Low-altitude thermoelectric transport helicopter

Abstract

The invention discloses a low-altitude thermoelectric helicopter which comprises a circular truss, and a plurality of rotors are mounted above the truss; a cab and a container are installed below the truss, a control cabinet is installed in the front of the cab, and a thermoelectric power generation body is installed behind the cab. Wherein the thermoelectric power generation body comprises a solid body formed by rolling an alloy thin plate, a spiral line is wound on the solid body, one end of the solid body is connected with an input end of a rectifier, and the other end of the solid body is connected with a negative electrode of a unilateral diode; two ends of the spiral line are connected with an alternating-current power supply; and the output end of the rectifier and the positive electrode of the unilateral diode are electrically connected with the rotor wing and the control cabinet to form a closed loop. The aircraft is long in voyage, sufficient in power and low in transportation cost.

Description

Technical Field

[0001] The invention relates to a helicopter, in particular to a low-altitude thermal power transport helicopter. Background Art

[0002] In recent years, with the introduction of a series of industrial policies, the low-altitude helicopter industry, as a key component of new and innovative productivity, is strongly driving the vigorous development of the "low-altitude economy." Low-altitude helicopters are widely used in modern transportation, logistics, security, emergency rescue, and other fields. However, helicopters currently still suffer from shortcomings such as short range and weak power. Summary of the Invention

[0003] The purpose of the present invention is to provide a low-altitude thermal electric transport helicopter, which has the advantages of long range, sufficient power and low transportation cost.

[0004] In order to achieve the above purpose, this paper adopts the following technical solutions:

[0005] A low-altitude thermoelectric helicopter, comprising:

[0006] A circular truss with a plurality of rotors mounted above the truss;

[0007] A cab and a cargo box are installed below the truss, a control cabinet is installed in the front of the cab, and a thermoelectric generator is installed in the rear;

[0008] The thermoelectric generator comprises a body formed by rolling an alloy sheet, a spiral wire is wound around the body, one end of the body is connected to the input end of a rectifier, and the other end is connected to the cathode of a unidirectional diode;

[0009] The two ends of the spiral line are connected to an AC power source; the output end of the rectifier and the positive electrode of the one-way diode are electrically connected to the rotor and the control cabinet to form a closed loop.

[0010] Preferably, the entity is fixed on a base made of high temperature resistant insulating material.

[0011] Preferably, a tail wing is further installed at the tail of the truss.

[0012] Preferably, a plurality of brackets are installed around the truss.

[0013] Preferably, a cargo box is installed below the truss.

[0014] Preferably, the cargo box is hung below the truss by a hook.

[0015] Preferably, the cargo box is fixed below the truss via a hanger.

[0016] Preferably, a partition is used to separate the front side of the cargo box into a power room and a temperature control room, a generator is installed in the power room, and a temperature control machine is installed in the temperature control room.

[0017] Preferably, the temperature control chamber is communicated with the cargo box.

[0018] Preferably, a driving chair is installed next to the control cabinet.

[0019] The advantages of the present invention are long range, sufficient power and low transportation cost. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 This is a schematic structural diagram of a low-altitude thermoelectric helicopter of the present invention;

[0021] Figure 2 It is a schematic diagram of the structure of a thermoelectric generator of the present invention.

[0022] Description of reference numerals:

[0023] 1. Rotor, 2. Truss, 3. Support base, 4. Tail, 5. Support, 6. Shaft, 7. Boom frame, 8. Boom, 9. Cargo box, 10. Thermoelectric generator, 11. Entity, 12. Base, 13. Reinforcement plate, 14. Partition, 15. Temperature controller, 16. Control cabinet, 17. Cab, 18. Driving seat, 19. Drive engine, 20. Power room, 21. Temperature control room, 22. Cargo box cover, 23. Thermoelectric chamber, 24. One-way diode, 25. Helix, 26. Generator, 27. Rectifier. DETAILED DESCRIPTION

[0024] The present invention is further described in detail below with reference to the accompanying drawings and embodiments.

[0025] See attached Figure 1 , Figure 1 This is a low-altitude thermoelectric helicopter comprising a truss 2, which is a circular skeleton with multiple rotors 1 mounted above the truss 2. The rotors 1 are arranged along the four sides of the truss 2. A cab 17 and a cargo box 9 are mounted below the truss 2. A control cabinet 16 is mounted in the front of the cab 17, and a thermoelectric generator 10 is mounted in the rear. A driver's chair 18 is mounted next to the control cabinet 16. A tail wing 4 is also mounted on the side of the truss 2. Several pairs of drive motors 19 are mounted on the left and right sides of the cab 17 to drive the corresponding rotors 1. A thermoelectric chamber 23 is provided in the cab 17, and the thermoelectric generator 10 is located in the thermoelectric chamber 23.

[0026] The thermoelectric generator 10 comprises a body 11 formed from a rolled alloy sheet, with a spiral wire 25 wound around it. One end of the body 11 is connected to the input of a rectifier 27, and the other end is connected to the cathode of a one-way diode 24. The two ends of the spiral wire 25 are connected to an AC power source. The output of the rectifier 27 and the anode of the one-way diode 24 are electrically connected to the rotor 1 and the control cabinet 16, forming a closed circuit. When AC power is applied to both ends of the spiral wire 25, the thermoelectric generator 10 generates current, which then forms a closed circuit with related electrical equipment through wires. The wire connecting the rectifier 27 and the one-way diode 24 is a strand of bare wire twisted together. The wires from the thermoelectric generator 10, the rotor 1, the drive motor 19, and the tail fin 4 control wires are all housed in the control cabinet 16. The helicopter's lift and lowering movements, as well as the navigation instruments, are all controlled by buttons on the control panel.

[0027] Entity 11 is fixed to a base 12 made of high-temperature resistant insulating material. Several brackets 5 are also installed around the truss 2. Brackets 5 are fixed to bracket bases 3, which are installed at the rear of truss 2. Brackets 5 are fixed to bracket bases 3, which are installed at the rear of truss 2. There are four brackets 5 at the four corners.

[0028] A cargo box 9 is also mounted below the truss 2. The cargo box 9 can be suspended from the truss 2 via a hook. Alternatively, the cargo box 9 can be secured to the truss 2 below via a boom 8. For example, a boom frame 7 and an axle 6 are provided below the truss 2. A reinforcing rib 13 is provided within the cargo box 9. One end of the boom 8 is connected to the boom frame 7 via the axle 6, and the other end is fixedly connected to the reinforcing rib 13.

[0029] The front side of the cargo box 9 is divided into a power room 20 and a temperature control room 21 by a partition 14. The power room 20 is equipped with a generator 26, and the temperature control room 21 is equipped with a temperature control machine 15. The temperature control room 21 is connected to the cargo box 9.

[0030] The above are preferred embodiments of the present invention and the technical principles used therein. For those skilled in the art, any obvious changes such as equivalent transformations, simple replacements, etc. based on the technical solution of the present invention, without departing from the spirit and scope of the present invention, are within the scope of protection of the present invention.

Claims

1. A low-altitude thermoelectric helicopter, characterized in that: include: A circular truss with a plurality of rotors mounted above the truss; A cab and a cargo box are installed below the truss, a control cabinet is installed in the front of the cab, and a thermoelectric generator is installed in the rear; The thermoelectric generator comprises a body formed by rolling an alloy sheet, a spiral wire is wound around the body, one end of the body is connected to the input end of a rectifier, and the other end is connected to the cathode of a unidirectional diode; The two ends of the spiral line are connected to an AC power source; the output end of the rectifier and the positive electrode of the one-way diode are electrically connected to the rotor and the control cabinet to form a closed loop.

2. The low-altitude thermoelectric helicopter according to claim 1, characterized in that: The entity is fixed on a base made of high-temperature resistant insulating material.

3. The low-altitude thermoelectric helicopter according to claim 1, characterized in that: A tail wing is also installed at the tail of the truss.

4. The low-altitude thermoelectric helicopter according to claim 1, characterized in that: A plurality of brackets are also installed around the truss.

5. The low-altitude thermoelectric helicopter according to claim 1, characterized in that: A cargo box is also installed below the truss.

6. The low-altitude thermoelectric helicopter according to claim 5, characterized in that: The cargo box is hung below the truss through a hook.

7. The low-altitude thermoelectric helicopter according to claim 5, characterized in that: The cargo box is fixed below the truss through a suspension rod.

8. The low-altitude thermoelectric helicopter according to claim 7, characterized in that: The front side of the cargo box is divided into a power room and a temperature control room by a partition. A generator is installed in the power room, and a temperature controller is installed in the temperature control room.

9. The low-altitude thermoelectric helicopter according to claim 8, characterized in that: The temperature control chamber is communicated with the cargo box.

10. The low-altitude thermoelectric helicopter according to claim 1, characterized in that: A driving chair is installed next to the control cabinet.

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