Sliding plate guiding type flight carrying device

Abstract

The utility model discloses a sliding plate guiding type flight carrying device which comprises a guiding device and a machine body erected on the guiding device and provided with a propelling device. A supporting plate is arranged at the bottom of the machine body; an elastic guide plate is arranged at the bottom of the supporting plate; a plurality of guide columns are arranged along a set running path at equal column distance intervals; a square penetrating opening is formed in the position, close to the top, of the guide column in the radial direction, a square notch is formed between the top face of the square penetrating opening and the top face of the guide column, and the width of the penetrating opening is larger than that of the notch. The thickness of the supporting plate is matched with the width of the notch, the thickness of the penetrating opening is matched with the thickness of the guide plate, and the thickness of the guide plate is larger than the width of the notch. The support plate is higher than the notch, and the guide plate is lower than the penetrating opening; the total height of the supporting plate and the guide plate is larger than that of the notch and the penetrating opening. The guide plates are arranged in the corresponding penetrating openings in a penetrating mode, and the supporting plates are arranged in the corresponding notches in a penetrating mode. And the structure is relatively simple, the laying cost is relatively low, and the using effect is more ideal.

Description

Technical Field

[0001] This utility model belongs to the technical field of guided flight carrier devices, and particularly relates to a skateboard guided flight carrier device. Background Technology

[0002] Guided flight vehicles generally include track-guided flight vehicles and cableway-guided flight vehicles. The movement path of the vehicle is limited by the guidance of a track or cableway, and the vehicle is propelled by a "flight" method similar to that of an airplane. It combines the advantages of existing rail-guided electric transportation vehicles and airplanes, and has the advantages of occupying less land resources, high speed, energy saving, simple structure, low manufacturing and transportation costs, and high safety.

[0003] For example, Chinese patent publication number CN207466650U, entitled "A Self-Balancing Cableway Flight Transport Device," discloses a self-balancing cableway flight transport device, such as... Figure 1 As shown, the system includes a cableway 1 mounted on a support pole 3, a machine body 5 movably suspended from the cableway 1 via a coupling device, and its propulsion device. Each coupling device includes upper and lower rollers 2, a hanging plate sandwiched between the rollers 2, and a suspension block. Hanging rods are respectively provided on the left and right sides of the top surface of the suspension block. The cableway 1 is sandwiched between the upper and lower rollers 2. The propulsion device includes a ducted fan 4 driven by a balance control device. The upper end of the hanging rod is connected to the corresponding inner side of the rear of the ducted fan 4. The balance control device includes a base frame, a balance block, a top pressure rod, a bottom pressure rod, and a middle frame. The horizontal block on the top pressure rod is movably and separably pressed against the top of the corresponding bottom pressure rod. The horizontal block on the bottom pressure rod is movably and separably pressed against the top surface of the middle frame. The left and right sides of the top surface of the balance block are connected to the corresponding front parts of the ducted fan 4 via corresponding ball joints. It can automatically adjust height and tilt, and compensate for centrifugal deflection during turns, resulting in higher stability.

[0004] While guided flight vehicles using this technology can certainly be used, they require relatively complex cableways and attachment devices, resulting in higher installation costs and less than ideal performance. Utility Model Content

[0005] To overcome the shortcomings of existing technologies, this utility model provides a skateboard-guided flight carrier device with a relatively simple structure, relatively low installation cost, and more ideal performance.

[0006] The technical solution adopted by this utility model to achieve the above-mentioned technical objectives is as follows: A skateboard-guided flight carrier device includes a guidance device and a body mounted on the guidance device and equipped with a propulsion device; a support plate is provided at the bottom of the body, and an elastic guide plate is provided at the bottom of the support plate; multiple guide columns are arranged at equal intervals along a set running path; a square through-hole is radially opened near the top of the guide column, and a square notch is opened between the top surface of the square through-hole and the top surface of the guide column, the width of the through-hole being greater than the width of the notch; the thickness of the support plate is...

[0007] The width of the notch is matched with the thickness of the through-hole and the thickness of the guide plate. The thickness of the guide plate is greater than the width of the notch. The height of the support plate is greater than the height of the notch and the height of the guide plate is less than the height of the through-hole. The total height of the support plate and the guide plate is greater than the total height of the notch and the through-hole. The guide plate is inserted into the corresponding through-hole and the support plate is inserted into the corresponding notch.

[0008] The fuselage is shaped like a high-wing fixed-wing aircraft. The fuselage as a whole has a roly-poly structure with a low center of gravity, and the fulcrum of the roly-poly structure is located at the bottom of the guide plate.

[0009] Both wings of the aforementioned high-wing are angled downwards.

[0010] The propulsion device is a ducted fan, which is located at the tail of the machine.

[0011] The inlet and outlet of the aforementioned opening are both provided with a chamfered edge B to facilitate the introduction of the guide plate end; the inlet and outlet of the aforementioned notch are both provided with a chamfered edge A to facilitate the introduction of the guide plate end.

[0012] The length of the guide plate is greater than three times the column spacing and less than four times the column spacing; the length of the support plate is greater than one times the column spacing and less than two times the column spacing.

[0013] The two ends of the guide plate are semi-circular.

[0014] The beneficial effects of this utility model are:

[0015] Due to the above structure, this utility model has a relatively simple structure, relatively low installation cost, and more ideal performance. Attached Figure Description

[0016] The present invention will be further described below with reference to the accompanying drawings and embodiments. Wherein:

[0017] Figure 1 is a schematic diagram of a prior art guided flight launch vehicle;

[0018] Figure 2 is a schematic diagram of this utility model;

[0019] Figure 3 is a schematic diagram of the body part of this utility model;

[0020] Figure 4 is a schematic diagram of the guide plate portion in this utility model;

[0021] Figure 5 is a schematic diagram of the guide post part in this utility model.

[0022] The markings and numbers in the attached diagram are explained as follows: 1. Cableway; 2. Roller; 3. Support rod; 4. Duct fan; 5. Body; 6. Guide column; 7. Guide plate; 8. Support plate; 9. Notch; 10. Through-hole; 11. Bevel on side B; 12. Bevel on side A. Detailed Implementation

[0023] As shown in Figures 2 to 5, an embodiment of this utility model is a skateboard-guided flight carrier device, comprising a guidance device and a body 5 mounted on the guidance device and equipped with a propulsion device; a support plate 8 is provided at the bottom of the body 5, and an elastic guide plate 7 is provided at the bottom of the support plate 8; multiple guide columns 6 are arranged at equal intervals along a set running path; a square through-hole 10 is radially opened near the top of the guide column 6, and the square through-hole 10...

[0024] A square notch 9 is provided between the top surface of the support plate 8 and the top surface of the guide post 6. The width of the through-hole 10 is greater than the width of the notch 9. The thickness of the support plate 8 is adapted to the width of the notch 9, and the thickness of the through-hole 10 is adapted to the thickness of the guide plate 7. The thickness of the guide plate 7 is greater than the width of the notch 9. The height of the support plate 8 is greater than the height of the notch 9, and the height of the guide plate 7 is less than the height of the through-hole 10. The total height of the support plate 8 and the guide plate 7 is greater than the total height of the notch 9 and the through-hole 10. The guide plate 7 is inserted into the corresponding through-hole 10, and the support plate 8 is inserted into the corresponding notch 9.

[0025] The aforementioned fuselage 5 is in the shape of a high-wing fixed-wing aircraft. The fuselage 5 as a whole has a roly-poly structure with a lower center of gravity, and the fulcrum of the roly-poly structure is located at the bottom of the guide plate 7.

[0026] Both wings of the aforementioned high-wing are angled downwards.

[0027] The propulsion device is a ducted fan 4, which is located at the tail of the machine.

[0028] The inlet and outlet edges of the through-hole 10 are provided with chamfered edges 11 on both sides to facilitate the insertion of the end of the guide plate 7; the inlet and outlet edges of the notch 9 are provided with chamfered edges 12 on both sides to facilitate the insertion of the end of the guide plate 7.

[0029] The length of the guide plate 7 is greater than three times the column spacing and less than four times the column spacing; the length of the support plate 8 is greater than one times the column spacing and less than two times the column spacing.

[0030] The two ends of the guide plate 7 are semi-circular.

[0031] The working principle of this utility model:

[0032] Due to the lift generated by the upper wing of the fuselage 5, and the fact that the fuselage 5 "flies" along the running path set by the guide column 6 under the propulsion of the propulsion device, the elastic guide plate 7 passes through each opening 10 on the running path in sequence. When flying low, the bottom surface of the guide plate 7 presses against the bottom surface of the opening 10, and when flying high, the top surface of the guide plate 7 presses against the top surface of the opening 10. The guide plate 7 is restricted to floating and passing through each opening 10, while the support plate 8 passes through each notch 9.

[0033] Because it has chamfer 12 on side A and chamfer 11 on side B, and the guide plate 7 is an elastic guide plate 7, moderate line bending does not affect the sequential passage of the guide plate 7.

[0034] When the aircraft is stopped, because both wings of the fuselage 5 are tilted downwards, the fuselage 5 has a self-sustaining structure with a lowered center of gravity. The fulcrum of this self-sustaining structure is located at the bottom of the guide plate 7. The fuselage 5 is supported by the guide plate 7 and stays on the corresponding guide post 6 without tipping over.

[0035] The propulsion device, in addition to the ducted fan 4, can also be other types of flight propulsion devices. In addition to being located at the tail, the propulsion device can also be located at other suitable locations on the fuselage.

Claims

1. A skateboard guided flying vehicle comprising a guiding device, a body mounted on the guiding device and provided with a propulsion device; characterized in that: The bottom of the body is provided with a support plate, and the bottom of the support plate is provided with an elastic guide plate; a plurality of guide columns are arranged along the set running path at equal column distance intervals; a square through hole is formed in the top portion of the guide column in the radial direction, a square gap is formed between the top surface of the square through hole and the top surface of the guide column, the width of the through hole is greater than the width of the gap; the thickness of the support plate is adapted to the width of the gap, the thickness of the through hole is adapted to the thickness of the guide plate, and the thickness of the guide plate is greater than the width of the gap; the height of the support plate is greater than the height of the gap, and the height of the guide plate is less than the height of the through hole; the total height of the support plate and the guide plate is greater than the total height of the gap and the through hole; the guide plate is inserted into the corresponding through hole, and the support plate is inserted into the corresponding gap.

2. A skateboard guided flying vehicle according to claim 1, characterized in that: The body is in the shape of a single-wing fixed-wing aircraft, and the overall body is a gravity-sinking Tumbler structure, and the fulcrum of the Tumbler structure is arranged at the bottom end of the guide plate.

3. A skateboard guided flying vehicle according to claim 2, wherein: Both sides of the single wing are inclined downward.

4. A skateboard guided flying vehicle according to claim 3, wherein: The propelling device is a ducted fan, which is arranged at the tail of the aircraft.

5. A skateboard guided flying vehicle according to claim 4, wherein: The inlet and outlet edges of the through hole are each provided with an edge chamfer for facilitating the insertion of the end of the guide plate; and the inlet and outlet edges of the gap are each provided with an edge chamfer for facilitating the insertion of the end of the guide plate.

6. A skateboard guided flying vehicle according to claim 5, wherein: The length of the guide plate is greater than three times the column distance and less than four times the column distance; and the length of the support plate is greater than one times the column distance and less than two times the column distance.

7. A skateboard guided flying vehicle according to claim 6, wherein: Both ends of the guide plate are semicircular.

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