CN206606352U - A kind of strong unmanned plane of endurance - Google Patents
A kind of strong unmanned plane of endurance Download PDFInfo
- Publication number
- CN206606352U CN206606352U CN201720062980.7U CN201720062980U CN206606352U CN 206606352 U CN206606352 U CN 206606352U CN 201720062980 U CN201720062980 U CN 201720062980U CN 206606352 U CN206606352 U CN 206606352U
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- unmanned plane
- fuselage
- bladder
- actuating unit
- storage device
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Abstract
The utility model is a kind of strong unmanned plane of endurance, includes fuselage, and described fuselage includes organic frame, wing arm, rotor driver, controlling organization；Also include actuating unit and Fu Sheng mechanisms, described Fu Sheng mechanisms include the bladder of gas, and density of the density less than air of the gas for its internal cavity, and the Fu Sheng mechanisms are connected to back and its buoyancy is not more than the self gravitation of fuselage；Described actuating unit is fuel cell, and it includes the battery cell in frame and the fuel storage device in bladder, and described fuel storage device is filled with the fuel air bag of hydrogen for its internal cavity.It helps to counteract that the part gravity of fuselage by being connected to the Fu Sheng mechanisms of fuselage, reduce the energy resource consumption of actuating unit, improve the endurance of unmanned plane, fuel storage device can also provide certain floating buoyancy auxiliary unmanned plane and offset gravity flight, the energy of actuating unit is further saved, the cruising time of unmanned plane is extended.
Description
【Technical field】
The utility model is related to a kind of unmanned plane, specifically refers to a kind of strong unmanned plane of endurance.
【Background technology】
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Possess that cost is low, efficiency-cost ratio is good, mobility is good due to it, it is easy to use many advantages, such as, at present in boat
Bat, agricultural, plant protection, auto heterodyne, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electricity
It is used widely in power inspection, the disaster relief, movies-making etc. field.
Unmanned plane generally comprises organic body portion, control section, power section and payload segment；Body part is frame,
And it is arranged on many wing arms in frame；Motor and rotor that power section refers to power source and is arranged on wing arm；Control unit
It is divided into the controlling organization in frame；Payload segment is the load being equipped in frame.Wherein power source can be lithium battery,
It can also be fuel cell.From above-mentioned, unmanned plane overall weight is larger, before the weight of payload segment carrying is not calculated
Put, the energy that it overcomes the self gravitation of its body part in flight and expended is not already small, greatly reduce its continuation of the journey
Ability, and it is unfavorable for effective utilization of the energy, it is unfavorable for energy-conserving and environment-protective.
In view of the above-mentioned problems, we have proposed a kind of new technical scheme.
【Utility model content】
The purpose of this utility model is to be to overcome the deficiencies in the prior art there is provided a kind of strong nobody of endurance
Machine, its is rational in infrastructure, reduces the energy resource consumption of actuating unit.
In order to solve above-mentioned technical problem, the utility model uses following technical proposals：
A kind of strong unmanned plane of endurance, includes fuselage, and described fuselage includes organic frame, is arranged in frame
Some wing arms, the rotor drivers located at wing arm two ends, and the controlling organization in frame, described rotor driver include
There are rotor motor and propeller；Also include the actuating unit that power is provided to rotor driver；Also include Fu Sheng mechanisms, it is described
Fu Sheng mechanisms include in set the bladder of cavity, the close of gas and the gas is included in the cavity of described bladder
Degree is less than the density of air, and the Fu Sheng mechanisms are connected to buoyancy that back and producing in air floats up to offset
The gravity of fuselage, the buoyancy of the Fu Sheng mechanisms is not more than the self gravitation of fuselage；Described actuating unit is fuel cell, institute
The fuel cell stated includes at least one battery cell and fuel storage device；Described battery cell is located in frame, its
Include anode end plate, cathode end plate, catalyst and electrolyte；Described fuel storage device is arranged inside bladder, its
To include the closed fuel air bag of cavity, hydrogen is filled with the cavity of the fuel air bag；Described fuel storage dress
It is put to be connected to battery cell to supply hydrogen to battery cell by tracheae.
In to a kind of above-mentioned improvement project of the unmanned plane of band Fu Sheng mechanisms, described bladder is balloon spheroid, its
Interior gas is hydrogen.
In to a kind of above-mentioned improvement project of the unmanned plane of band Fu Sheng mechanisms, described bladder is balloon spheroid, its
Interior gas is helium.
Compared with prior art, the beneficial effects of the utility model are：It passes through the Fu Sheng mechanisms being connected on fuselage, side
The part gravity for offsetting unmanned aerial vehicle body is helped, the energy resource consumption of actuating unit is greatly reduced, the endurance of unmanned plane is improved,
In addition, the fuel storage device in the actuating unit of unmanned plane, which can also provide certain floating buoyancy auxiliary unmanned plane, offsets weight
Power is flown, and is further saved the energy of actuating unit, is extended the cruising time of unmanned plane.
The utility model is described in further detail with embodiment below in conjunction with the accompanying drawings：
【Brief description of the drawings】
Fig. 1 is the schematic perspective view of the utility model embodiment；
Fig. 2 is the utility model embodiment front view；
Fig. 3 is the structural representation of the utility model embodiment.
【Embodiment】
A kind of strong unmanned plane of endurance, as shown in the embodiment such as Fig. 1,2,3, includes fuselage, described machine
Body includes organic frame 10, some wing arms 20, the rotor driver located at the two ends of wing arm 20 being arranged in frame 10, and is located at
Controlling organization in frame 10, described rotor driver includes rotor motor 30 and propeller 40；Also include and give rotor dress
Put the actuating unit that power is provided；Also include Fu Sheng mechanisms, described Fu Sheng mechanisms include the interior bladder 50 for setting cavity,
Gas and density of the density less than air of the gas are included in the cavity of described bladder 50, described in embodiment
Bladder 50 be balloon spheroid, gas in it is hydrogen or helium；The Fu Sheng mechanisms are connected to back and in sky
The buoyancy floated up is produced in gas to offset the gravity of fuselage, the buoyancy of the Fu Sheng mechanisms is not more than itself weight of fuselage
Power, can so ensure unmanned plane fuselage be unlikely to Fu Sheng mechanisms rising floating buoyancy drive under be subjected to displacement,
Leave ground；Described actuating unit is fuel cell, and described fuel cell includes at least one battery cell and fuel
Storage device 70；Described battery cell is in frame 10, and it includes anode end plate, cathode end plate, catalyst and electrolysis
Liquid；Described fuel storage device 70 is arranged inside bladder 50, and it is the closed fuel air bag for including cavity, described
Hydrogen is filled with the cavity of fuel air bag；Described fuel storage device its battery cell is connected to electricity by tracheae 60
Pond monomer supply hydrogen.
The utility model on the fuselage of unmanned plane by connecting one with the Fu Sheng mechanisms for rising floating buoyancy, to offset
Part gravity in unmanned aerial vehicle body deadweight, unmanned plane is driven which reduces unmanned mechanism of ocean in driving rotor driver
The energy offset gravity acting during upward flight and consumed, greatly reduces the energy resource consumption of actuating unit, improves unmanned plane
Endurance, effectively increases energy utilization rate, and energy-conserving and environment-protective can also make unmanned plane be easier to lift-off of taking off, rapidly enter
Working condition.Further, since the fuel storage device 70 being built in bladder 50, which is its internal cavity, is filled with the closed of hydrogen
Air bag, its own possesses certain floating buoyancy, with conventional actuating unit（Lithium battery）Need the feelings being arranged in frame 10
Condition is compared, actuating unit of the present utility model with little need for consumption the energy come offset actuating unit its own gravity go up to the air fly
OK（Only need the gravity of burden battery cell）, additionally it is possible to certain floating buoyancy auxiliary unmanned plane is provided and offsets gravity flight, is entered
The energy of actuating unit is saved to one step, the cruising time of unmanned plane is extended.
Although the utility model is described in detail with reference to above example, by the disclosure for people in the art
Member is not it is readily apparent that and departing from the principle of the present utility model and the situation of scope of described claim restriction
Under, the utility model can be made a variety of changes or be changed.Therefore, the detailed description of the embodiment of the present disclosure is only used for explaining, and
The utility model is not intended to limit, but is defined by the subject-matter of the claims the scope of protection.
Claims (3)
1. the strong unmanned plane of a kind of endurance, it is characterised in that include fuselage, described fuselage includes organic frame, set
In some wing arms, the rotor driver located at wing arm two ends in frame, and the controlling organization in frame, described rotation
Swing device includes rotor motor and propeller；Also include the actuating unit that power is provided to rotor driver；Also include auxiliary
Mechanism is risen, described Fu Sheng mechanisms include the interior bladder for setting cavity, gas has been included in the cavity of described bladder
And the density of the gas is less than the density of air, the Fu Sheng mechanisms are connected to back and produced in air and floated up
Buoyancy to offset the gravity of fuselage, the buoyancy of the Fu Sheng mechanisms is not more than the self gravitation of fuselage；Described actuating unit
For fuel cell, described fuel cell includes at least one battery cell and fuel storage device；Described battery cell
In frame, it includes anode end plate, cathode end plate, catalyst and electrolyte；Described fuel storage device is arranged at
Inside bladder, it is the closed fuel air bag for including cavity, and hydrogen is filled with the cavity of the fuel air bag；It is described
Fuel storage device its by tracheae be connected to battery cell with to battery cell supply hydrogen.
2. the strong unmanned plane of a kind of endurance according to claim 1, it is characterised in that described bladder is balloon
Spheroid, the gas in it is hydrogen.
3. the strong unmanned plane of a kind of endurance according to claim 1, it is characterised in that described bladder is balloon
Spheroid, the gas in it is helium.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720062980.7U CN206606352U (en) | 2017-01-17 | 2017-01-17 | A kind of strong unmanned plane of endurance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720062980.7U CN206606352U (en) | 2017-01-17 | 2017-01-17 | A kind of strong unmanned plane of endurance |
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| Publication Number | Publication Date |
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| CN206606352U true CN206606352U (en) | 2017-11-03 |
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| CN201720062980.7U Active CN206606352U (en) | 2017-01-17 | 2017-01-17 | A kind of strong unmanned plane of endurance |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045543A (en) * | 2017-12-12 | 2018-05-18 | 中国科学院工程热物理研究所 | The jettison system of unmanned plane |
| NO20180140A1 (en) * | 2018-01-29 | 2019-07-30 | Sjur Haugen | Drone with increased lifting ability and integrated range extender |
-
2017
- 2017-01-17 CN CN201720062980.7U patent/CN206606352U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045543A (en) * | 2017-12-12 | 2018-05-18 | 中国科学院工程热物理研究所 | The jettison system of unmanned plane |
| NO20180140A1 (en) * | 2018-01-29 | 2019-07-30 | Sjur Haugen | Drone with increased lifting ability and integrated range extender |
| NO344297B1 (en) * | 2018-01-29 | 2019-10-28 | Sjur Haugen | Drone with increased lifting capacity and integrated range extender |
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