CN212125524U - Remote flight device - Google Patents

Abstract

The application discloses long-range flying device, long-range flying device includes the fuselage, sets up power consumption subassembly, the deposit electric energy on fuselage and does in fuselage both sides power device, setting the first power and the deposit electric energy of power device power supply do the second power of power consumption subassembly power supply. The power device provides flight power for the remote flight device. This application has set up first power and second power, and first power is independent for the power device power supply, and the second power is independent for the power consumption subassembly power supply, the flight device's of increase power supply deposit. More importantly, the power device is provided with a special first power supply as a power supply, and even if the electric quantity of the second power supply is exhausted in the flying process of the remote flying device, so that the power device cannot work, the power device can also work normally, the remote flying device is ensured to continue flying or return to the air, the cruising ability of the remote flying device is enhanced, and the flying time is long.

Description

Remote flight device

Technical Field

The application relates to unmanned aerial vehicle application, especially relates to a long-range flight device.

Background

Among the flight devices, the unmanned aircraft is the most common. Such flying devices operate either entirely or intermittently autonomously by an onboard computer, using an unmanned aircraft operated by a radio remote control device and a self-contained program control device.

The flying device is widely applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster rescue, wild animal observation, infectious disease monitoring, surveying and mapping, news report, electric power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.

However, the current flight device generally has poor cruising ability and short flight time, and the application of the flight device is limited to a great extent.

SUMMERY OF THE UTILITY MODEL

The application aims at providing a long-range flight device, duration is strong, and flight time is long.

The application discloses long-range flying device, long-range flying device includes the fuselage, sets up power consumption subassembly, the deposit electric energy on fuselage and does in fuselage both sides power device, setting the first power and the deposit electric energy of power device power supply do the second power of power consumption subassembly power supply. The power device provides flight power for the remote flight device.

Optionally, the remote flying device further comprises a connecting rod, one end of the connecting rod is connected with the power device, and the other end of the connecting rod is connected with the power device; the second power supply is arranged on the connecting rod.

Optionally, the number of the power devices is four, two of the power devices are arranged on one of two sides of the machine body, and the other two of the power devices are arranged on the other of the two sides of the machine body; correspondingly, the number of the second power supplies is four, and the second power supplies are correspondingly arranged on the four connecting rods respectively.

Optionally, the body is provided with a battery accommodating chamber, and the first power supply is arranged in the battery accommodating chamber.

Optionally, the battery holds storehouse top opening, long-range flying device still includes the dead lever, the dead lever both ends connect respectively in the both sides in battery holds the storehouse.

Optionally, the number of the fixing rods is two, and the fixing rods are bent.

Optionally, the power plant comprises a motor and rotor blades; the motor with the connecting rod is kept away from the one end of fuselage is connected, first power does the motor power supply, the rotor blade with the transmission shaft of motor is connected.

Optionally, the long-range flight device further comprises a landing gear, and the landing gear is arranged above and below the aircraft and connected with the aircraft body.

This application has set up first power and second power, and first power is independent for the power device power supply, and the second power is independent for the power consumption subassembly power supply, the flight device's of increase power supply deposit. More importantly, the power device is provided with a special first power supply as a power supply, and even if the electric quantity of the second power supply is exhausted in the flying process of the remote flying device, so that the power device cannot work, the power device can also work normally, the remote flying device is ensured to continue flying or return to the air, the cruising ability of the remote flying device is enhanced, and the flying time is long.

Drawings

The accompanying drawings, which are included to provide a further understanding of the embodiments of the application, are incorporated in and constitute a part of this specification, illustrate embodiments of the application and together with the description serve to explain the principles of the application. It is obvious that the drawings in the following description are only some embodiments of the application, and that for a person skilled in the art, other drawings can be derived from them without inventive effort. In the drawings:

FIG. 1 is a schematic illustration of a remote heeling apparatus according to an embodiment of the present application;

FIG. 2 is an exploded view of a remote flying device according to an embodiment of the present application.

Wherein, 100, the fuselage; 110. a battery housing compartment; 200. a power plant; 210. a motor; 220. a rotor blade; 400. a first power supply; 500. a second power supply; 600. a circuit board; 700. a connecting rod; 800. fixing the rod; 900. a landing gear.

Detailed Description

It is to be understood that the terminology, the specific structural and functional details disclosed herein are for the purpose of describing particular embodiments only, and are representative, but that the present application may be embodied in many alternate forms and should not be construed as limited to only the embodiments set forth herein.

In the description of the present application, the terms "first", "second" are used for descriptive purposes only and are not to be construed as indicating relative importance or as implicitly indicating the number of technical features indicated. Thus, unless otherwise specified, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature; "plurality" means two or more. The terms "comprises" and "comprising," and any variations thereof, are intended to cover a non-exclusive inclusion, such that one or more other features, integers, steps, operations, elements, components, and/or combinations thereof may be present or added.

Further, terms of orientation or positional relationship indicated by "center", "lateral", "upper", "lower", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, are described based on the orientation or relative positional relationship shown in the drawings, are simply for convenience of description of the present application, and do not indicate that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present application.

Furthermore, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly and may include, for example, fixed connections, removable connections, and integral connections; can be mechanically or electrically connected; either directly or indirectly through intervening media, or through both elements. The specific meaning of the above terms in the present application can be understood by those of ordinary skill in the art as appropriate.

The present application is described in detail below with reference to the figures and alternative embodiments.

As shown in fig. 1 and 2, as an embodiment of the present application, a long-range flight device is disclosed, which includes a body 100, power devices 200 disposed at both sides of the body 100, power consuming components (not shown) disposed on the body 100, a first power source 400 storing electric energy and supplying power to the power devices 200, and a second power source 500 storing electric energy and supplying power to the power consuming components. The power device 200 provides flight power for the remote flight device. The electricity utilization components include other electricity utilization devices on the flight device, such as a camera, an indicator light, an illuminating light and the like, besides the power device 200. The first power source 400 and the second power source 500 may be devices such as lithium batteries that can store electric power and supply power. The long-range flying device also includes a circuit board 600.

The application has set up first power 400 and second power 500, and first power 400 independently supplies power for power device 200, and second power 500 independently supplies power for the power consumption subassembly, the flight device's of increase power reserve. More importantly, the power device 200 is provided with the special first power supply 400 as a power supply source, so that even if the remote flying device runs off the electric quantity of the second power supply 500 to cause the camera, the indicator light, the illuminating lamp and the like to be incapable of working, the power device 200 can also work normally, the remote flying device is ensured to continue flying or return to the air, the cruising ability of the remote flying device is enhanced, and the flying time is long.

Specifically, the remote flying device further comprises a connecting rod 700, wherein one end of the connecting rod 700 is connected with the power device 200, and the other end of the connecting rod 700 is connected with the power device 200; the second power source 500 is disposed on the connection bar 700. The second power supply 500 supplies power to the power utilization components such as the camera, the indicator light and the illuminating lamp, the basic function that the flight of the flight device is not influenced when the power utilization components are powered off and stop working is achieved, the design space of the flight device is limited, the second power supply 500 is designed on the connecting rod 700, and the space of the remote flight device body 100 can be saved. And for second power 500 of power consumption subassembly power supplies such as camera, pilot lamp, light, even lead to power capacity to reduce because the setting leads to on connecting rod 700, but can not influence this basic function of line device flight, when furthest has saved the space of long-range flight device fuselage 100, it is less to long-range flight device's overall performance influence.

In order to make the long-range flying device fly more smoothly and have sufficient flying power, the power devices 200 are four, two of the power devices 200 are arranged on one of the two sides of the fuselage 100, and the other two power devices 200 are arranged on the other of the two sides of the fuselage 100. Correspondingly, the number of the second power supplies 500 is also four, and the second power supplies are correspondingly and respectively arranged on the four connecting rods 700. The number of the second power supplies 500 is four, and the second power supplies are respectively arranged on the four connecting rods 700, so that firstly, the space of the connecting rods 700 can be fully utilized, the number of the second power supplies 500 is increased, and the cruising ability of the remote flight device is further improved; secondly, the long-range flight device is used for the open air more, carries out tasks such as taking photo by plane, agriculture, plant protection, and the environment is complicated, abominable, and four second power 500 sets up can be when long-range flight device descends on four connecting rods 700, because the weight of long-range flight device all around has evenly increased, and it is more steady to descend.

The body 100 is further provided with a battery receiving chamber 110, and the first power source 400 is disposed in the battery receiving chamber 110. The power device 200 is a main device consuming electric energy, the first power source 400 supplies power to the power device 200, the power device is arranged in the battery accommodating bin 110 of the aircraft body 100, the space of the aircraft body 100 is large, the first power source 400 can be designed to be larger according to the required volume, the corresponding electric capacity is also large, and the cruising ability of the long-range flight device is enhanced. Specifically, the circuit board 600 is disposed in the battery receiving chamber 110 and located below the first power source 400.

To facilitate heat dissipation, and to reduce the weight of the long range flight device to further enhance endurance, the battery receiving compartment 110 may be provided with an open top. Further, the remote flying device further comprises a fixing rod 800, and two ends of the fixing rod 800 are respectively connected to two sides of the battery accommodating chamber 110. The fixing rod 800 may play a role in fixing the first power supply 400, and may also increase the structural strength of the body 100 while ensuring the heat dissipation effect.

Specifically, the number of the fixing rods 800 is two, and the fixing rods 800 are bent. The contact area with the first power supply 400 is further enlarged, and the limiting effect is better.

The power plant 200 includes a motor 210 and rotor blades 220; the motor 210 is connected with one end of the connecting rod 700 far away from the fuselage 100, the first power source 400 supplies power to the motor 210, and the rotor blade 220 is connected with the transmission shaft of the motor 210.

The long-range flight device further comprises landing gears 900 disposed above and below the aircraft and connected to the fuselage 100. Landing gear 900 facilitates landing of the teleflight device in complex outdoor terrain.

The foregoing is a more detailed description of the present application in connection with specific alternative embodiments, and the specific implementations of the present application are not to be considered limited to these descriptions. For those skilled in the art to which the present application pertains, several simple deductions or substitutions may be made without departing from the concept of the present application, and all should be considered as belonging to the protection scope of the present application.

Claims (8)

1. A long-range flying device, comprising:

a body;

the power devices are arranged on two sides of the aircraft body and provide flying power for the remote flying device;

the power utilization assembly is arranged on the machine body;

the first power supply stores electric energy and supplies power to the power device;

and the second power supply stores electric energy and supplies power to the power utilization assembly.

2. The long-range flying device of claim 1, further comprising a connecting rod, wherein one end of said connecting rod is connected to said power device and the other end of said connecting rod is connected to said power device; the second power supply is arranged on the connecting rod.

3. A teleflight device as claimed in claim 2, wherein the power means are four, two of said power means being provided on one of the two sides of the fuselage and two of said power means being provided on the other of the two sides of the fuselage; correspondingly, the number of the second power supplies is four, and the second power supplies are correspondingly arranged on the four connecting rods respectively.

4. A teleflight device as in claim 2, wherein the fuselage is provided with a battery compartment and the first power source is disposed in the battery compartment.

5. The long-range flying device of claim 4, wherein said battery compartment is open at the top thereof, and said long-range flying device further comprises a fixing rod, both ends of said fixing rod are connected to both sides of said battery compartment.

6. The long-range flying device of claim 5, wherein said fixed rods are two, said fixed rods being bent.

7. A long-range flying device according to claim 2 wherein said power means comprises a motor and rotor blades; the motor with the connecting rod is kept away from the one end of fuselage is connected, first power does the motor power supply, the rotor blade with the transmission shaft of motor is connected.

8. A teleflight device according to claim 1, further comprising landing gear, disposed above and below the aircraft, connected to the fuselage.

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