Power hydrogen balloon aircraft

Abstract

The invention discloses a power hydrogen balloon aircraft, and relates to the technical field of aircrafts. A bearing plate is arranged at the bottom of the main frame, the two driving steering engines are fixed to the bearing plate and symmetrically arranged, the driving steering engines are connected with the propellers through steering engine power output rods, the control module is electrically connected with the driving steering engines and the propellers, and the control module is in wireless signal connection with the remote controller. The operation platform is connected with the bottom of the main frame through traction ropes. According to the invention, hydrogen balloon buoyancy is successfully combined with an electric driving technology, and long-time suspension and flexible control of the aircraft are realized. Through wireless connection between the remote controller and the control module, a user can accurately control the flight state of the aircraft within a safe distance. And the stability and the safety of the aircraft are improved through the reasonable layout design and the use of the propeller cover. And due to the design of the expansion frame of the operation platform, the possibility of installing additional equipment or functions is provided for a user.

Description

Technical Field

[0001] The present invention relates to the technical field of aircraft, in particular to a powered hydrogen balloon aircraft. Background Art

[0002] Traditional hydrogen balloon aircraft mainly rely on the buoyancy of hydrogen to rise into the air, lacking active power systems and effective control methods, making it difficult to accurately control the flight direction and altitude. Although existing electric aircraft have strong controllability, they are often limited by their own weight and energy consumption, making it difficult to achieve the effect of long-term suspension and long-distance flight. Therefore, developing an aircraft that can combine the advantages of both, with both buoyancy support and active control capabilities, has become the focus of industry research. Summary of the invention

[0003] The technical problem to be solved by the present invention is to provide a powered hydrogen balloon aircraft, which combines the buoyancy of the hydrogen balloon with an electric drive system to achieve stable suspension and remote control of the aircraft.

[0004] In order to solve the above technical problems, the technical solution provided by the present invention is as follows: a powered hydrogen balloon aircraft, comprising a sphere, a power mechanism, a remote controller and an operating platform;

[0005] The sphere is connected to the top of the power mechanism via a load rope;

[0006] The power mechanism includes a main frame, a driving steering gear, a steering gear power output rod, a propeller and a control module. A bearing plate is provided at the bottom of the main frame, two driving steering gears are fixed on the bearing plate and symmetrically provided, the driving steering gear is connected to the propeller through the steering gear power output rod, the control module is electrically connected to the driving steering gear and the propeller, and the control module is connected to the remote controller by wireless signal;

[0007] The operating platform is connected to the bottom of the main frame through a traction rope.

[0008] Furthermore, the propeller includes a mounting frame, a driving motor and a rotating blade. The mounting frame is arranged at the end of the steering gear power output rod and is arranged perpendicular to the steering gear power output rod. The driving motor is arranged at both ends of the mounting frame, and the rotating blade is connected to the power output end of the driving motor.

[0009] Furthermore, a propeller cover fixing frame is provided on the mounting frame, and a semicircular propeller cover is provided on the outer side of the propeller cover fixing frame.

[0010] Furthermore, the control module includes a power base, a transformer and a receiver, the power base is connected to the battery on the operating platform, the transformer is electrically connected to the power base, the receiver is electrically connected to the transformer, the servo, and the drive motor, and the receiver is connected to the remote control wireless signal.

[0011] Furthermore, the operating platform includes a main frame and an expansion frame, the top of the main frame is connected to the bottom of the main frame through a traction rope, and the expansion frame is arranged on one side of the top of the main frame.

[0012] The advantages of the present invention compared with the prior art are:

[0013] 1. The present invention successfully combines the buoyancy of hydrogen balloons with electric drive technology, achieving long-term suspension and flexible control of the aircraft.

[0014] 2. Through the wireless connection between the remote controller and the control module, the user can accurately control the flight status of the aircraft within a safe distance.

[0015] 3. Reasonable layout design and the use of propeller covers improve the stability and safety of the aircraft.

[0016] 4. The expansion frame design of the operating platform provides users with the possibility of installing additional devices or functions. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 It is a structural schematic diagram of a powered hydrogen balloon aircraft of the present invention.

[0018] Figure 2 It is a front view of a powered hydrogen balloon aircraft of the present invention.

[0019] Figure 3 It is a partial structural diagram of the power mechanism.

[0020] Figure 4 It is a top view of part of the structure of the power mechanism.

[0021] Figure 5 It is a schematic diagram of the structure of the remote control.

[0022] As shown in the figure: 1. sphere, 2. remote control, 3. load rope, 4. main frame, 5. driving servo, 6. servo power output rod, 7. propeller, 8. load plate, 9. traction rope, 10. mounting frame, 11. driving motor, 12. rotating blades, 13. propeller cover fixing frame, 14. semicircular propeller cover, 15. power base, 16. transformer, 17. receiver, 18. main frame, 19. expansion frame. DETAILED DESCRIPTION

[0023] In the description of the present invention, it is necessary to understand that the orientations or positional relationships indicated by terms such as “upper”, “lower”, “front”, “back”, “left”, “right”, “inside”, “outside”, “vertical” and “circumferential” are based on the orientations or positional relationships shown in the accompanying 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 on the present invention.

[0024] In the present invention, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", "fixed" and the like 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 a direct connection or an indirect connection through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0025] A powered hydrogen balloon aircraft of the present invention will be described in further detail below in conjunction with the accompanying drawings.

[0026] Combined with Figure 1-5 The specific implementation process of a powered hydrogen balloon aircraft of the present invention is as follows:

[0027] A powered hydrogen balloon aircraft mainly comprises a sphere 1, a power mechanism, a remote controller 2 and an operating platform;

[0028] The sphere 1 is the main part of the aircraft, providing necessary buoyancy support so that the aircraft can stably float in the air. The sphere 1 is connected to the power mechanism through a load rope 3. The sphere 1 can be a hydrogen balloon or a helium balloon.

[0029] The power mechanism includes:

[0030] The main frame 4 serves as a supporting structure for the power mechanism and fixes other components.

[0031] The bearing plate 8 is disposed at the bottom of the main frame 4 and is used for mounting the driving steering gear 5 .

[0032] Two driving steering gears 5 are symmetrically arranged, and the propeller 7 is driven to rotate through the steering gear power output rod 6, thereby changing the direction of the propeller 7.

[0033] The steering gear power output rod 6 connects the driving steering gear 5 and the propeller 7 to transmit torque.

[0034] The propeller 7 includes a mounting frame 10, a driving motor 11 and rotating blades 12. The rotation of the driving motor 11 drives the blades to rotate, thereby generating thrust.

[0035] The control module is responsible for receiving signals from the remote controller 2, controlling the operation of the driving servo 5 and the driving motor 11, and realizing remote control of the aircraft.

[0036] The remote controller 2 is used to send wireless signals to the control module to control the flight status of the aircraft.

[0037] Operation platform: connected to the bottom of the main frame 4 through a traction rope 9, providing a user with an operating space and a place to place items such as batteries to ensure the continuous operation of the aircraft.

[0038] The detailed design of the propeller 7 is as follows: the mounting frame 10 is vertically arranged with the servo power output rod 6, drive motors 11 are installed at both ends, the drive motors 11 are connected to the rotating blades 12, forming an efficient propulsion system, and the rotation speed difference of the drive motors 11 at both ends is used to realize the steering of the entire aircraft.

[0039] Propeller cover design: A propeller cover fixing frame 13 is provided on the mounting frame 10, and a semicircular propeller cover 14 is provided on the outer side, which helps to reduce noise and improve flight safety.

[0040] The detailed structure of the control module includes a power base 15, a transformer 16 and a receiver 17. The power base 15 is connected to the battery on the operating platform, the transformer 16 adjusts the voltage, and the receiver 17 receives the signal from the remote controller 2 and controls the driving servo 5 and the driving motor 11.

[0041] Expandability of the operating platform: The operating platform consists of a main frame 18 and an expansion frame 19. The main frame 18 is connected to the main frame 4, and the expansion frame 19 is used to install additional equipment or increase user operating space.

[0042] The present invention and its embodiments are described above, and such description is not restrictive. The drawings show only one embodiment of the present invention, and the actual structure is not limited thereto. In short, if ordinary technicians in the field are inspired by it, without departing from the purpose of the invention, they can design a structure and embodiment similar to the technical solution without creativity, which should belong to the protection scope of the present invention.

Claims

1. A powered hydrogen balloon aircraft, characterized in that: It comprises a sphere (1), a power mechanism, a remote controller (2) and an operating platform; The sphere (1) is connected to the top of the power mechanism via a load rope (3); The power mechanism comprises a main frame (4), a driving steering gear (5), a steering gear power output rod (6), a propeller (7) and a control module, wherein a bearing plate (8) is provided at the bottom of the main frame (4), the driving steering gear (5) is fixed on the bearing plate (8) and two driving steering gears (5) are symmetrically provided, the driving steering gear (5) is connected to the propeller (7) via the steering gear power output rod (6), the control module is electrically connected to the driving steering gear (5) and the propeller (7), and the control module is wirelessly connected to the remote controller (2); The operating platform is connected to the bottom of the main frame (4) via a traction rope (9).

2. A powered hydrogen balloon aircraft according to claim 1, characterized in that: The propeller (7) comprises a mounting frame (10), a driving motor (11) and a rotating blade (12); the mounting frame (10) is arranged at the end of a steering gear power output rod (6) and is arranged perpendicular to the steering gear power output rod (6); the driving motor (11) is arranged at both ends of the mounting frame (10); and the rotating blade (12) is connected to the power output end of the driving motor (11).

3. A powered hydrogen balloon aircraft according to claim 2, characterized in that: A propeller cover fixing frame (13) is arranged on the mounting frame (10), and a semicircular propeller cover (14) is arranged outside the propeller cover fixing frame (13).

4. A powered hydrogen balloon aircraft according to claim 3, characterized in that: The control module comprises a power base (15), a transformer (16) and a receiver (17); the power base (15) is connected to a battery on an operating platform; the transformer (16) is electrically connected to the power base (15); the receiver (17) is electrically connected to the transformer (16), a steering gear and a drive motor (11); and the receiver (17) is wirelessly connected to a remote controller (2).

5. A powered hydrogen balloon aircraft according to claim 4, characterized in that: The operating platform comprises a main frame (18) and an expansion frame (19); the top of the main frame (18) is connected to the bottom of the main frame (4) via a traction rope (9); and the expansion frame (19) is arranged on one side of the top of the main frame (18).

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