Intelligent integrated nest capable of accommodating double airplanes

Abstract

The invention discloses an intelligent integrated nest capable of accommodating double airplanes, and relates to the technical field of unmanned aerial vehicles. Comprising a box body, electric push rods are installed on the front wall and the rear wall of an inner cavity of the box body, the output ends of the two electric push rods are connected with sliding covers through protruding blocks, the sliding covers are slidably installed on the top of the box body, bases are installed on the left side and the right side of the bottom of the inner cavity of the box body, and the bases are connected with fixing plates through balance assemblies. A connecting column is fixed to the upper end of the fixing plate, a mounting plate is fixed to the top of the connecting column, and through cooperation of an electric push rod, an oil liquid assembly, the mounting plate and a moving plate, the moving plate can conduct centering, abutting and limiting on the unmanned aerial vehicle, and meanwhile the area of the parking platform is increased when limiting of the unmanned aerial vehicle is relieved; through the cooperation between the arranged balance assembly and the double-shaft tilt angle sensor in the connecting column, when the mounting carrier or the placing position of the box body inclines, the stopping plate is always kept in a horizontal state.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and particularly to an intelligent integrated hangar capable of accommodating two aircrafts. Background Art

[0002] An intelligent integrated hangar generally refers to a highly automated and intelligent device or system for storing, maintaining, and managing devices such as unmanned aerial vehicles. It not only provides a safe parking location for unmanned aerial vehicles but also can automatically perform operations such as battery replacement, data transmission, and flight plan update, thus greatly improving the efficiency and autonomy of unmanned aerial vehicle operations. At the same time, with the increase in the application scenarios of unmanned aerial vehicles, some new types of mobile intelligent hangars or vehicle-mounted intelligent hangars are widely used because they inherit the functions of fixed hangars such as providing storage for unmanned aerial vehicles, automatic battery replacement, and data transmission, and also enhance the operation range and flexibility of unmanned aerial vehicles.

[0003] However, for the existing mobile intelligent integrated hangars for two aircrafts, in order to facilitate the installation and transportation of the vehicle carrier, most of them have been optimized in terms of being small or lightweight, resulting in a relatively small landing platform in the existing hangar, and it is easy for the unmanned aerial vehicle to fall and be damaged due to inaccurate landing. However, the landing platform in the hangar usually works in conjunction with a centering mechanism, which makes it inconvenient for the existing intelligent integrated hangar to have a centering mechanism function while increasing the area of the landing platform. On the other hand, when the existing mobile hangar is in use, if the parking position of the vehicle carrier is uneven or the position of the mobile intelligent hangar is uneven, it is easy for the unmanned aerial vehicle to deviate during takeoff and landing. However, the centering mechanism used in conjunction with the existing landing platform is fixedly installed, which makes it inconvenient for the existing intelligent integrated hangar to adjust the balance of the landing platform while not affecting the operation of the centering mechanism. Summary of the Invention

[0004] The purpose of the present invention is to provide an intelligent integrated hangar capable of accommodating two aircrafts to solve the problems proposed in the above background art that it is inconvenient for the existing intelligent integrated hangar to have a centering mechanism function while increasing the area of the landing platform, and it is also inconvenient to adjust the balance of the landing platform while not affecting the operation of the centering mechanism. The technical solution of the present invention provides a solution significantly different from the prior art for the technical problem that the prior art solution is too single.

[0005] To achieve the above object, the present invention provides the following technical solution: An intelligent integrated aircraft hangar capable of accommodating two aircraft, including a box body. Electric push rods are installed on the front and rear walls of the inner cavity of the box body. The output ends of the two electric push rods are connected with a sliding cover through bumps. The sliding cover is slidably installed on the top of the box body. Bases are installed on the left and right sides of the bottom of the inner cavity of the box body. The bases are connected with a fixing plate through a balancing component. A connecting column is fixed at the upper end of the fixing plate. An installation plate is fixed at the top of the connecting column. A plurality of first chutes are opened at the upper end of the installation plate. The inner side of the first chute is slidably connected with a second chute through a slider. The second chute is opened at the top end of an adjusting plate. The adjusting plate is rotatably installed outside the connecting column through a bearing. An installation block is fixed at the outer end of the slider. An expansion block is slidably connected with the inner cavity of the installation block through a spring. A moving plate is fixedly connected to the inward side of the expansion block. An expansion plate is slidably connected with the inner cavity of the moving plate through a spring; An oil hydraulic component, the oil hydraulic component is arranged between the electric push rod and the adjusting plate, and the oil hydraulic component is used for adjusting the position of the slider.

[0006] Preferably, a plurality of the first chutes and the second chutes are respectively arranged at equal angles on the installation plate and the adjusting plate. A plurality of the second chutes are designed as inclined arcs. The inclined arc design of the second chutes is used for adjusting the position of the slider.

[0007] Preferably, the outer side of the parking plate and the inward side of the moving plate are both inclined designs, and the inclined directions of the outer side of the parking plate and the inward side of the moving plate are opposite.

[0008] Preferably, the moving plate is arc-shaped, and the shape of the expansion plate corresponds to the shape of the moving plate.

[0009] Preferably, the balancing component includes a first gear disk and a rotating column. The first gear disk is rotatably installed at the rear side of the base through a motor. The rotating column is rotatably installed in a hole on one side of the base through a bearing. A second gear disk is meshed with the outer side of the first gear disk. The second gear disk is fixed on the outer side of the rear end of the rotating column. An adjusting rod is fixed on the outer side of the front end of the rotating column. A third gear disk is rotatably connected with the groove of the adjusting rod through a motor. The outer end of the third gear disk is meshed with an installation gear disk. The installation gear disk is rotatably installed in the groove of the adjusting rod through convex columns on the left and right sides. The fixing plate is installed at the upper end of the installation gear disk.

[0010] Preferably, the first gear disk and the third gear disk are respectively arranged on a transverse axis and a longitudinal axis.

[0011] Preferably, the oil fluid assembly includes two first oil fluid tanks, which are respectively installed at the left corner of the rear wall of the inner cavity of the box and the right corner of the front wall. A first plug body is slidably connected to the inner cavity of the first oil fluid tank through a spring. The inner cavity of the first plug body is connected to a second oil fluid tank through a hose. A second plug body is slidably connected to the inner cavity of the second oil fluid tank through a spring. The outer end of the second plug body is connected to an adjusting ring through a convex block, and the adjusting ring is installed at the bottom of the adjusting plate.

[0012] Preferably, the two first oil fluid tanks are arranged oppositely. The outer ends of the two first plug bodies respectively correspond to the convex blocks at the output ends of two electric push rods. The two electric push rods are arranged oppositely. The second oil fluid tank is designed in an arc shape, and the center of the arc of the second oil fluid tank corresponds to the center of the connecting column. A dual-axis inclination sensor is arranged inside the connecting column.

[0013] Compared with the prior art, the beneficial effects of the present invention are as follows: In the present invention, by setting electric push rods, sliding covers, oil fluid assemblies and adjusting plates, during the process of the electric push rods opening the sliding covers, the positions of the first plug bodies and the second plug bodies in the first oil fluid tank and the second oil fluid tank are adjusted synchronously, and the position of the adjusting plate is adjusted by driving the position adjustment of the second plug body, so that the position change of the second chute drives the slider and the moving plate to slide outwards in the first chute, so that the moving plate no longer resists and centers the drone. Cooperating with the springs in the mounting blocks to adjust the positions of the telescopic blocks and the moving plates, and the telescopic plates in the moving plates to expand and contract synchronously, thereby increasing the landing area of the drone on the landing board. When the drone takes off, while releasing the centering limit of the drone, a larger landing platform is provided for the landing of the drone. After the drone lands, the moving plate is reset to expand and contract to complete the centering resistance limit of the drone, thus optimizing the problem of the small landing platform in the nest caused by the miniaturization of the traditional mobile drone nest.

[0014] In the present invention, through the balance assembly and the dual-axis inclination sensor in the connecting column, when the installation carrier or the placement position of the box body is inclined, after the dual-axis inclination sensor in the connecting column detects the inclination angle data, the motor connecting the first gear disk and the third gear disk is started through the controller, and the corresponding positive or reverse rotation of the inclination angle is carried out, so that the first gear disk drives the second gear disk, the rotating column and the adjusting rod to adjust the horizontal position in the transverse direction, and at the same time the third gear disk drives the mounting gear disk, the fixing plate, the connecting column and the mounting plate to adjust the horizontal position in the longitudinal direction, so that the landing board always remains in a horizontal state, providing a stable take-off and landing platform for the drone, and reducing the damage caused by the drone landing accident due to the small landing platform. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a front cross-sectional structural schematic diagram of the present invention; Figure 2Schematic diagram of the split structure of the box body and the sliding cover of the present invention; Figure 3 Schematic diagram of the bottom view structure of the electric push rod, base, adjusting plate and oil fluid assembly of the present invention; Figure 4 Schematic diagram of the split bottom view structure of the balance assembly, adjusting plate, mounting plate, slider and stop plate of the present invention; Figure 5 Schematic diagram of the split top view structure of the stop plate, adjusting plate, mounting plate, moving plate and telescopic plate of the present invention; Figure 6 Schematic diagram of the unfolded top view structure of the moving plate and the telescopic plate of the present invention; Figure 7 Schematic diagram of the unfolded bottom view structure of the moving plate and the telescopic plate of the present invention; Figure 8 is Figure 7 Enlarged schematic diagram at position A in Figure 9 is Figure 7 Enlarged schematic diagram at position B in Figure 10 Schematic diagram of the structure of the oil fluid assembly and the balance assembly of the present invention; Figure 11 Schematic diagram of the split structure of the oil fluid assembly and the balance assembly of the present invention.

[0016] In the figure: 1. Box body; 2. Electric push rod; 3. Sliding cover; 4. Base; 5. Balance assembly; 51. First gear disk; 52. Second gear disk; 53. Rotating column; 54. Adjusting rod; 55. Third gear disk; 56. Mounting gear disk; 6. Fixed plate; 7. Connecting column; 8. Mounting plate; 9. First chute; 10. Slider; 11. Second chute; 12. Adjusting plate; 13. Stop plate; 14. Oil fluid assembly; 141. First oil tank; 142. First plug; 143. Second oil tank; 144. Second plug; 145. Adjusting ring; 151. Mounting block; 152. Telescopic block; 153. Moving plate; 154. Telescopic plate. Detailed implementation manners

[0017] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.

[0018] Embodiment 1

[0019] Please refer to Figures 1 to 11, the present invention provides a technical solution: an intelligent integrated hangar capable of accommodating two aircraft. Electric push rods 2 are installed on both the front wall and the rear wall of the inner cavity of the box body 1. The output ends of the two electric push rods 2 are connected with a sliding cover 3 through bumps. The sliding cover 3 is slidably installed on the top of the box body 1. Bases 4 are installed on both the left and right sides of the bottom of the inner cavity of the box body 1. The bases 4 are connected with a fixing plate 6 through a balance assembly 5. A connecting column 7 is fixed at the upper end of the fixing plate 6. An installation plate 8 is fixed at the top of the connecting column 7. A plurality of first chutes 9 are opened at the upper end of the installation plate 8. The inner side of the first chutes 9 is slidably connected with a second chute 11 through a slider 10. The second chute 11 is opened at the top end of an adjusting plate 12. The adjusting plate 12 is rotatably installed on the outside of the connecting column 7 through a bearing. The plurality of first chutes 9 and second chutes 11 are respectively opened at equal angles on the installation plate 8 and the adjusting plate 12. The plurality of second chutes 11 are designed as inclined arcs. The inclined arc design of the second chutes 11 is used to adjust the position of the slider 10. An installation block 151 is fixed at the outer end of the slider 10. An expansion block 152 is slidably connected to the inner cavity of the installation block 151 through a spring. A moving plate 153 is fixedly connected to the inward side of the expansion block 152. The outer side of the parking plate 13 and the inward side of the moving plate 153 are both inclined. The inclined directions of the outer side of the parking plate 13 and the inward side of the moving plate 153 are opposite. An expansion plate 154 is slidably connected to the inner cavity of the moving plate 153 through a spring. The moving plate 153 is arc-shaped. The shape of the expansion plate 154 corresponds to the shape of the moving plate 153. The oil hydraulic component 14 is arranged between the electric push rod 2 and the adjusting plate 12. The oil hydraulic component 14 includes two first oil hydraulic tanks 141. The two first oil hydraulic tanks 141 are respectively installed at the left angle of the rear wall of the inner cavity of the box body 1 and the right angle of the front wall. A first plug body 142 is slidably connected to the inner cavity of the first oil hydraulic tank 141 through a spring. The inner cavity of the first plug body 142 is connected with a second oil hydraulic tank 143 through a hose. The two first oil hydraulic tanks 141 are arranged oppositely. The outer ends of the two first plug bodies 142 respectively correspond to the bumps at the output ends of the two electric push rods 2. The two electric push rods 2 are arranged oppositely. The second oil hydraulic tank 143 is designed as an arc. The center of the arc of the second oil hydraulic tank 143 corresponds to the center of the connecting column 7. A dual-axis inclination sensor is arranged in the connecting column 7. A second plug body 144 is slidably connected to the inner cavity of the second oil hydraulic tank 143 through a spring. The outer end of the second plug body 144 is connected with an adjusting ring 145 through a bump. The adjusting ring 145 is installed at the bottom of the adjusting plate 12. The oil hydraulic component 14 is used to adjust the position of the slider 10; When using the drone, the operator starts two electric push rods 2 through the controller, causing the bumps at the output ends of the two electric push rods 2 to move relatively, and pushing the two sliding covers 3 to slide to the maximum opening positions on the left and right sides respectively at the upper end of the box body 1. At the same time, when the bumps at the output ends of the electric push rods 2 move to the large position, they will first touch the first plug body 142 in the corresponding moving direction, causing the first plug body 142 to move inward in the first oil tank 141, and squeezing the oil in the inner cavity of the first oil tank 141 into the second oil tank 143 through the hose. The increase in the oil in the inner cavity of the second oil tank 143 drives the second plug body 144 to move outward in the second oil tank 143. When the second plug body 144 moves, it drives the adjusting plate 12 to rotate and adjust the position on the connecting column 7 through the adjusting ring 145. When the adjusting plate 12 rotates, the position of the second sliding groove 11 changes, driving the slider 10 and the moving plate 153 to slide outward to the maximum position in the first sliding groove 9. During this process, the moving plate 153 no longer resists and centers the drone. The spring in the mounting block 151 adjusts the positions of the telescopic block 152 and the moving plate 153, and the telescopic plate 154 in the moving plate 153 expands and contracts synchronously, thereby increasing the landing area of the drone on the landing plate 13.

[0020] Embodiment 2

[0021] On the basis of Embodiment 1, please refer to Figures 1 to 11, electric push rods 2 are installed on both the front wall and the rear wall of the inner cavity of the box body 1. The output ends of the two electric push rods 2 are connected with a sliding cover 3 through bumps. The sliding cover 3 is slidably installed on the top of the box body 1. Bases 4 are installed on both the left and right sides of the bottom of the inner cavity of the box body 1. The bases 4 are connected with a fixing plate 6 through a balancing component 5. The balancing component 5 includes a first gear disk 51 and a rotating column 53. The first gear disk 51 is rotatably installed at the rear side of the base 4 through a motor. The rotating column 53 is rotatably installed in an opening on one side of the base 4 through a bearing. A second gear disk 52 is meshed with the outer side of the first gear disk 51. The second gear disk 52 is fixed to the outer side of the rear end of the rotating column 53. An adjusting rod 54 is fixed to the outer side of the front end of the rotating column 53. A third gear disk 55 is rotatably connected to the groove of the adjusting rod 54 through a motor. The first gear disk 51 and the third gear disk 55 are respectively arranged on a transverse axis and a longitudinal axis. The outer end of the third gear disk 55 is meshed with an installation gear disk 56. The installation gear disk 56 is rotatably installed in the groove of the adjusting rod 54 through protruding columns on both the left and right sides. A fixing plate 6 is installed at the upper end of the installation gear disk 56. A connecting column 7 is fixed to the upper end of the fixing plate 6. An installation plate 8 is fixed to the top of the connecting column 7. A plurality of first sliding grooves 9 are opened at the upper end of the installation plate 8. The inner side of the first sliding grooves 9 is slidably connected with a second sliding groove 11 through a slider 10. The second sliding groove 11 is opened at the top end of an adjusting plate 12. The adjusting plate 12 is rotatably installed outside the connecting column 7 through a bearing. The plurality of first sliding grooves 9 and the second sliding grooves 11 are respectively opened at equal angles on the installation plate 8 and the adjusting plate 12. The plurality of second sliding grooves 11 are designed as inclined arcs. The inclined arc design of the second sliding grooves 11 is used to adjust the position of the slider 10. An installation block 151 is fixed to the outer end of the slider 10. An expansion block 152 is slidably connected to the inner cavity of the installation block 151 through a spring. A moving plate 153 is fixedly connected to the inward side of the expansion block 152. The outer side of the stop plate 13 and the inward side of the moving plate 153 are both inclined. The inclined directions of the outer side of the stop plate 13 and the inward side of the moving plate 153 are opposite. An expansion plate 154 is slidably connected to the inner cavity of the moving plate 153 through a spring. The moving plate 153 is arc-shaped. The shape of the expansion plate 154 corresponds to the shape of the moving plate 153. The oil hydraulic component 14 is arranged between the electric push rod 2 and the adjusting plate 12. The oil hydraulic component 14 is used to adjust the position of the slider 10; When the installation carrier or the placement position of the box body 1 is tilted, after the biaxial inclination sensor in the connecting column 7 detects the inclination angle data, the motor connecting the first gear disk 51 and the third gear disk 55 is turned on through the controller, and a forward or reverse rotation corresponding to the inclination angle is performed, so that the first gear disk 51 drives the second gear disk 52, the rotating column 53 and the adjusting rod 54 to adjust the horizontal position in the transverse direction, and at the same time the third gear disk 55 drives the installation gear disk 56, the fixing plate 6, the connecting column 7 and the installation plate 8 to adjust the horizontal position in the longitudinal direction, so that the stop plate 13 always maintains a horizontal state.

[0022] Working principle: When using the intelligent integrated hangar that can accommodate two aircraft, first, the operator starts two electric push rods 2 through the controller, making the bumps at the output ends of the two electric push rods 2 move relatively, and pushing the two sliding covers 3 to slide to the left and right sides respectively at the upper end of the box body 1 to the maximum opening position. At the same time, when the bumps at the output ends of the electric push rods 2 move to the large position, they will first contact the first plug body 142 in the corresponding moving direction, making the first plug body 142 move inward in the first oil tank 141, and squeezing the oil in the inner cavity of the first oil tank 141 into the second oil tank 143 through the hose. The increase in the oil in the inner cavity of the second oil tank 143 drives the second plug body 144 to move outward in the second oil tank 143. When the second plug body 144 moves, it drives the adjusting plate 12 to rotate and adjust the position on the connecting column 7 through the adjusting ring 145. When the adjusting plate 12 rotates, the position of the second chute 11 changes, driving the slider 10 and the moving plate 153 to slide outward to the maximum position in the first chute 9, and during this process, the moving plate 153 no longer resists and centers the UAV; At the same time, when the moving plate 153 moves to the maximum position, the inclined surface at the inner end of the moving plate 153 coincides with the inclined surface on the outer side of the parking plate 13, and with the spring reset in the mounting block 151, it drives the telescopic block 152 and the moving plate 153 to move downward, making the inclined surface at the inner end of the moving plate 153 coincide with the inclined surface on the outer side of the parking plate 13 to the horizontal position. At the same time, during this process, the gap between the moving plates 153 increases during the outward movement, making the springs in the moving plates 153 gradually reset, and pushing the telescopic plate 154 to gradually move out to one side in the inner cavity of the moving plate 153. When the moving plate 153 moves to the maximum position, the synchronous deployment of the telescopic plate 154 is completed synchronously, thereby increasing the landing area of the UAV on the parking plate 13; When the UAV returns and lands on the parking plate 13, the two electric push rods 2 are started to reset through the controller. The first plug body 142 and the second plug body 144 are reset synchronously in the first oil tank 141 and the second oil tank 143, making the subsequent linkage parts operate in the opposite direction. When the moving plate 153 fits and moves inward at the upper end of the parking plate 13, the position of the UAV is gradually adjusted by centering and resisting, and the centering and resisting limit is completed after full reset; During the above process, when the installation carrier or placement position of the box body 1 is tilted, after the biaxial inclination sensor in the connecting column 7 detects the inclination angle data, it sends the data to the controller. The adjustment system in the controller turns on the motor connected to the first gear disk 51 and the third gear disk 55, and controls the motor connected to the first gear disk 51 and the third gear disk 55 to rotate forward or reverse at the corresponding inclination angle. When the motor connected to the third gear disk 55 rotates forward or reverse, the first gear disk 51 drives the second gear disk 52, the rotating column 53 and the adjusting rod 54 to adjust the horizontal position in the transverse direction. At the same time, when the motor connected to the third gear disk 55 rotates forward or reverse, it drives the mounting gear disk 56, the fixing plate 6, the connecting column 7 and the mounting plate 8 to adjust the horizontal position in the longitudinal direction, so that the stop plate 13 always remains in a horizontal state, providing a stable take-off and landing platform for the drone.

[0023] The content not described in detail in this specification belongs to the prior art well-known to those skilled in the art. In the description of the present invention, unless otherwise stated, the meaning of "a plurality of" is two or more; the terms "upper", "lower", "left", "right", "inner", "outer", "front end", "rear end", "head", "tail", etc. indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation of the present invention. In addition, the terms "first", "second", "third", etc. are only used for descriptive purposes and cannot be understood as indicating or implying relative importance. In the description of the present invention, it should be noted that unless otherwise clearly specified and limited, the terms "connected" and "connected" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0024] Although the present invention has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.

Claims

1. An intelligent integrated aircraft hangar capable of accommodating two aircraft, characterized in that: It includes a box body (1). Electric push rods (2) are installed on the front wall and the rear wall of the inner cavity of the box body (1). The output ends of the two electric push rods (2) are connected with a sliding cover (3) through bumps. The sliding cover (3) is slidably installed on the top of the box body (1). On the left and right sides of the bottom of the inner cavity of the box body (1), bases (4) are installed. The bases (4) are connected with a fixing plate (6) through a balance assembly (5). A connecting column (7) is fixed at the upper end of the fixing plate (6). An installation plate (8) is fixed at the top of the connecting column (7). A plurality of first chutes (9) are opened at the upper end of the installation plate (8). The inner side of the first chute (9) is slidably connected with a second chute (11) through a slider (10). The second chute (11) is opened at the top end of an adjusting plate (12). The adjusting plate (12) is rotatably installed on the outside of the connecting column (7) through a bearing. The outer end of the slider (10) is fixed with an installation block (151). An expansion block (152) is slidably connected in the inner cavity of the installation block (151) through a spring. The inward side of the expansion block (152) is fixedly connected with a moving plate (153). An expansion plate (154) is slidably connected in the inner cavity of the moving plate (153) through a spring; An oil liquid assembly (14) is arranged between the electric push rod (2) and the adjusting plate (12). The oil liquid assembly (14) is used for adjusting the position of the slider (10).

2. The intelligent integrated hangar capable of accommodating two aircraft according to claim 1, wherein: A plurality of the first chutes (9) and the second chutes (11) are respectively opened at equal angles on the installation plate (8) and the adjusting plate (12). A plurality of the second chutes (11) are designed as inclined arcs. The inclined arc design of the second chute (11) is used for adjusting the position of the slider (10).

3. The intelligent integrated hangar capable of accommodating two aircraft according to claim 2, characterized in that: The outer side of the stop plate (13) and the inward side of the moving plate (153) are both inclined designs. The inclined directions of the outer side of the stop plate (13) and the inward side of the moving plate (153) are opposite.

4. The intelligent integrated hangar capable of accommodating two aircraft according to claim 3, wherein: The moving plate (153) is of an arc design. The shape of the expansion plate (154) corresponds to the shape of the moving plate (153).

5. The intelligent integrated hangar capable of accommodating two aircraft according to claim 4, characterized in that: The balance assembly (5) includes a first gear disc (51) and a rotating column (53). The first gear disc (51) is rotatably installed at the rear side of the base (4) through a motor. The rotating column (53) is rotatably installed in a hole on one side of the base (4) through a bearing. A second gear disc (52) is meshed with the outside of the first gear disc (51). The second gear disc (52) is fixed on the outside of the rear end of the rotating column (53). An adjusting rod (54) is fixed on the outside of the front end of the rotating column (53). A third gear disc (55) is rotatably connected in the groove of the adjusting rod (54) through a motor. The outer end of the third gear disc (55) is meshed with an installation gear disc (56). The installation gear disc (56) is rotatably installed in the groove of the adjusting rod (54) through protruding columns on the left and right sides. The fixing plate (6) is installed at the upper end of the installation gear disc (56).

6. The intelligent integrated hangar capable of accommodating two aircrafts according to claim 5, characterized in that: The first gear disc (51) and the third gear disc (55) are respectively arranged on a transverse axis and a longitudinal axis.

7. An intelligent integrated hangar capable of accommodating two aircrafts according to claim 6, characterized in that: The oil component (14) includes two first oil tanks (141). The two first oil tanks (141) are respectively installed at the left-angle of the inner cavity rear wall of the box body (1) and the right-angle of the front arm. A first plug body (142) is slidably connected to the inner cavity of the first oil tank (141) through a spring. A second oil tank (143) is connected to the inner cavity of the first plug body (142) through a hose. A second plug body (144) is slidably connected to the inner cavity of the second oil tank (143) through a spring. The outer end of the second plug body (144) is connected to an adjusting ring (145) through a convex block. The adjusting ring (145) is installed at the bottom of the adjusting plate (12).

8. An intelligent integrated aircraft hangar capable of accommodating two aircrafts according to claim 7, characterized in that: The two first oil tanks (141) are arranged oppositely. The outer ends of the two first plug bodies (142) respectively correspond to the convex blocks at the output ends of the two electric push rods (2). The two electric push rods (2) are arranged oppositely. The second oil tank (143) is designed in an arc shape. The center of the arc of the second oil tank (143) corresponds to the center of the connecting column (7). A dual-axis inclination sensor is arranged in the connecting column (7).

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