, a pneumatic cylinder is fixedly connected to the outer surface of the rotating block, and the top end of the pneumatic cylinder is hinged to the bottom end of the lighting lamp.

[0020] The beneficial effects of the present invention are as follows:

[0021] 1. The present invention provides a rotating rod, a spring, a flexible sponge and a toothed plate. When an operator de-ices an aircraft wing, the operator can start the first motor to make the rotating shaft drive the first gear to rotate. Since the outer surface of the first gear meshes with the outer surface of the second gear, the second gear can rotate, and then the first gear and the second gear can drive the toothed plate to move rightward, thereby causing the round rod to move rightward. The round rod will squeeze and push the inner surface of the slide groove, thereby causing the rotating rod to rotate around the circular axis, and then the two rotating rods will gradually approach each other, so that the flexible sponge can contact the outer surface of the wing. When the mechanical arm moves, it will drive the flexible sponge to move, thereby pushing away and scraping off the loose ice on the wing surface, thereby improving the de-icing efficiency.

[0022] 2. The present invention provides a delivery pipe, a heat-resistant hose, a fixed pipe and a nozzle. High-pressure steam will enter the interior of the fixed pipe through the delivery pipe and the heat-resistant hose, and then be sprayed out by the nozzle, so that the ice on the outer surface of the wing can be removed, thereby achieving the purpose of rapid de-icing. The operator can start the second motor so that the rotating shaft drives the rotating plate to rotate, and then drives the mounting plate to rotate, thereby adjusting the angle of the mounting plate.

[0023] 3. The present invention provides a cylinder, a lighting lamp and a pneumatic cylinder. Due to the design of the lighting lamp, the lighting lamp can play a lighting role after being turned on, so as to facilitate the operator to de-ice the aircraft at night. The operator can start the pneumatic cylinder so that the pneumatic cylinder can push the lighting lamp to rotate around the cylinder as the axis, thereby adjusting the angle of the lighting lamp and then adjusting the lighting angle, which is convenient for the operator to use. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 It is a schematic diagram of the structure of the present invention;

[0025] Figure 2 It is a schematic cross-sectional structural diagram of the side of the present invention;

[0026] Figure 3 It is a schematic cross-sectional structural diagram of the movable block of the present invention;

[0027] Figure 4 It is a schematic cross-sectional structural diagram of the mounting plate of the present invention;

[0028] Figure 5 It is a schematic diagram of the bottom structure of the present invention when viewed from above;

[0029] Figure 6 for Figure 2 A schematic diagram of the local enlarged structure at point A in the middle;

[0030] Figure 7 for Figure 3Schematic diagram of the local enlarged structure at point B in the middle.

[0031] In the figure: 1. mounting plate; 2. fixing plate; 3. round shaft; 4. rotating rod; 5. slide groove; 6. mounting box; 7. spring; 8. movable block; 9. flexible sponge; 10. tooth plate; 11. connecting plate; 12. round rod; 13. first motor; 14. rotating shaft; 15. first gear; 16. fixed shaft; 17. second gear; 18. mechanical arm; 19. fixed block; 20. rotating plate; 21. second motor; 22. rotating shaft; 23. mounting block; 24. conveying pipe; 25. steam diverter valve; 26. heat-resistant hose; 27. fixed pipe; 28. nozzle; 29. ​​retaining ring; 30. supporting plate; 31. cylinder; 32. lighting lamp; 33. fixing rod; 34. rotating block; 35. pneumatic cylinder; 36. top plate. DETAILED DESCRIPTION

[0032] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0033] like Figures 1 to 7 As shown, an embodiment of the present invention provides an aircraft deicing device, comprising:

[0034] A mounting plate 1, a fixing plate 2 is fixedly mounted on the bottom of the right side of the mounting plate 1;

[0035] A deicing mechanism, which is arranged on the right side of the mounting plate 1;

[0036] A driving mechanism, the driving mechanism is arranged inside the mounting plate 1;

[0037] Among them, the de-icing mechanism includes a circular shaft 3, the outer surface of the circular shaft 3 is fixedly sleeved with the inner wall of the fixed plate 2, the outer surface of the circular shaft 3 is movably sleeved with a rotating rod 4, a slide groove 5 is opened inside the rotating rod 4, the inner side of the rotating rod 4 is fixedly installed with a mounting box 6, the interior of the mounting box 6 is movably sleeved with a movable block 8, the inner surface of the movable block 8 is fixedly installed with a spring 7, the other end of the spring 7 is fixedly connected to the outer surface of the rotating rod 4, the outer surface of the movable block 8 is fixedly installed with a flexible sponge 9, the front and rear sides of the interior of the mounting plate 1 are movably sleeved with toothed plates 10, the right end of the toothed plate 10 is fixedly connected with a connecting plate 11, the interior of the connecting plate 11 is fixedly sleeved with a round rod 12, the top end of the round rod 12 penetrates the connecting plate 11 and extends to the interior of the slide groove 5 and is movably connected to the inner surface of the slide groove 5, the movement of the connecting plate 11 will cause the round rod 12 to squeeze and push the inner surface of the slide groove 5.

[0038] By setting the tooth plates 10, when the two tooth plates 10 move to the right, the connecting plate 11 and the round rod 12 will be driven to move to the right, so that the outer surface of the round rod 12 squeezes and pushes the inner surface of the slide groove 5, and then the rotating rod 4 can rotate inward with the round shaft 3 as the axis, so that the flexible sponge 9 can contact the outer surface of the aircraft wing. When the mounting plate 1 moves back and forth as a whole, the flexible sponge 9 can push and scrape off the melted and loosened ice on the outer surface of the wing, thereby speeding up the removal of ice on the aircraft surface.

[0039] The driving mechanism includes:

[0040] A first motor 13, the top of the first motor 13 is fixedly connected to the bottom of the mounting plate 1, the other end of the output shaft of the first motor 13 is fixedly connected to a rotating shaft 14, the top end of the rotating shaft 14 passes through the mounting plate 1 and extends to the inside of the mounting plate 1 and is movably sleeved with the inner wall of the mounting plate 1, and the outer surface of the rotating shaft 14 is fixedly sleeved with a first gear 15 located inside the mounting plate 1;

[0041] A fixed shaft 16, the outer surface of which is fixedly sleeved with the inner wall of the mounting plate 1, the outer surface of which is movably sleeved with a second gear 17, the outer surface of which is meshingly connected with the outer surface of the first gear 15, and the outer surfaces of the first gear 15 and the second gear 17 are both meshingly connected with the inner surface of the tooth plate 10.

[0042] The operator starts the first motor 13 to make the rotating shaft 14 drive the first gear 15 to rotate, so that the first gear 15 drives the second gear 17 to rotate, and further the first gear 15 and the second gear 17 can drive the tooth plate 10 to move.

[0043] A rotating plate 20 is fixedly mounted on the left side of the mounting plate 1 , a fixing block 19 is movably sleeved on the outer surface of the rotating plate 20 , and a mechanical arm 18 is fixedly connected to the left side of the fixing block 19 .

[0044] When the mechanical arm 18 is in operation, it will drive the fixed block 19 and the rotating plate 20 to move, thereby enabling the mounting plate 1 to move.

[0045] Among them, a second motor 21 is fixedly sleeved inside the right end of the robotic arm 18, and the other end of the output shaft of the second motor 21 is fixedly connected to a rotating shaft 22. The other end of the rotating shaft 22 passes through the fixed block 19 and extends to the interior of the rotating plate 20 and is movably sleeved with the inner wall of the fixed block 19. The outer surface of the rotating shaft 22 is fixedly sleeved with the inner wall of the rotating plate 20.

[0046] The operator starts the second motor 21 so that the rotating shaft 22 can drive the rotating plate 20 to rotate, thereby causing the mounting plate 1 to rotate.

[0047] A mounting block 23 is fixedly mounted on the top of the robot arm 18 , and a conveying pipe 24 is fixedly sleeved inside the mounting block 23 .

[0048] By providing the mounting block 23 , the mounting block 23 can fix the delivery pipe 24 .

[0049] The right end of the delivery pipe 24 is fixedly connected to a steam diverter valve 25 , and both ends of the steam diverter valve 25 are fixedly connected to heat-resistant hoses 26 .

[0050] By providing the steam diverter valve 25 , the steam diverter valve 25 can divert the high-pressure steam delivered through the delivery pipe 24 .

[0051] Among them, a top plate 36 is fixedly installed on the top of the rotating rod 4, and a clamping ring 29 is fixedly installed on the top of the top plate 36. A fixed tube 27 is fixedly sleeved inside the clamping ring 29. The clamping ring 29 fixes the fixed tube 27. The left end of the fixed tube 27 is fixedly connected to the right end of the heat-resistant hose 26, and the outer surface of the fixed tube 27 is fixedly connected to the nozzle 28.

[0052] The steam delivered through the heat-resistant hose 26 can be sprayed through the nozzle 28 to remove ice from the wings of the aircraft.

[0053] A support plate 30 is fixedly mounted on the top of the mounting plate 1 , a cylinder 31 is fixedly sleeved between the support plates 30 , and an illuminating lamp 32 is movably sleeved on the outer surface of the cylinder 31 .

[0054] By providing the lighting lamp 32 , the lighting lamp 32 can play a lighting role, thereby facilitating operators to perform de-icing operations at night.

[0055] Among them, a fixing rod 33 is fixedly connected between the support plates 30, a rotating block 34 is movably sleeved on the outer surface of the fixing rod 33, a pneumatic cylinder 35 is fixedly connected to the outer surface of the rotating block 34, and the top end of the pneumatic cylinder 35 is hinged to the bottom end of the lighting lamp 32.

[0056] The operator can start the pneumatic cylinder 35 so that the pneumatic cylinder 35 pulls the lighting lamp 32 to rotate around the cylinder 31 as the axis, thereby adjusting the lighting angle of the lighting lamp 32 .

[0057] Working principle and usage process:

[0058] After the operator parks the de-icing vehicle at a suitable position, the operator starts the mechanical arm 18, which drives the mounting plate 1 to move, thereby moving the two flexible sponges 9 to both sides of the wing. By delivering high-pressure steam to the inside of the delivery pipe 24, the steam will enter the inside of the fixed pipe 27 through the heat-resistant hose 26, and then be sprayed out by the nozzle 28, thereby clearing the ice covering the outer surface of the wing and allowing the ice to melt quickly.

[0059] When the ice on the outer surface of the wing melts and loosens, the first motor 13 can be started to make the rotating shaft 14 drive the first gear 15 to rotate, and then the first gear 15 drives the second gear 17 to rotate. Since the outer surfaces of the first gear 15 and the second gear 17 are meshed with the inner surface of the toothed plate 10, the first gear 15 and the second gear 17 can drive the toothed plate 10 to move rightward, so that the connecting plate 11 and the round rod 12 move rightward, and the outer surface of the round rod 12 will squeeze and push the inner surface of the slide groove 5, so that the rotating rod 4 rotates around the circular shaft 3 as the axis, so that the two rotating rods 4 gradually approach each other, so that the two flexible sponges 9 can contact the outer surface of the wing. After being subjected to pressure, the spring 7 will push the movable block 8 outward, so that the flexible sponge 9 can fit the outer surface of the wing. When the mechanical arm 18 moves, it will drive the flexible sponge 9 to move, so that the flexible sponge 9 can simultaneously push away and scrape off the loose ice on both sides of the wing, thereby improving the de-icing efficiency.

[0060] When the operator de-ices the aircraft at night, the operator can start the lighting lamp 32 so that the lighting lamp 32 can play a lighting role, thereby facilitating the operator to perform de-icing operations. The operator can start the pneumatic cylinder 35 so that the pneumatic cylinder 35 drives the lighting lamp 32 to rotate around the cylinder 31 as the axis, and then adjust the angle of the lighting lamp 32, thereby adjusting the lighting angle, which is convenient for the operator to use and improves the flexibility of the device.

[0061] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.

[0062] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An aircraft deicing device, characterized in that: Included are: A mounting plate (1), wherein a fixing plate (2) is fixedly mounted on the bottom of the right side of the mounting plate (1); A deicing mechanism, wherein the deicing mechanism is arranged on the right side of the mounting plate (1); A driving mechanism, the driving mechanism being arranged inside the mounting plate (1); The deicing mechanism comprises a circular shaft (3), the outer surface of the circular shaft (3) is fixedly sleeved with the inner wall of the fixed plate (2), the outer surface of the circular shaft (3) is movably sleeved with a rotating rod (4), a sliding groove (5) is provided inside the rotating rod (4), a mounting box (6) is fixedly installed on the inner side of the rotating rod (4), a movable block (8) is movably sleeved inside the mounting box (6), a spring (7) is fixedly installed on the inner surface of the movable block (8), and the other end of the spring (7) is fixedly connected to the outer surface of the rotating rod (4). A flexible sponge (9) is fixedly mounted on the outer surface of the movable block (8); tooth plates (10) are movably sleeved on both the front and rear sides of the interior of the mounting plate (1); a connecting plate (11) is fixedly connected to the right end of the tooth plate (10); a round rod (12) is fixedly sleeved inside the connecting plate (11); the top end of the round rod (12) passes through the connecting plate (11) and extends to the interior of the slide groove (5) and is movably connected to the inner surface of the slide groove (5); the movement of the connecting plate (11) causes the round rod (12) to squeeze and push the inner surface of the slide groove (5).

2. An aircraft deicing device according to claim 1, characterized in that: The driving mechanism comprises: A first motor (13), the top of the first motor (13) is fixedly connected to the bottom of the mounting plate (1), the other end of the output shaft of the first motor (13) is fixedly connected to a rotating shaft (14), the top end of the rotating shaft (14) passes through the mounting plate (1) and extends to the inside of the mounting plate (1) and is movably sleeved with the inner wall of the mounting plate (1), and the outer surface of the rotating shaft (14) is fixedly sleeved with a first gear (15) located inside the mounting plate (1); A fixed shaft (16), the outer surface of which is fixedly sleeved with the inner wall of the mounting plate (1), the outer surface of which is movably sleeved with a second gear (17), the outer surface of which is meshingly connected with the outer surface of the first gear (15), and the outer surfaces of the first gear (15) and the second gear (17) are both meshingly connected with the inner surface of the tooth plate (10).

3. The aircraft deicing device according to claim 1, characterized in that: A rotating plate (20) is fixedly mounted on the left side of the mounting plate (1), a fixed block (19) is movably sleeved on the outer surface of the rotating plate (20), and a mechanical arm (18) is fixedly connected to the left side of the fixed block (19).

4. An aircraft deicing device according to claim 3, characterized in that: A second motor (21) is fixedly sleeved inside the right end of the mechanical arm (18); the other end of the output shaft of the second motor (21) is fixedly connected to a rotating shaft (22); the other end of the rotating shaft (22) passes through the fixed block (19) and extends to the inside of the rotating plate (20) and is movably sleeved with the inner wall of the fixed block (19); the outer surface of the rotating shaft (22) is fixedly sleeved with the inner wall of the rotating plate (20).

5. The aircraft deicing device according to claim 3, characterized in that: A mounting block (23) is fixedly mounted on the top of the mechanical arm (18), and a conveying pipe (24) is fixedly sleeved inside the mounting block (23).

6. An aircraft deicing device according to claim 5, characterized in that: The right end of the delivery pipe (24) is fixedly connected to a steam diverter valve (25), and both ends of the steam diverter valve (25) are fixedly connected to heat-resistant hoses (26).

7. The aircraft deicing device according to claim 1, characterized in that: A top plate (36) is fixedly installed on the top of the rotating rod (4), a clamping ring (29) is fixedly installed on the top of the top plate (36), a fixed tube (27) is fixedly sleeved inside the clamping ring (29), the clamping ring (29) plays a fixing role on the fixed tube (27), the left end of the fixed tube (27) is fixedly connected to the right end of the heat-resistant hose (26), and a nozzle (28) is fixedly connected to the outer surface of the fixed tube (27).

8. The aircraft deicing device according to claim 1, characterized in that: A support plate (30) is fixedly mounted on the top of the mounting plate (1), a cylinder (31) is fixedly sleeved between the support plates (30), and a lighting lamp (32) is movably sleeved on the outer surface of the cylinder (31).

9. An aircraft deicing device according to claim 8, characterized in that: A fixing rod (33) is fixedly connected between the support plates (30), a rotating block (34) is movably sleeved on the outer surface of the fixing rod (33), a pneumatic cylinder (35) is fixedly connected to the outer surface of the rotating block (34), and the top end of the pneumatic cylinder (35) is hinged to the bottom end of the lighting lamp (32).

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