Aircraft parking device for building outer wall

Abstract

The utility model discloses an aircraft parking device for a building outer wall, which relates to the field of aircrafts and comprises a parking bin, a bin door is rotatably mounted on the inner wall of the parking bin, a mounting groove is formed in the upper side of the parking bin, and a silica gel cushion convenient for buffering is fixedly mounted in the mounting groove. A storage groove is formed in the upper side of the parking bin, and a second-stage driving hole is formed in the inner wall of the storage groove. According to the device, an aircraft is transported to fly, a hanging rod is attached to a silica gel buffering pad, then a clamping motor is started, a starting motor is started, and the output end of the starting motor drives a sealing plate to rotate; and the sealing plate rotates outwards to open the inner bin of the transportation aircraft, the sealing plate drives the bin door to be opened together, the conveying motor is started, the output end of the conveying motor drives the conveying belt to rotate, the conveying belt conveys the goods pushed in to a designated pickup area, pickup is completed, and the pickup convenience is greatly improved.

Description

Technical Field

[0001] The utility model relates to the field of aircraft, and in particular to an aircraft parking device for building exterior walls. Background Art

[0002] With the promotion of low-altitude economy, drone logistics and UAM urban air traffic systems are gradually being promoted. The site conditions required for drone takeoff and landing do not match the urban building environment. The designated takeoff and landing areas are often in remote areas with insufficient logistics demand. People-concentrated areas have high logistics demand but cannot get effective drone logistics services. Traditional tricycle / electric vehicle transportation puts a serious burden on traffic. The traditional method of setting up a helipad on the top of the building is inefficient, difficult to pick up, and has many disadvantages because it cannot be delivered directly to the direct destination and requires another transfer. At the same time, the top of the building is mostly occupied by fire water tanks, air conditioners, or various maintenance machinery. In response to the pain points of the current traditional helipad, the utility model sets up a vertical lifting parking device on the outer wall of the building for taking off and landing aircraft, improving efficiency and saving take-off and landing sites. Utility Model Content

[0003] The purpose of this application is to provide an aircraft parking device for a building exterior wall, which is used for taking off and landing aircraft, thereby improving efficiency and saving take-off and landing space.

[0004] To achieve the above-mentioned objectives, the present application provides the following technical solutions: an aircraft parking device for a building exterior wall, comprising a parking compartment, a compartment door being rotatably installed on the inner wall of the parking compartment, an installation groove being provided on the upper side of the parking compartment, a silicone cushioning pad being fixedly installed in the installation groove for facilitating cushioning, a storage groove being provided on the upper side of the parking compartment, a secondary drive hole being provided on the inner wall of the storage groove, a clip being rotatably installed in the secondary drive hole for facilitating limiting the hanging rod, a snap-on motor being fixedly installed on one side of the parking compartment, and an output shaft of the snap-on motor being fixedly connected to one side of the clip.

[0005] Preferably, a limiting tube is fixedly installed on the lower side of the parking compartment, a parking platform for parking the aircraft is fixedly installed on one side of the limiting tube, two adjustment tubes are slidably installed on the inner wall of the limiting tube, and the opposite ends of the two adjustment tubes are fixedly installed with splints for fixing the transport aircraft.

[0006] Preferably, a dual-axis motor is fixedly mounted on the inner wall of the position-limiting tube, and an adjusting screw is fixedly mounted on both output ends of the dual-axis motor. The two adjusting tubes are correspondingly threadedly mounted on the surfaces of the two adjusting screws.

[0007] Preferably, a plurality of damping telescopic rods are fixedly mounted on the upper side of the docking platform, a same buffer plate is fixedly mounted on the top ends of the plurality of damping telescopic rods, and buffer springs are sleeved and mounted on the surfaces of the plurality of damping telescopic rods.

[0008] Preferably, a mounting opening is provided on the upper side of the buffer plate, and a first-level positioner is fixedly installed in the mounting opening.

[0009] Preferably, a conveyor belt is fixedly installed on the inner wall of the berthing bin, a three-stage drive hole is opened on one side of the berthing bin, a conveying motor is fixedly installed on one side of the berthing bin, and the output end of the conveying motor is fixedly connected to the transmission roller of the transmission belt.

[0010] In summary, the technical effects and advantages of the utility model are:

[0011] 1. In the utility model, the transport aircraft flies and fits the hanging rod on the silicone cushion pad, and then the clamping motor is started, the output end of the clamping motor drives the clamp to rotate, and the hanging rod is limited and fixed, thereby fixing the transport aircraft, so that the sealing plate fits the warehouse door, and then the opening motor is started, the opening motor output end drives the sealing plate to rotate, so that the sealing plate rotates outward to open the inner warehouse of the transport aircraft, and the sealing plate drives the warehouse door to open together, so that the transport aircraft is connected with the parking warehouse, and the pushing motor is started, the pushing motor output end drives the driving screw to rotate, the driving screw drives the driving block to move, and the driving block drives the pushing plate to move, thereby pushing the goods in the transport aircraft into the parking warehouse, and starting the transmission motor, the transmission motor output end drives the conveyor belt to rotate, and the transmission belt transports the pushed goods to the designated pickup area, completing the pickup, which greatly improves the convenience of pickup.

[0012] 2. In the present invention, the output end of the dual-axis motor drives the two adjusting screws to rotate, and the two adjusting screws respectively drive the corresponding adjusting tubes to move. The two adjusting tubes drive the corresponding two splints to approach each other, squeezing and fixing the surface of the transport aircraft, thereby improving the stability of the transport aircraft when parked.

[0013] 3. In the present invention, when the transport aircraft lands on the docking platform, the downward impact force of the aircraft is received by the buffer plate, and the downward impact is offset by the buffer spring, and the rebound force of the spring is offset by the damping telescopic rod, thereby buffering the transport aircraft and effectively protecting the transport aircraft. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present application. For those skilled in the art, other drawings can be obtained based on these drawings without paying any creative work.

[0015] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model;

[0016] Figure 2 This is a schematic diagram of the explosion structure of the utility model;

[0017] Figure 3 This is a schematic diagram of the related structure of the clamping block and the hanging rod in the utility model;

[0018] Figure 4 This is a schematic diagram of the cutaway structure of the utility model;

[0019] Figure 5 This is a schematic diagram of the cross-sectional structure of the regulating tube in the present utility model;

[0020] Figure 6 It is a schematic diagram of the cross-section structure of the buffer plate in the present invention.

[0021] In the figure: 1. Parking compartment; 2. Transport aircraft; 3. Hanging rod; 4. Silicone cushion; 5. Clamp; 6. Snap-on motor; 7. Limiting tube; 8. Parking platform; 9. Damping telescopic rod; 10. Buffer spring; 11. Buffer plate; 12. Adjusting tube; 13. Clamp; 14. Dual-axis motor; 15. Adjusting screw; 16. Primary positioner; 17. Secondary positioner; 18. Driving block; 19. Push plate; 20. Driving screw; 21. Pushing motor; 22. Sealing plate; 23. Opening motor; 24. Warehouse door; 25. Conveyor belt; 26. Conveying motor. DETAILED DESCRIPTION

[0022] 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 embodiments described 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 making creative efforts are within the scope of protection of the present invention.

[0023] See also Figure 1-6 , the embodiment provided by the utility model:

[0024] The transport aircraft 2 includes a controller, a flight wing, and an energy supply battery. The flight principle of the transport aircraft 2 is consistent with the existing UAV technology. A cargo transport compartment is provided in the transport aircraft 2. A push plate 19 is slidably installed on the inner wall of the transport aircraft 2. The push plate 19 is convenient for pushing the cargo in the cargo compartment of the transport aircraft 2. A sliding groove is provided on the upper side of the transport aircraft 2. A first-level driving hole is provided on one side of the transport aircraft 2. A sealing plate 22 is rotatably installed in the first-level driving hole. An opening motor 23 is fixedly installed on one side of the transport aircraft 2. The output shaft of the opening motor 23 is fixedly connected to one side of the sealing plate 22. The opening motor 23 is a servo motor. A compartment door 24 is rotatably installed on the inner wall of the docking compartment 1. The compartment door 24 is connected by a rotating shaft and can be rotated in the left and right directions. A hanging rod 3 is fixedly installed on one side of the transport aircraft 2. An installation slot is provided on the upper side of the docking compartment 1. A silicone cushioning pad 4 is fixedly installed in the groove for buffering the hanging rod 3. The hanging rod 3 is in the shape of a round rod and a semicircular buffering groove is provided on the upper side of the silicone cushioning pad 4. A storage groove is provided on the upper side of the parking compartment 1. A secondary driving hole is provided on the inner wall of the storage groove. A clip 5 is rotatably installed in the secondary driving hole for limiting the hanging rod 3. A semicircular slot is provided on the upper side of the clip 5. A card-connecting motor 6 is fixedly installed on one side of the parking compartment 1. The output shaft of the card-connecting motor 6 is fixedly connected to one side of the clip 5. A limit tube 7 is fixedly installed on the lower side of the berth 1, and a docking platform 8 for docking the aircraft is fixedly installed on one side of the limit tube 7, which is convenient for docking the transport aircraft 2. A conveyor belt 25 is fixedly installed on the inner wall of the berth 1. The height of the conveyor belt 25 is the same as the height inside the transport aircraft 2 warehouse, which is convenient for transporting goods. A three-level drive hole is opened on one side of the berth 1, and a transmission motor 26 is fixedly installed on one side of the berth 1. The output end of the transmission motor 26 is fixedly connected to the transmission roller of the transmission belt.

[0025] like Figure 4 As shown, a slide groove is provided on the inner top wall of the transport aircraft 2, and a driving block 18 is slidably installed on the inner wall of the slide groove. The lower side of the driving block 18 is fixedly connected to the upper side of the push plate 19, and a driving screw 20 is rotatably installed on the inner wall of the slide groove. The driving block 18 is screwed on the surface of the driving screw 20. A motor groove is provided on the inner wall of the slide groove, and a pushing motor 21 is fixedly installed in the motor groove. The pushing motor 21 is a servo motor, and the output shaft of the pushing motor 21 is coaxially fixedly connected to one end of the driving screw 20.

[0026] like Figure 4 and Figure 6As shown, a plurality of damping telescopic rods 9 are fixedly installed on the upper side of the parking platform 8, and a same buffer plate 11 is fixedly installed on the top of the plurality of damping telescopic rods 9. The surfaces of the plurality of damping telescopic rods 9 are sleeved with buffer springs 10. When the transport aircraft 2 lands on the parking platform 8, the downward impact force of the aircraft is received by the buffer plate 11, and the downward impact is offset by the buffer spring 10, and the rebound force of the spring is offset by the damping telescopic rod 9, thereby buffering the transport aircraft 2. An installation opening is opened on the upper side of the buffer plate 11, and the installation opening is provided inside the A first-level locator 16 is fixedly installed, and a corresponding second-level locator 17 is fixedly installed on the lower side of the transport aircraft 2. The first-level locator 16 and the locator are existing technologies, which can enable the transport aircraft 2 to locate the position of the buffer plate 11. At the same time, a visual sensor is installed on the transport aircraft 2, which can determine the specific parking position based on visual effects. In addition, power supply connectors are also installed on the first-level locator 16 and the second-level locator 17. When the first-level locator 16 and the second-level locator 17 are attached together, the transport aircraft 2 can be replenished with energy.

[0027] When the device is in use, it is first necessary to open up the outer wall of the building to the outside world, and then install the parking compartment 1 at the connecting port, and the parking platform 8 of the parking compartment 1 is facing the outside of the building, and then it can be used. When the transport aircraft 2 needs to transport the goods into the parking compartment 1, firstly, the first-level positioning and the second-level positioning device 17 are used to quickly locate the landing position of the transport aircraft 2. At the same time, the transport aircraft 2 is equipped with a visual sensor to determine the specific parking direction. When the aircraft is slowly parked, the hanging rod 3 is attached to the silicone cushion pad 4, and the clamping motor 6 is first started. The output end of the clamping motor 6 drives the clamp 5 to rotate, and the hanging rod 3 is limited and fixed, thereby fixing the transport aircraft 2, so that the sealing plate 22 is attached to the warehouse door 24. At the same time, The lower side of the transport aircraft 2 is fitted with the upper side of the buffer plate 11, and then the opening motor 23 is started. The output end of the opening motor 23 drives the sealing plate 22 to rotate, so that the sealing plate 22 rotates outward to open the inner warehouse of the transport aircraft 2, and the sealing plate 22 drives the warehouse door 24 to open together, so that the transport aircraft 2 is connected with the parking warehouse 1, and finally the pushing motor 21 is started. The output end of the pushing motor 21 drives the driving screw 20 to rotate, and the driving screw 20 drives the driving block 18 to move, and the driving block 18 drives the pushing plate 19 to move, thereby pushing the goods in the transport aircraft 2 into the parking warehouse 1, and by starting the conveying motor 26, the output end of the conveying motor 26 drives the conveyor belt 25 to rotate, and the transmission belt transports the pushed goods to the designated pickup area to complete the pickup.

[0028] like Figure 2 and 5As shown, two adjusting tubes 12 are slidably installed on the inner wall of the limiting tube 7, and the opposite ends of the two adjusting tubes 12 are fixedly installed with splints 13 for fixing the transport aircraft 2. The inner wall of the limiting tube 7 is fixedly installed with a dual-axis motor 14. The dual-axis motor 14 is a prior art, which has two driving shafts and can rotate in the same direction. The two output ends of the dual-axis motor 14 are fixedly installed with adjusting screws 15, and the thread lines of the two adjusting screws 15 are in opposite directions. The two adjusting tubes 12 are correspondingly screwed and installed on the surfaces of the two adjusting screws 15. The output end of the dual-axis motor 14 drives the two adjusting screws 15 to rotate, and the two adjusting screws 15 respectively drive the corresponding adjusting tubes 12 to move, and the two adjusting tubes 12 drive the corresponding two splints 13 to approach each other, squeeze and fix the surface of the transport aircraft 2, thereby improving the parking stability of the transport aircraft 2.

[0029] Finally, it should be noted that the above are only preferred embodiments of the present invention and are not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments or make equivalent replacements for some of the technical features therein. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. An aircraft parking device for a building exterior wall, comprising a parking compartment (1), characterized in that: A door (24) is rotatably mounted on the inner wall of the mooring bin (1), a mounting groove is provided on the upper side of the mooring bin (1), a silicone cushioning pad (4) for facilitating buffering is fixedly mounted in the mounting groove, a receiving groove is provided on the upper side of the mooring bin (1), a secondary driving hole is provided on the inner wall of the receiving groove, a clamp (5) for facilitating limiting the hanging rod (3) is rotatably mounted in the secondary driving hole, a clamping motor (6) is fixedly mounted on one side of the mooring bin (1), and an output shaft of the clamping motor (6) is fixedly connected to one side of the clamp (5).

2. The aircraft parking device for a building exterior wall according to claim 1, characterized in that: A limiting tube (7) is fixedly installed on the lower side of the parking compartment (1), a parking platform (8) for parking the aircraft is fixedly installed on one side of the limiting tube (7), two adjusting tubes (12) are slidably installed on the inner wall of the limiting tube (7), and splints (13) for fixing the transport aircraft (2) are fixedly installed at opposite ends of the two adjusting tubes (12).

3. The aircraft parking device for a building exterior wall according to claim 2, characterized in that: A dual-axis motor (14) is fixedly mounted on the inner wall of the position limiting tube (7), and an adjusting screw (15) is fixedly mounted on both output ends of the dual-axis motor (14). The two adjusting tubes (12) are correspondingly screw-connected and mounted on the surfaces of the two adjusting screws (15).

4. The aircraft parking device for a building exterior wall according to claim 3, characterized in that: A plurality of damping telescopic rods (9) are fixedly mounted on the upper side of the docking platform (8); a common buffer plate (11) is fixedly mounted on the top ends of the plurality of damping telescopic rods (9); and a buffer spring (10) is sleeved and mounted on the surfaces of the plurality of damping telescopic rods (9).

5. The aircraft parking device for building exterior walls according to claim 4, characterized in that: An installation opening is provided on the upper side of the buffer plate (11), and a first-level positioner (16) is fixedly installed in the installation opening.

6. The aircraft parking device for building exterior walls according to claim 5, characterized in that: A conveyor belt (25) is fixedly installed on the inner wall of the mooring bin (1), a three-stage drive hole is opened on one side of the mooring bin (1), a conveying motor (26) is fixedly installed on one side of the mooring bin (1), and the output end of the conveying motor (26) is fixedly connected to the transmission roller of the transmission belt.

Images