CN112124179B - Can carry on large-scale unmanned aerial vehicle's cabin and vehicle - Google Patents
Can carry on large-scale unmanned aerial vehicle's cabin and vehicle Download PDFInfo
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- CN112124179B CN112124179B CN202011010095.7A CN202011010095A CN112124179B CN 112124179 B CN112124179 B CN 112124179B CN 202011010095 A CN202011010095 A CN 202011010095A CN 112124179 B CN112124179 B CN 112124179B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
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Abstract
The invention discloses a vehicle cabin capable of carrying a large unmanned aerial vehicle and a vehicle, which comprise a cabin body positioned in a vehicle body, an unmanned aerial vehicle carrying platform connected in a sliding fit manner in the cabin body and an opening positioned on the vehicle body and used for enabling the unmanned aerial vehicle carrying platform to extend out of the cabin body, wherein an opening and closing door is arranged at the opening, the ratio of the width of the opening to the width of the unmanned aerial vehicle carrying platform is M, M is less than 1, the ratio of the length of the cabin to the length of the unmanned aerial vehicle carrying platform is K, K is less than 1, the unmanned aerial vehicle carrying platform comprises at least two platform assemblies which are mutually hinged along the length direction of the cabin, each platform assembly comprises a main board and side boards hinged on two sides of the main board, the ratio of the width of the opening to the width of the main board is N, N is more than or equal to 1, the ratio of the length of the cabin to the length of the platform assembly is S, and S is more than or equal to 1. According to the invention, the large telescopic and foldable platform is integrated in the vehicle carrier, so that the problem that the unmanned aerial vehicle cannot be lifted normally on a soft and bumpy road surface without a road in the field is solved.
Description
Technical Field
The invention belongs to the technical field of special vehicles, and particularly discloses a vehicle cabin capable of carrying a large unmanned aerial vehicle and a vehicle.
Background
In China, military unmanned aerial vehicles mainly use large unmanned aerial vehicles to achieve strategic or battle-level fire attack; in actual combat, real-time information of a combat battlefield is often lacked, unmanned aerial vehicle reconnaissance and positioning technology cannot really fall into actual combat, a battlefield information support vehicle which can realize one-key retraction and release, remote battlefield information acquisition and in-vehicle information processing and transmission of an unmanned aerial vehicle reconnaissance and positioning system is urgently needed to be developed for improving the capacity of the army in acquiring battlefield information, and the sensing capacity of the army to real-time battlefield dynamics is improved. At present, domestic light high locomotive can use by all regions, but can use the plane less in the car, and the interior no big plane of car can't satisfy the condition that unmanned aerial vehicle safety goes up and down, for this reason, has developed a section of integrated electronic unmanned aerial vehicle telescopic platform in the car in the brand-new, realizes unmanned aerial vehicle and vehicle integration, breaks through the bottleneck that unmanned aerial vehicle does not have the way in the field, the unable normal flight in soft mud hole road surface.
The Chinese utility model CN210116652U discloses a planar take-off and landing platform for a vehicle-mounted unmanned aerial vehicle, which comprises an apron, a base and a buffer column, wherein the apron is in a flat plate shape and is provided with a locking component, two mutually perpendicular lock rod groups are arranged on the locking component, one lock rod group moves transversely, and the other lock rod group moves longitudinally to limit or unlock the unmanned aerial vehicle; the base is arranged below the parking apron and fixedly arranged on a top plate of the vehicle body; the number of the buffer columns is at least one, the buffer columns are arranged between the parking apron and the base and comprise telescopic sections, and springs are sleeved on the peripheries of the buffer columns. The utility model discloses a take-off and landing platform size is limited, can only be applicable to unmanned aerial vehicle's take-off and landing, is not suitable for large-scale unmanned aerial vehicle.
Disclosure of Invention
In order to solve the problem that a plane type take-off and landing platform of a vehicle-mounted unmanned aerial vehicle cannot be compatible with a large-size unmanned aerial vehicle platform in the background art, the invention provides a vehicle cabin and a vehicle capable of carrying the large-size unmanned aerial vehicle, and the problem that the unmanned aerial vehicle cannot normally lift on a soft mud-hollow road surface without roads in the field is solved by integrating a large telescopic and foldable platform in a vehicle.
The invention discloses a vehicle cabin capable of carrying a large unmanned aerial vehicle, which comprises a cabin body, an unmanned aerial vehicle carrying platform and an opening, wherein the cabin body is positioned in a vehicle body, the unmanned aerial vehicle carrying platform is connected in the cabin body in a sliding fit mode, the opening is positioned on the vehicle body and used for enabling the unmanned aerial vehicle carrying platform to extend out of the cabin body, an opening and closing door is arranged at the opening, the ratio of the width of the opening to the width of the unmanned aerial vehicle carrying platform is M, M is less than 1, the ratio of the length of the cabin to the length of the unmanned aerial vehicle carrying platform is K, K is less than 1, the unmanned aerial vehicle carrying platform comprises at least two platform assemblies which are mutually hinged along the length direction of the cabin body, each platform assembly comprises a main board and side boards hinged to two sides of the main board, the ratio of the width of the opening to the width of the main board is N, N is more than or equal to 1, the ratio of the length of the cabin body to the platform assembly is S, and S is more than or equal to 1.
In a preferred embodiment of the invention, a support rod assembly is arranged between the platform assembly which is connected with the cabin in a sliding fit manner and the vehicle body, one end of the support rod assembly is hinged with the bottom of the platform assembly, and the other end of the support rod assembly is detachably connected with the vehicle body.
In a preferred embodiment of the invention, a support rod assembly is arranged between two adjacent platform assemblies, one end of the support rod assembly is hinged with one platform assembly through a hinge arm, and the other end of the support rod assembly is detachably connected with the other platform assembly.
In a preferred embodiment of the present invention, a support rod assembly receiving cavity is disposed at the bottom end of the platform assembly in sliding fit connection with the cabin.
In a preferred embodiment of the present invention, a platform retraction slide rail for slidably guiding another platform assembly is disposed on an inner side wall of the support bar assembly receiving cavity, a support bar is fixedly disposed on another platform assembly slidably connected to the platform retraction slide rail, the platform retraction slide rail includes a first groove for receiving the support bar, a second groove for supporting and guiding another platform assembly, and a third groove for supporting another platform assembly in an extended state in cooperation with the support bar, the third groove includes a horizontal limiting portion and a hook portion, the hook portion is disposed obliquely above the horizontal limiting portion, and a first boss for cooperating with the horizontal limiting portion and a second boss for cooperating with the hook portion are disposed on the support bar.
In a preferred embodiment of the present invention, the opening is located at a rear end or a side end of the vehicle body.
In a preferred embodiment of the present invention, a linear module and a guide module are disposed in the cabin along a length direction of the cabin, and a moving end of the linear module and a moving end of the guide module are both fixedly connected to the platform assembly.
In a preferred embodiment of the present invention, the linear module includes a rack fixedly connected in the cabin and a gear fixedly connected to the platform assembly, the gear is in meshing transmission with the rack, and the gear is driven to rotate by a power source.
In a preferred embodiment of the present invention, the guide module comprises a pair of guide rail slider mechanisms symmetrically arranged with respect to the linear module.
In a preferred embodiment of the present invention, the main plate and the side plates are formed by splicing an aluminum alloy frame and an anti-slip pattern steel plate.
The invention also discloses a vehicle which comprises a vehicle cabin capable of carrying the large unmanned aerial vehicle.
The invention has the beneficial effects that: the invention has simple structure and high practicability, and the structural design of the folding platform assembly enables the vehicle to carry a large-size unmanned aerial vehicle lifting platform, thereby improving the universality of the vehicle and reducing the landing difficulty of a large-size unmanned aerial vehicle; furthermore, the platform assembly is simple in structural design and high in stability, and can be matched with the supporting rod assembly with adjustable length to support platforms of various sizes; furthermore, the supporting rod assembly accommodating cavity is integrated on the loading platform assembly, so that the supporting rod assembly is convenient to accommodate; furthermore, the full-automatic extension and recovery of the platform assembly are realized through the matching design of the linear module and the guide module.
Drawings
FIG. 1 is a structural diagram of a vehicle cabin capable of carrying a large unmanned aerial vehicle according to the invention when the vehicle cabin is unfolded;
FIG. 2 is a structural diagram of a vehicle cabin capable of carrying a large unmanned aerial vehicle according to the invention when the vehicle cabin is retracted;
FIG. 3 is a top view of a vehicle cabin capable of carrying a large unmanned aerial vehicle according to the present invention when deployed;
FIG. 4 is a sectional view A-A of FIG. 3;
FIG. 5 is an isometric view of a vehicle bay of the present invention that can carry a large unmanned aerial vehicle when deployed;
FIG. 6 is an enlarged view of part B of FIG. 5;
FIG. 7 is a schematic view of a retractable sliding rail of a platform capable of carrying a large unmanned aerial vehicle according to the present invention;
FIG. 8 is a schematic view of a support bar for carrying a large-sized unmanned aerial vehicle according to the present invention;
FIG. 9 is a schematic view of the invention when a large unmanned aerial vehicle can be carried;
FIG. 10 is a schematic view of an opening process of a large unmanned aerial vehicle according to the present invention;
FIG. 11 is a schematic view of an opening process of the invention for carrying a large-sized unmanned aerial vehicle;
fig. 12 is a schematic view of an unfolded state of the unmanned aerial vehicle according to the present invention;
wherein: 1-a primary platform assembly; 2-a secondary platform assembly; 3-auxiliary supporting plate; 4-a first-stage support rod assembly;
5-a secondary support rod assembly; 6-a cavity; 7-platform retraction slide rail; 8-a support ring; 9-a hinge; 10-a motor assembly; 11-a gear transmission mechanism; 12-a guide rail assembly; 13-rear door; 14-a wheel cover;
15-a controller assembly; 16-nested inner rail set; 17-outer rail set; 18-a base plate; 19-support bar.
Detailed Description
The technical solutions of the present invention (including the preferred ones) are further described in detail by way of fig. 1 to 6 and enumerating some alternative embodiments of the present invention. It is to be understood that the described embodiments are merely a few embodiments of the invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments of the present invention without any inventive step, are within the scope of the present invention.
The invention discloses a vehicle cabin capable of carrying a large unmanned aerial vehicle, which comprises a cabin body, an unmanned aerial vehicle carrying platform and an opening, wherein the cabin body is positioned in a vehicle body, the unmanned aerial vehicle carrying platform is connected in the cabin body in a sliding fit mode, the opening is positioned on the vehicle body and used for enabling the unmanned aerial vehicle carrying platform to extend out of the cabin body, an opening and closing door is arranged at the opening, the ratio of the width of the opening to the width of the unmanned aerial vehicle carrying platform is M, M is less than 1, the ratio of the length of the cabin to the length of the unmanned aerial vehicle carrying platform is K, K is less than 1, the unmanned aerial vehicle carrying platform comprises at least two platform assemblies which are mutually hinged along the length direction of the cabin body, each platform assembly comprises a main board and side boards hinged to two sides of the main board, the ratio of the width of the opening to the width of the main board is N, N is more than or equal to 1, the ratio of the length of the cabin body to the platform assembly is S, and S is more than or equal to 1. The platform assembly is unfolded and folded manually.
Preferably, a support rod assembly is arranged between the platform assembly which is connected with the cabin in a sliding fit manner and the vehicle body, one end of the support rod assembly is hinged with the bottom of the platform assembly, and the other end of the support rod assembly is detachably connected with the vehicle body.
Preferably, a support rod assembly is arranged between two adjacent platform assemblies, one end of each support rod assembly is hinged with one platform assembly through a hinge arm, and the other end of each support rod assembly is detachably connected with the other platform assembly.
Preferably, the bottom end of the platform assembly in sliding fit connection with the cabin is provided with a support rod assembly receiving cavity.
Preferably, be provided with the platform shrink slide rail that is used for another platform assembly of sliding guide on the inside wall of cavity is accomodate to the bracing piece assembly, sliding fit connects and fixes being provided with the support bar on another platform assembly on the platform shrink slide rail, platform shrink slide rail is including the first groove that is used for accomodating the support bar, be used for supporting the third groove that leads another platform assembly complex second groove and be used for supporting another platform assembly that is in the development attitude with the support bar cooperation, the third groove includes horizontal spacing portion and couple portion, the couple position is in horizontal spacing portion top to one side, be provided with on the support bar be used for with horizontal spacing portion complex first boss and with couple portion complex second boss.
Preferably, the opening is located at a rear end or a side end of the vehicle body.
Preferably, be provided with the straight line module and the direction module of arranging along its length direction in the cabin, the removal end of straight line module with the removal end of direction module all with platform assembly rigid coupling.
Preferably, the linear module comprises a rack fixedly connected in the cabin and a gear fixedly connected on the platform assembly, the gear is in meshing transmission with the rack, and the gear is driven to rotate by a power source.
Preferably, the guide module comprises a pair of guide rail sliding block mechanisms symmetrically arranged corresponding to the linear module.
Preferably, the main plate and the side plates are formed by splicing an aluminum alloy frame and an anti-skid pattern steel plate.
The invention also discloses a vehicle which comprises a vehicle cabin capable of carrying the large unmanned aerial vehicle.
The operation of the invention will be further explained with reference to an embodiment of the drawings attached to the description,
the invention comprises a base assembly positioned in a cabin of a vehicle body, wherein the base assembly comprises a guide rail 12, a gear transmission mechanism 11 and a bottom plate 18 which are connected and fixed in a carriage through a high-strength bolt after being machined; the primary platform assembly 1 and the secondary platform assembly 2 comprise aluminum alloy sections, hinges 9, primary supporting rod assemblies 4 and secondary supporting rod assemblies 5, and anti-skid pattern steel plates are covered on the surfaces of the primary supporting rod assemblies and the secondary supporting rod assemblies to form a frame structure, so that the structure is light in weight and high in strength; cavities 6 are arranged in the primary platform assembly 1 and the secondary platform assembly 2 and used for receiving and releasing the auxiliary supporting plates 3, the primary supporting rod assembly 4 and the secondary supporting rod assembly 5; the auxiliary supporting plate 3 is connected with the main platform through a hinge, the first-stage supporting rod assembly 4 and the second-stage supporting rod assembly 5 are made of stainless steel, and the auxiliary supporting plate is not prone to rusting after being used for a long time.
Two supporting rod assembly accommodating cavities 6 are arranged below a primary platform assembly 1, 1 platform contraction sliding rail 7 is respectively arranged on the inner walls of the two supporting rod assembly accommodating cavities 6, a secondary platform assembly 2 is integrally matched on the platform contraction sliding rail 7 in a sliding mode and can contract or extend along the platform contraction sliding rail 7, in order to ensure that the primary platform assembly 1 and the secondary platform assembly 2 are positioned in the same plane in an unfolded state, a supporting strip 19 is fixedly arranged on the secondary platform assembly 2, and the platform contraction sliding rail 7 is designed into three sections, which are respectively: the platform contraction sliding rail comprises a first groove 7.1 for accommodating a supporting strip, a second groove 7.2 for supporting and guiding another platform assembly to be matched with and a third groove 7.3 for supporting another platform assembly in a unfolding state in a matching way with the supporting strip, the width of the first groove 7.1 corresponds to the width of the supporting strip 19, the width of the second groove 7.2 corresponds to the thickness of the second-stage platform assembly 2, an arc top transition section is arranged between the second groove 7.2 and the third groove 7.3, so that the height of the second-stage platform assembly 2 can be conveniently adjusted, the width of the third groove 7.3 is larger than the thickness of the second-stage platform assembly 2 (namely larger than the width of the second groove 7.2), the third groove 7.3 comprises a horizontal limiting part 7.4 and a hook part 7.5, the hook part 7.5 is positioned above the horizontal limiting part 7.4, a first boss 19.1 for being matched with the horizontal limiting part 7.4 and a second boss 19.2 matched with the hook part 7.5 are arranged on the supporting strip 19, the support bars 19 are matched with the horizontal limiting parts 7.4 and the hook parts 7.5 by manual adjustment.
The primary platform assembly 1 and the secondary platform assembly 2 both comprise a main plate and side plates, the side plates are symmetrically hinged to two sides of the main plate, and foldable triangular support plates matched with the main plate are hinged to the side plates.
The invention adopts a motor 10 for driving, the motor is arranged below the right side of a primary platform assembly 1, a motor gear and a rack on a base are mutually meshed to form a gear transmission mechanism 11, so that the primary platform assembly 1 is driven to extend along the direction of a guide rail 12, a secondary platform assembly 2 below the primary platform assembly 1 is unfolded through a platform contraction slide rail 7, a support rod is taken out from a cavity 6, a primary support rod assembly 4 is supported on a support ring 8 on the rear periphery of the whole vehicle, one end of a secondary support rod assembly 5 is connected with a hinge 9 fixed in the cavity 6 and is convenient to store in the cavity 9, and the other end of the secondary support rod assembly 2 is supported on the secondary platform assembly, so that the purposes of integrating a large platform in the vehicle and freely stretching are achieved.
Claims (7)
1. The utility model provides a can carry on large-scale unmanned aerial vehicle's cabin, connects in the unmanned aerial vehicle microscope carrier in the cabin and is located the automobile body and supply the unmanned aerial vehicle microscope carrier to stretch out the outdoor uncovered of cabin, uncovered department is provided with opening and closing door, its characterized in that including the cabin that is located the automobile body: the ratio of the width of the opening to the width of the unmanned aerial vehicle carrying platform is M, M is less than 1, the ratio of the length of the cabin to the length of the unmanned aerial vehicle carrying platform is K, K is less than 1, the unmanned aerial vehicle carrying platform comprises at least two platform assemblies which are mutually hinged along the length direction of the cabin, each platform assembly comprises a main board and side boards which are hinged to two sides of the main board, the ratio of the width of the opening to the width of the main board is N, N is more than or equal to 1, the ratio of the length of the cabin to the length of the platform assemblies is S, and S is more than or equal to 1; a support rod assembly is arranged between every two adjacent platform assemblies, one end of each support rod assembly is hinged with the primary platform assembly (1) through a hinge arm, and the other end of each support rod assembly is detachably connected with the secondary platform assembly (2); a supporting rod assembly accommodating cavity is arranged at the bottom end of the primary platform assembly (1) in sliding fit connection with the cabin; the utility model discloses a support bar assembly, including bracing piece assembly accomodate cavity, be provided with the platform shrink slide rail that is used for sliding guide secondary platform assembly (2) on the inside wall of bracing piece assembly accomodate cavity, sliding fit connects and fixedly is provided with support bar (19) on secondary platform assembly (2) on the shrink slide rail of platform, platform shrink slide rail is including first groove (7.1) that are used for accomodating support bar (19), second groove (7.2) that are used for supporting guide secondary platform assembly (2) and be used for supporting third groove (7.3) that are in the secondary platform assembly (2) of expansion state with the support bar cooperation, the groove width of first groove (7.1) is corresponding with the width of support bar (19), the groove width of second groove (7.2) is corresponding with the thickness of secondary platform assembly (2), be provided with the arc top changeover portion between second groove (7.2) and third groove (7.3), make things convenient for the adjustment of secondary platform assembly (2) height, the width of third groove (7.3) is greater than the thickness of secondary platform assembly (2), the groove width of the third groove (7.3) is larger than that of the second groove (7.2), the third groove comprises a horizontal limiting part (7.4) and a hook part (7.5), the hook part (7.5) is located obliquely above the horizontal limiting part (7.4), and a first boss (19.1) matched with the horizontal limiting part (7.4) and a second boss (19.2) matched with the hook part (7.5) are arranged on the supporting strip (19).
2. The vehicle cabin capable of carrying the large unmanned aerial vehicle according to claim 1, characterized in that: and a support rod assembly is arranged between the platform assembly which is connected with the cabin in a sliding fit manner and the vehicle body, one end of the support rod assembly is hinged with the bottom of the platform assembly, and the other end of the support rod assembly is detachably connected with the vehicle body.
3. The vehicle cabin capable of carrying the large unmanned aerial vehicle according to claim 1, characterized in that: the opening is positioned at the rear end or the side end of the vehicle body.
4. The vehicle cabin capable of carrying the large unmanned aerial vehicle according to claim 1, characterized in that: the cabin is internally provided with a linear module and a guide module which are arranged along the length direction of the linear module, and the moving end of the linear module and the moving end of the guide module are fixedly connected with the platform assembly.
5. The cabin capable of carrying a large unmanned aerial vehicle according to claim 4, characterized in that: the linear module comprises a rack fixedly connected in the cabin and a gear fixedly connected on the platform assembly, the gear is in meshed transmission with the rack, and the gear is driven to rotate by a power source.
6. The cabin capable of carrying a large unmanned aerial vehicle according to claim 4, characterized in that: the guide module comprises a pair of guide rail sliding block mechanisms which are symmetrically arranged corresponding to the linear module.
7. A vehicle, characterized in that: comprising a cabin according to any one of claims 1-6, on which a large drone can be carried.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202011010095.7A CN112124179B (en) | 2020-09-23 | 2020-09-23 | Can carry on large-scale unmanned aerial vehicle's cabin and vehicle |
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| CN202011010095.7A CN112124179B (en) | 2020-09-23 | 2020-09-23 | Can carry on large-scale unmanned aerial vehicle's cabin and vehicle |
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| CN112124179B true CN112124179B (en) | 2022-01-25 |
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| CN113232576B (en) * | 2021-05-19 | 2022-08-05 | 南京航空航天大学 | Splicing two-section folding vehicle-mounted unfolding platform and operation method |
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