Hangar and Aircraft Kit
By using drive devices and clamping equipment in the hangar, the problems of low space utilization and bumping and scratching during the aircraft parking are solved, and the stable storage of the aircraft and the improvement of space utilization are achieved.
Patent Information
- Application Number
- CN202110170097.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2021-02-07
- Publication Date
- 2025-07-22
- Estimated Expiration
- 2041-02-07
AI Technical Summary
When the aircraft is parked in the hangar, the deployed area of the fixed wings and rotors is large, resulting in low space utilization and is prone to bumps and scratches with the hangar during movement.
The first driving device and the second driving device are respectively connected to the shutdown table, and the first driving device drives the shutdown table into and out of the box, and the second driving device drives the shutdown table to flip, and clamp the aircraft with the clamping equipment to achieve the storage of the aircraft and the improvement of space utilization.
It improves the space utilization inside the hangar, reduces the collision and scratch between the aircraft and the hangar, and realizes the stable storage of the aircraft.
Smart Images

Figure CN112829958B_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of aircraft, and in particular to a hangar and an aircraft kit. Background Art
[0002] When an aircraft lands and parks, it needs to be moved inside the hangar. When the aircraft is stored in the hangar, due to the large deployment area of the fixed wings and rotors, the utilization rate of the internal space of the hangar is low. In addition, during the process of moving the aircraft inside the hangar, the aircraft and the hangar are prone to bumping and scratching. Summary of the Invention
[0003] The purpose of the present invention is to provide a hangar and an aircraft kit, which can park and store the aircraft with a high space utilization rate.
[0004] In a first aspect, the hangar provided by the present invention includes: a box body, a parking platform, a first driving device, and a second driving device;
[0005] The first driving device and the second driving device are respectively connected to the parking platform;
[0006] The first driving device is used to drive the parking platform to enter and exit the box body;
[0007] The second driving device is used to drive the parking platform to flip.
[0008] Combined with the first aspect, the present invention provides a first possible implementation manner of the first aspect, wherein the first driving device includes a telescopic device, the fixed end of the telescopic device is connected to the box body, the movable end of the telescopic device is connected to the parking platform, and the telescopic device is used to drive the parking platform to move along the x-axis.
[0009] Combined with the first possible implementation manner of the first aspect, the present invention provides a second possible implementation manner of the first aspect, wherein the second driving device includes a flipping driving member, the fixed end of the flipping driving member is connected to the movable end of the telescopic device, the movable end of the flipping driving member is connected to the parking platform, and the flipping driving member is used to drive the parking platform to flip around the x-axis.
[0010] Combined with the first aspect, the present invention provides a third possible implementation manner of the first aspect, wherein the first driving device includes a first rotation driving member, the first rotation driving member is installed on the box body, and the first rotation driving member is in transmission connection with the parking platform, and the first rotation driving member is used to drive the parking platform to rotate around the y-axis.
[0011] Combined with the third possible implementation manner of the first aspect, the present invention provides a fourth possible implementation manner of the first aspect, wherein the second driving device includes a second rotary driving member, a fixed end of the second rotary driving member is connected to a movable end of the first rotary driving member, and a movable end of the second rotary driving member is connected to the parking platform;
[0012] A rotating shaft of the first rotary driving member is perpendicular to a rotating shaft of the second rotary driving member.
[0013] Combined with the third possible implementation manner of the first aspect, the present invention provides a fifth possible implementation manner of the first aspect, wherein the rotating shaft of the first rotary driving member is located at the top of a side opening of the box body.
[0014] Combined with the first aspect, the present invention provides a sixth possible implementation manner of the first aspect, wherein the parking platform includes a clamping device for clamping an aircraft.
[0015] Combined with the sixth possible implementation manner of the first aspect, the present invention provides a seventh possible implementation manner of the first aspect, wherein the clamping device includes: a bearing ring, a clamping driving device, and a plurality of clamping jaws;
[0016] The plurality of clamping jaws are respectively mounted on the bearing ring, and the plurality of clamping jaws enclose a clamping area;
[0017] The clamping driving device is in transmission connection with the plurality of clamping jaws.
[0018] Combined with the seventh possible implementation manner of the first aspect, the present invention provides an eighth possible implementation manner of the first aspect, wherein the clamping driving device includes a driving ring coaxial with the bearing ring, and the plurality of clamping jaws are respectively slidably connected between the bearing ring and the driving ring;
[0019] A sliding member is connected to the clamping jaw, and a sliding groove is provided on the driving ring, and the sliding member is slidably connected in the sliding groove.
[0020] In a second aspect, an aircraft kit provided by the present invention includes: an aircraft and a hangar provided by the first aspect, and the aircraft is parked on the parking platform.
[0021] The embodiments of the present invention bring the following beneficial effects: By using the first driving device and the second driving device to be respectively connected to the parking platform, the aircraft can be parked on the parking platform. By driving the parking platform to enter and exit the box body through the first driving device, the aircraft can be stored. Moreover, by driving the parking platform to flip through the second driving device, the space utilization rate inside the hangar can be improved.
[0022] To make the above objects, features, and advantages of the present invention more apparent and understandable, the following provides preferred embodiments in conjunction with the accompanying drawings and describes them in detail as follows. Description of the Drawings
[0023] In order to more clearly illustrate the specific embodiments of the present invention or the technical solutions in related technologies, the following will briefly introduce the drawings required for use in the description of the specific embodiments or related technologies. Obviously, the drawings in the following description are some embodiments of the present invention. For those of ordinary skill in the art, without creative efforts, other drawings can also be obtained based on these drawings.
[0024] Figure 1 Schematic diagram of the first hangar and the aircraft provided by the embodiment of the present invention;
[0025] Figure 2 Cross-sectional view of the first hangar and the aircraft provided by the embodiment of the present invention;
[0026] Figure 3 Schematic diagram of the second hangar provided by the embodiment of the present invention;
[0027] Figure 4 Schematic diagram of the parking platform of the hangar provided by the embodiment of the present invention.
[0028] Reference Signs: 100 - box body; 101 - side opening; 200 - parking platform; 210 - bearing ring; 220 - clamping drive device; 221 - drive ring; 222 - driving gear; 230 - clamping jaw; 240 - sliding member; 300 - first drive device; 310 - telescopic device; 320 - first rotary drive member; 400 - second drive device; 410 - flipping drive member; 420 - second rotary drive member; 500 - aircraft. Detailed Embodiments
[0029] The following will clearly and completely describe the technical solutions of the present invention in conjunction with the drawings. Obviously, the described embodiments are some embodiments of the present invention, rather than all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts fall within the scope of protection of the present invention.
[0030] In the description of the present invention, it should be noted that the orientation or positional relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings. It is 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 construed as a limitation on the present invention. In addition, the terms "first", "second", "third" are only used for descriptive purposes and cannot be construed as indicating or implying relative importance. For the physical quantities in the formulas, if there is no separate annotation, they should be understood as the basic quantities of the basic units of the International System of Units, or the derived quantities derived from the basic quantities through mathematical operations such as multiplication, division, differentiation, or integration.
[0031] In the description of the present invention, it should be noted that unless otherwise clearly specified and defined, the terms "installed", "connected", "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, and it can be the communication inside two elements. 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.
[0032] Embodiment 1
[0033] As Figure 1 and Figure 3 shown, the hangar provided by the embodiment of the present invention includes: a box body 100, a parking platform 200, a first driving device 300, and a second driving device 400;
[0034] The first driving device 300 and the second driving device 400 are respectively connected to the parking platform 200;
[0035] The first driving device 300 is used to drive the parking platform 200 to enter and exit the box body 100;
[0036] The second driving device 400 is used to drive the parking platform 200 to flip.
[0037] Specifically, the first driving device 300 can drive the parking platform 200 to enter and exit the box body 100 in a telescopic or rotating manner. When the parking platform 200 is outside the box body 100, the second driving device 400 drives the parking platform 200 to flip; when the parking platform 200 flips to the horizontal state, the parking platform 200 can be used for the takeoff and landing of the aircraft 500; when the parking platform 200 flips to the vertical state, the first driving device 300 can drive the parking platform 200 into the interior of the aircraft 500, and the aircraft 500 can be stored in a state where the occupied space is relatively small, improving the space utilization rate inside the hangar.
[0038] In the first hangar provided by the embodiments of the present invention, as Figure 1 and Figure 2 shown, the first driving device 300 includes a telescopic device 310. The fixed end of the telescopic device 310 is connected to the box body 100, and the movable end of the telescopic device 310 is connected to the parking platform 200. The telescopic device 310 is used to drive the parking platform 200 to move along the x-axis.
[0039] Specifically, the telescopic device 310 can adopt a telescopic cylinder or an electric telescopic rod. In addition, the telescopic device 310 can also include a telescopic bracket, which is slidably connected to the slide rail inside the box body 100. The telescopic bracket is driven to rotate by a motor through a gear rack, or a telescopic cylinder is used to drive the telescopic bracket to move along the x-axis, so as to drive the parking platform 200 to enter and exit the box body 100.
[0040] Furthermore, the second driving device 400 includes a flipping driving member 410. The fixed end of the flipping driving member 410 is connected to the movable end of the telescopic device 310, and the movable end of the flipping driving member 410 is connected to the parking platform 200. The flipping driving member 410 is used to drive the parking platform 200 to flip around the x-axis.
[0041] Specifically, the flipping driving member 410 can adopt a rotary power device such as a stepping motor or a servo motor. The parking platform 200 is driven by the flipping driving member 410 to flip around the x-axis, so that the parking platform 200 can be switched between a horizontal state and an upright state. When the parking platform 200 flips to the horizontal state, the parking platform 200 can be used for the vertical takeoff and landing of the aircraft 500; when the parking platform 200 flips to the upright state, the telescopic device 310 can drive the parking platform 200 into the box body 100.
[0042] In the second hangar provided by the embodiments of the present invention, as Figure 3 shown, the first driving device 300 includes a first rotary driving member 320. The first rotary driving member 320 is installed on the box body 100, and the first rotary driving member 320 is in transmission connection with the parking platform 200. The first rotary driving member 320 is used to drive the parking platform 200 to rotate around the y-axis.
[0043] Specifically, the rotating shaft of the first rotary driving member 320 is located inside the box body 100 close to the side opening 101. The rotating shaft of the first rotary driving member 320 is parallel to the y-axis direction. The parking platform 200 rotates around the rotating shaft of the first rotary driving member 320, so as to make the parking platform 200 enter and exit the box body 100.
[0044] Furthermore, the second driving device 400 includes a second rotary driving member 420. The fixed end of the second rotary driving member 420 is connected to the movable end of the first rotary driving member 320, and the movable end of the second rotary driving member 420 is connected to the parking platform 200; the rotating shaft of the first rotary driving member 320 is perpendicular to the rotating shaft of the second rotary driving member 420.
[0045] Specifically, the first rotation driving member 320 drives the parking platform 200 to rotate around the axis of the first rotation driving member 320, so that the parking platform 200 is moved to the outside of the box body 100, or the parking platform 200 is moved to the inside of the box body 100. When the parking platform 200 is moved to the outside of the box body 100 and the axis of the second rotation driving member 420 extends in the horizontal direction, the second rotation driving member 420 drives the parking platform 200 to flip around the axis of the second rotation driving member 420, so that the bearing surface of the parking platform 200 can be switched between the horizontal state and the vertical state.
[0046] Furthermore, the axis of the first rotation driving member 320 is located at the top of the side opening 101 of the box body 100. When the first rotation driving member 320 drives the parking platform 200 to move outside the box body 100 around the axis of the first rotation driving member 320, the axis of the second rotation driving member 420 is located above the side opening 101. Thus, when the parking platform 200 flips around the axis of the second rotation driving member 420 to the horizontal state, the bearing surface of the parking platform 200 is higher than the side opening 101, which can prevent the unmanned aerial vehicle from colliding or scratching with the box body 100 during the process of landing on the parking platform 200.
[0047] As Figure 1 、 Figure 2 、 Figure 3 and Figure 4 shown, the parking platform 200 includes a clamping device. By clamping the aircraft 500 with the clamping device, the stability of the aircraft 500 can be ensured during the flipping process of the aircraft 500.
[0048] Furthermore, the clamping device includes: a bearing ring 210, a clamping driving device 220 and a plurality of clamping jaws 230;
[0049] The plurality of clamping jaws 230 are respectively installed on the bearing ring 210, and the plurality of clamping jaws 230 enclose to form a clamping area;
[0050] The clamping driving device 220 is in transmission connection with the plurality of clamping jaws 230.
[0051] Specifically, the plurality of clamping jaws 230 are respectively slidably connected to the bearing ring 210. By driving the plurality of clamping jaws 230 with the clamping driving device 220, the opening degree of the clamping area is further adjusted. The clamped member installed at the bottom of the aircraft 500 can be inserted into the clamping area, and the clamped member is jointly clamped by the plurality of clamping jaws 230, so as to fix the aircraft 500.
[0052] Furthermore, the clamping driving device 220 includes a driving ring 221. The driving ring 221 is coaxial with the bearing ring 210, and the plurality of clamping jaws 230 are respectively slidably connected between the bearing ring 210 and the driving ring 221;
[0053] A sliding member 240 is connected to the jaw 230. The driving ring 221 is provided with a sliding groove, and the sliding member 240 is slidably connected in the sliding groove. Among them, the clamping driving device 220 further includes a motor and a driving gear 222. The driving gear 222 is in transmission connection with the motor, and drives the driving ring 221 to rotate around its own axis by meshing the driving gear 222 with the toothed ring connected to the driving ring 221.
[0054] Specifically, the extending direction of the sliding groove has an acute angle with the radial direction of the driving ring 221. When the driving ring 221 rotates around its own axis, the sliding member 240 slides along the sliding groove, and the jaw 230 moves synchronously with the sliding member 240, so as to realize the adjustment of the opening degree of the clamping area between the plurality of jaws 230.
[0055] It should be noted that the jaw 230 is provided with a limiting side surface, and any one jaw 230 is slidably connected between the limiting side surface of another jaw 230 and the inner groove side wall surface of the bearing ring 210, so as to ensure that the jaw 230 can slide stably.
[0056] Embodiment 2
[0057] As Figure 1 、 Figure 2 and Figure 3 shown, the aircraft kit provided by the embodiment of the present invention includes: an aircraft 500 and the hangar provided by Embodiment 1. The aircraft 500 is parked on the parking platform 200.
[0058] In the embodiment of the present invention, the aircraft kit has the technical effect of the hangar. The aircraft 500 can be parked on the parking platform 200. The first driving device 300 can drive the aircraft 500 to enter and exit the box body 100, and the second driving device 400 drives the parking platform 200 to drive the aircraft 500 to flip, so that the aircraft 500 can be stored in the box body 100 in a state of occupying less space, improving the space utilization rate of the hangar.
[0059] Finally, it should be noted that: the above embodiments are only used to illustrate the technical solutions of the present invention, not to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that: they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements on some or all of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the scope of the technical solutions of the embodiments of the present invention.
Claims
1. An aircraft hangar, characterized in that, Comprising: A box body (100), a parking platform (200), a first driving device (300) and a second driving device (400); The first driving device (300) is connected to the parking platform (200) through the second driving device (400); The first driving device (300) is used to drive the parking platform (200) to enter and exit the box body (100); The second driving device (400) is used to drive the parking platform (200) to flip; The first driving device (300) includes a telescopic device (310), the fixed end of the telescopic device (310) is connected to the box body (100), the movable end of the telescopic device (310) is connected to the parking platform (200) through the second driving device (400), and the telescopic device (310) is used to drive the parking platform (200) to move along the x-axis; The second driving device (400) includes a flipping driving member (410), the fixed end of the flipping driving member (410) is connected to the movable end of the telescopic device (310), the movable end of the flipping driving member (410) is connected to the parking platform (200), and the flipping driving member (410) is used to drive the parking platform (200) to flip around the x-axis. When the parking platform (200) flips to the upright state, the telescopic device (310) can drive the parking platform (200) into the interior of the box body (100).
2. The hangar according to claim 1, wherein The parking platform (200) includes a clamping device, and the clamping device is used to clamp an aircraft (500).
3. The hangar according to claim 2, characterized in that, The clamping device includes: a bearing ring (210), a clamping driving device (220) and a plurality of clamping jaws (230); A plurality of the clamping jaws (230) are respectively installed on the bearing ring (210), and a plurality of the clamping jaws (230) enclose to form a clamping area; The clamping driving device (220) is in transmission connection with a plurality of the clamping jaws (230).
4. The hangar according to claim 3, characterized in that, The clamping driving device (220) includes a driving ring (221), the driving ring (221) is coaxial with the bearing ring (210), and a plurality of the clamping jaws (230) are respectively slidably connected between the bearing ring (210) and the driving ring (221); A sliding member (240) is connected to the clamping jaw (230), and the driving ring (221) is provided with a sliding groove, and the sliding member (240) is slidably connected in the sliding groove.
5. An aircraft hangar, characterized in that, Comprising: A box body (100), a parking platform (200), a first driving device (300) and a second driving device (400); The first driving device (300) is connected to the parking platform (200) through the second driving device (400); The first driving device (300) is used to drive the parking platform (200) to enter and exit the box body (100); The second driving device (400) is used to drive the parking platform (200) to flip; The first driving device (300) includes a first rotary driving member (320). The first rotary driving member (320) is installed on the box body (100), and the first rotary driving member (320) is in transmission connection with the parking platform (200) through the second driving device (400). The first rotary driving member (320) is used to drive the parking platform (200) to rotate around the y-axis; The second driving device (400) includes a second rotary driving member (420). The fixed end of the second rotary driving member (420) is connected to the movable end of the first rotary driving member (320), and the movable end of the second rotary driving member (420) is connected to the parking platform (200); The axis of rotation of the first rotary driving member (320) is perpendicular to the axis of rotation of the second rotary driving member (420). The second rotary driving member (420) drives the parking platform (200) to flip around the axis of rotation of the second rotary driving member (420), so that the bearing surface of the parking platform (200) switches between a horizontal state and an upright state; when the parking platform (200) flips to the upright state, the first rotary driving member (320) can drive the parking platform (200) into the interior of the box body (100).
6. The hangar according to claim 5, wherein, The axis of rotation of the first rotary driving member (320) is located at the top of the side opening (101) of the box body (100).
7. The hangar according to claim 5, characterized in that, The parking platform (200) includes a clamping device, and the clamping device is used to clamp the aircraft (500).
8. The hangar according to claim 7, characterized in that, The clamping device includes: a bearing ring (210), a clamping driving device (220) and a plurality of clamping jaws (230); A plurality of the clamping jaws (230) are respectively installed on the bearing ring (210), and a plurality of the clamping jaws (230) enclose a clamping area; The clamping driving device (220) is in transmission connection with a plurality of the clamping jaws (230).
9. The hangar according to claim 8, wherein, The clamping driving device (220) includes a driving ring (221). The driving ring (221) is coaxial with the bearing ring (210), and a plurality of the clamping jaws (230) are respectively slidably connected between the bearing ring (210) and the driving ring (221); A sliding member (240) is connected to the clamping jaw (230), and the driving ring (221) is provided with a sliding groove, and the sliding member (240) is slidably connected in the sliding groove.
10. An aircraft kit, characterized in that, Including: An aircraft (500) and the hangar according to any one of claims 1-9, and the aircraft (500) is parked on the parking platform (200).
Citation Information
Patent Citations
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