CN105292439A - Petrol-electric hybrid power airship - Google Patents
Petrol-electric hybrid power airship Download PDFInfo
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- CN105292439A CN105292439A CN201510748283.2A CN201510748283A CN105292439A CN 105292439 A CN105292439 A CN 105292439A CN 201510748283 A CN201510748283 A CN 201510748283A CN 105292439 A CN105292439 A CN 105292439A
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Abstract
The invention relates to the field of aviation, in particular to a petrol-electric hybrid power airship. The petrol-electric hybrid power airship comprises an airship body (1) and a power device (2), and the power device (2) is arranged below the airship body (1). The petrol-electric hybrid power airship is characterized in that the power device (2) is a petrol-electric hybrid power device and comprises three propellers (21, 22, 23), wherein two of the propellers (21, 22) are electric propellers, and one propeller (23) is liquid fuel power propeller. According to the petrol-electric hybrid power airship, the liquid fuel power propeller and the electric propellers are organically combined, so that control response of the airship in the aviation process can be rapidly achieved, and the flight posture is rapidly adjusted so that different aviation requirements can be met.
Description
Technical field
The present invention relates to aviation field, relate to a kind of oily electric hybrid dirigible more specifically.
Background technology
Current unmanned vehicle has high easy control, the further flexibility of application due to it, very popular, and the application obtained widely, it has potential huge applications space in industrial or agricultural application aspect such as Homeland Security, industry, agricultural, fire-fighting, forestry, communications and transportation, its promotion and application prospect is boundless, becomes current research and development focus.But unmanned vehicle of the prior art mostly has following shortcoming: the shortcomings such as cruise duration is short, load carrying ability is little, poor controllability, the wide range of industrial applications of existence to unmanned vehicle of these shortcomings creates very big restriction.
Summary of the invention
The present invention, for overcoming at least one defect (deficiency) described in above-mentioned prior art, provides a kind of oily electric hybrid dirigible.
The present invention is intended to solve the problems of the technologies described above at least to a certain extent.
For solving the problems of the technologies described above, technical scheme of the present invention is as follows:
A kind of oily electric hybrid dirigible, comprise dirigible hull and engine installation, described engine installation is arranged on the below of dirigible hull; Described engine installation is oily electric hybrid device, comprises three screw propellers, and wherein two screw propellers are electric propeller, and another screw propeller is liquid fuel power spin oar.
Compared with prior art, the beneficial effect of technical solution of the present invention is:
Oily electric hybrid dirigible provided by the invention, by the combination of liquid fuel power spin oar and electric propeller, dirigible carries out the adjustment of dirigible navigation attitude in the process of navigation simultaneously in conjunction with electric propeller using liquid fuel power spin oars such as gasoline as main power resources, existence due to liquid fuel power spin oar makes dirigible can obtain enough power and longer cruise duration, must adjust in conjunction with electric propeller on this basis, make dirigible can obtain control response fast in the process of navigation, rapid adjustment flight attitude, to adapt to different navigation demands.
Further, as optimal technical scheme, described three screw propellers are that del is arranged, wherein said electric propeller transverse horizontal is arranged, described liquid fuel power spin oar is positioned at the rear of two electric propeller lines and described liquid fuel power spin oar is positioned on the midperpendicalar of two electric propeller lines.The engine installation that del is arranged can use the liquid fuel motors such as gasoline as major impetus, and both sides motor carries out pose adjustment, is conducive to the wind loading rating greatly improving dirigible.The inverted triangle power arrangement that its engine petrol is rearmounted simultaneously, there are 2 advantages: 1. liquid fuel power spin oar, powerful air-flow can not affect the motor helical oar (if liquid fuel power spin oar is preposition, powerful air-flow can make the air turbulence of motor helical oar) of attitude regulation; 2. liquid fuel power spin oar, the powerful air-flow through screw propeller directly flows to rear empennage, rear empennage boundary 1ayer flow velocity is obviously increased, the efficiency of rear empennage is significantly improved, effectively reduces the turn radius of dirigible.
Further, as optimal technical scheme, the S. A. of described electric propeller can rotate around the line of two electric propellers.Because the S. A. of electric propeller can rotate around the line of two electric propellers, therefore make the present invention in use can by controlling the force vector of two electric propellers in left and right, fluid,matching fluid fuel power spin oar, flight attitude is controlled, the efficiency that airship's posture controls can be improved, save by oil mass, further raising cruise duration, and realize the function such as vertical takeoff and landing, pivot stud, aerial reversing of dirigible, make dirigible of the present invention have the easy control of height, the application variety under different occasion and environment can be met.
Further, as optimal technical scheme, described electric propeller includes two sub-screw propellers, and described two sub-propeller coaxials are arranged.The existence of two sub-screw propellers, the power making electric propeller can provide larger, makes electric propeller that dynamic response can be provided more quickly and easily to adjust the navigation attitude of dirigible.
Further, as optimal technical scheme, land for ease of dirigible and protect the engine installation of dirigible, the below of described dirigible hull is provided with support.
Accompanying drawing explanation
Fig. 1 is the structural representation of embodiment of the present invention front view.
Fig. 2 is the enlarged drawing of A in Fig. 1.
Fig. 3 is the structural representation of embodiment of the present invention upward view.
Fig. 4 is the enlarged drawing of B in Fig. 3.
Fig. 5 is the structural representation of embodiment of the present invention block diagram.
Accompanying drawing, only for exemplary illustration, can not be interpreted as the restriction to this patent; In order to better the present embodiment is described, some parts of accompanying drawing have omission, zoom in or out, and do not represent the size of actual product; To those skilled in the art, in accompanying drawing, some known features and explanation thereof may be omitted is understandable; The corresponding same or analogous parts of same or analogous label; The term describing position relationship in accompanying drawing, only for exemplary illustration, can not be interpreted as the restriction to this patent.
Detailed description of the invention
Below in conjunction with drawings and Examples, technical scheme of the present invention is described further.
Embodiment 1
A kind of oily electric hybrid dirigible, comprise dirigible hull 1 and engine installation 2, described engine installation 2 is arranged on the below of dirigible hull 1, and the below of described dirigible hull 1 is also provided with support 3; Described engine installation 2 is oily electric hybrid device, comprise three screw propellers 21,22,23, wherein two screw propellers 21,22 are electric propeller, and a screw propeller 23 is liquid fuel (can be the liquid fuels such as gasoline, kerosene, hydrogen) power spin oar; Described three screw propellers 21,22,23 are arranged in del, wherein said electric propeller 21,22 transverse horizontal is arranged, described liquid fuel power spin oar 23 is positioned at the rear of two electric propellers 21,22 line and described liquid fuel power spin oar 23 is positioned on the midperpendicalar of two electric propellers 21,22 line; Described electric propeller 21,22 includes two sub-screw propellers 211,212, and described two sub-screw propellers 211,212 are coaxially arranged; The S. A. of described electric propeller 21,22 can rotate around the line of two electric propellers 21,22.
In use, when the dirigible navigation of the present invention's oil electric hybrid, greater weight attendant equipment can be carried, and provide power to realize the long-time navigation of dirigible by liquid fuel power spin oar, in addition in the process of navigation by change two electric propellers attitude to realize the adjustment of the navigation attitude such as vertical takeoff and landing, hovering, pivot stud, aerial reversing of dirigible to realize different navigation demands.
Obviously, the above embodiment of the present invention is only for example of the present invention is clearly described, and is not the restriction to embodiments of the present invention.For those of ordinary skill in the field, can also make other changes in different forms on the basis of the above description.Here exhaustive without the need to also giving all embodiments.All any amendments done within the spirit and principles in the present invention, equivalent to replace and improvement etc., within the protection domain that all should be included in the claims in the present invention.
Claims (5)
1. an oily electric hybrid dirigible, comprise dirigible hull (1) and engine installation (2), described engine installation (2) is arranged on the below of dirigible hull (1); It is characterized in that, described engine installation (2) is oily electric hybrid device, comprises three screw propellers (21,22,23), and wherein two screw propellers (21,22) are electric propeller, and a screw propeller (23) is liquid fuel power spin oar.
2. oily electric hybrid dirigible according to claim 1, it is characterized in that, described three screw propellers (21,22,23) are arranged in del, wherein said electric propeller (21,22) transverse horizontal is arranged, described liquid fuel power spin oar (23) is positioned at the rear of two electric propellers (21,22) line and described liquid fuel power spin oar (23) is positioned on the midperpendicalar of two electric propellers (21,22) line.
3. oily electric hybrid dirigible according to claim 1, is characterized in that, the S. A. of described electric propeller (21,22) can rotate around the line of two electric propellers (21,22).
4. the oily electric hybrid dirigible according to any one of claim 1-3, is characterized in that, described electric propeller (21,22) includes two sub-screw propellers (211,212), and described two sub-screw propellers (211,212) are coaxially arranged.
5. oily electric hybrid dirigible according to claim 4, is characterized in that, the below of described dirigible hull (1) is provided with support (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510748283.2A CN105292439A (en) | 2015-11-06 | 2015-11-06 | Petrol-electric hybrid power airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510748283.2A CN105292439A (en) | 2015-11-06 | 2015-11-06 | Petrol-electric hybrid power airship |
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| Publication Number | Publication Date |
|---|---|
| CN105292439A true CN105292439A (en) | 2016-02-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510748283.2A Pending CN105292439A (en) | 2015-11-06 | 2015-11-06 | Petrol-electric hybrid power airship |
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| CN (1) | CN105292439A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081047A (en) * | 2016-07-28 | 2016-11-09 | 无锡信大气象传感网科技有限公司 | A kind of sounding balloon of adjustable point monitoring |
| CN106240787A (en) * | 2016-07-28 | 2016-12-21 | 无锡信大气象传感网科技有限公司 | A kind of using method of highly controllable sounding balloon |
| CN106240786A (en) * | 2016-07-28 | 2016-12-21 | 无锡信大气象传感网科技有限公司 | A kind of highly controllable sounding balloon |
| CN113830279A (en) * | 2021-11-09 | 2021-12-24 | 中国电子科技集团公司第三十八研究所 | Propeller electric propulsion device for adjusting posture of airship |
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| CN2895243Y (en) * | 2006-05-16 | 2007-05-02 | 河南送变电建设公司 | Remote control boat seaplane |
| CN201494622U (en) * | 2009-12-18 | 2010-06-02 | 杨礼诚 | Wired electric flying and floating aircraft |
| CN204210726U (en) * | 2014-11-11 | 2015-03-18 | 张宏志 | A kind of solar power rotor inflation soft body unmanned airship |
| CN104443343A (en) * | 2014-11-13 | 2015-03-25 | 上海交通大学 | Vectored thruster suspension type flight device |
| CN204568048U (en) * | 2015-04-24 | 2015-08-19 | 常州大学 | A kind of eight axles drive the small-sized dirigible of solar power remote control |
| CN104943844A (en) * | 2015-05-21 | 2015-09-30 | 东莞市诸葛流智能***有限公司 | Robot capable of carrying out indoor floating and flying operations |
| CN205150215U (en) * | 2015-11-06 | 2016-04-13 | 东莞华南设计创新院 | Hybrid formula power dirigible |
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Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2895243Y (en) * | 2006-05-16 | 2007-05-02 | 河南送变电建设公司 | Remote control boat seaplane |
| CN201494622U (en) * | 2009-12-18 | 2010-06-02 | 杨礼诚 | Wired electric flying and floating aircraft |
| CN204210726U (en) * | 2014-11-11 | 2015-03-18 | 张宏志 | A kind of solar power rotor inflation soft body unmanned airship |
| CN104443343A (en) * | 2014-11-13 | 2015-03-25 | 上海交通大学 | Vectored thruster suspension type flight device |
| CN204568048U (en) * | 2015-04-24 | 2015-08-19 | 常州大学 | A kind of eight axles drive the small-sized dirigible of solar power remote control |
| CN104943844A (en) * | 2015-05-21 | 2015-09-30 | 东莞市诸葛流智能***有限公司 | Robot capable of carrying out indoor floating and flying operations |
| CN205150215U (en) * | 2015-11-06 | 2016-04-13 | 东莞华南设计创新院 | Hybrid formula power dirigible |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081047A (en) * | 2016-07-28 | 2016-11-09 | 无锡信大气象传感网科技有限公司 | A kind of sounding balloon of adjustable point monitoring |
| CN106240787A (en) * | 2016-07-28 | 2016-12-21 | 无锡信大气象传感网科技有限公司 | A kind of using method of highly controllable sounding balloon |
| CN106240786A (en) * | 2016-07-28 | 2016-12-21 | 无锡信大气象传感网科技有限公司 | A kind of highly controllable sounding balloon |
| CN113830279A (en) * | 2021-11-09 | 2021-12-24 | 中国电子科技集团公司第三十八研究所 | Propeller electric propulsion device for adjusting posture of airship |
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Application publication date: 20160203 |