CN110194268A - A kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity - Google Patents
A kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity Download PDFInfo
- Publication number
- CN110194268A CN110194268A CN201910509286.9A CN201910509286A CN110194268A CN 110194268 A CN110194268 A CN 110194268A CN 201910509286 A CN201910509286 A CN 201910509286A CN 110194268 A CN110194268 A CN 110194268A
- Authority
- CN
- China
- Prior art keywords
- shell
- unmanned plane
- anger
- gas turbine
- wheel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000005611 electricity Effects 0.000 title claims abstract description 15
- 230000001914 calming effect Effects 0.000 claims abstract description 14
- 238000004804 winding Methods 0.000 claims abstract description 11
- 230000005540 biological transmission Effects 0.000 claims abstract description 3
- 239000007921 spray Substances 0.000 claims description 3
- 239000000295 fuel oil Substances 0.000 abstract description 12
- 238000005265 energy consumption Methods 0.000 abstract description 5
- 239000003921 oil Substances 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 239000007789 gas Substances 0.000 description 29
- 239000000567 combustion gas Substances 0.000 description 5
- 239000000446 fuel Substances 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 239000002828 fuel tank Substances 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000010248 power generation Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 239000010723 turbine oil Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000010721 machine oil Substances 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
- B64C15/12—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The invention discloses a kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity, including shell, the wheel of calming the anger being rotatably arranged in shell, with calm the anger wheel transmission connection and with calm the anger take turns rotation center it is coaxial and be located in shell engine spindle, be arranged in and calm the anger the permanent magnet on taking turns and with permanent magnet be correspondingly arranged coil windings inside the shell, the coil windings are connected with battery by the output module that generates electricity, the shell is communicated with gas turbine close to the one end for wheel of calming the anger, and the other end of shell is provided with the jet pipe sprayed for gas.The beneficial effects of the present invention are: this programme provides power using fuel oil, more energy are capable of providing compared to battery identical in quality, to increase the cruising ability of unmanned plane, in flight course, fuel oil can continue to consume, and be conducive to that unmanned plane is made constantly to reduce self weight during flight, to save energy consumption, power is provided using fuel oil, additionally it is possible to increase the maximum take-off weight of unmanned plane.
Description
Technical field
The present invention relates to air vehicle technique field, specifically a kind of unmanned plane is filled with miniature gas turbine oil electric mixed dynamic
It sets.
Background technique
Currently, application of the unmanned plane in fields such as mapping, plant protection, electric inspection process, petroleum line walking, frontier defense monitoring is more and more wider
It is general, but the disadvantage that cruise duration is short, lifting capacity is relatively small greatly limits the development of professional unmanned plane and pushes away
Extensively.By taking traditional pure electric agricultural plant protection unmanned plane as an example, need specially to transport equipped with the lorry of larger loading space in operation
It transmits electricity generating equipment needed for pond and scene charging, is not used only, transition is cumbersome also increases additional cost to user.For
This problem, have at present using minitype piston engine add again microgenerator combine Unmanned Aerial Vehicle Powerplants, the device with
Fuel tank is installed on unmanned plane together, with unmanned plane flight operation, passes through hair again using piston engine fuel consumption
Motor, which produces electricl energy, provides power supply for unmanned plane.Cruise duration can further be promoted and increase loading capacity.But it is limited to piston
The construction and operation logic of engine, so that the power device power to weight ratio of the type is smaller, and except own vol other than fuel tank
It is bigger than normal with weight.Continuation of the journey and loading capacity hoisting power for unmanned plane is limited.
Summary of the invention
In order to overcome the deficiencies of the prior art, the present invention provides a kind of unmanned plane miniature gas turbine oil electric mixed dynamics
Device, for improving the cruising ability of unmanned plane.
Technical solution used by the present invention solves the above problems is: a kind of unmanned plane micro-gas-turbine machine oil electricity mixing
Power device including shell, the wheel of calming the anger being rotatably arranged in shell, is sequentially connected with wheel of calming the anger and takes turns rotation center with calming the anger
It is coaxial and be located in shell engine spindle, the permanent magnet calmed the anger on wheel is set and is correspondingly arranged inside the shell with permanent magnet
Coil windings, the coil windings are connected with battery by the output module that generates electricity, and the shell is close to wheel of calming the anger
One end is communicated with gas turbine, and the other end of shell is provided with the jet pipe sprayed for gas.
Further, in order to preferably realize the present invention, diffuser is provided in the shell.
It further, further include the supporting structure for installing shell, the shell in order to preferably realize the present invention
It is rotatablely connected with supporting structure.
Further, in order to preferably realize the present invention, the supporting structure includes ring support and two mounting blocks,
The shell is rotatably installed in ring support, and the ring support is rotatably installed between two mounting blocks.
Beneficial effect acquired by this programme is:
(1) this programme provides power using fuel oil, is capable of providing more energy compared to battery identical in quality, thus
The cruising ability for increasing unmanned plane, in flight course, fuel oil can continue to consume, and be conducive to make unmanned plane during flight
Constantly reduce self weight, to save energy consumption, provides power using fuel oil, additionally it is possible to increase the maximum take-off weight of unmanned plane；
(2) this programme can be generated electricity using the power that fuel oil generates, and improve the utilization rate of power produced by fuel oil, right
Power generation generate electric energy carry out deposit be used in later period fuel consumption it is complete after using electric energy continue support unmanned plane during flying, to increase
Add unmanned plane cruising ability；
(3) this programme uses miniature gas turbine, since the rotor speed of miniature gas turbine is compared to piston IC engine
Fast decades of times, according to Faraday's law, phase homogenous quantities, identical winding, same magnetic field intensity generator, use micro-gas-turbine
Generated power drives generated power much larger than piston engine when machine driving, to reach equal-wattage, use is miniature
Gas turbine powered generating set can be more light and small, and hair thus can be greatly reduced compared to existing piston type generating equipment
Motor weight, to be conducive to reduce unmanned plane self weight；
(4) based on the working principle of miniature gas turbine, inherently there is bigger power compared to piston engine
Mass ratio, the miniature gas turbine weight of equal-wattage often only have piston-engined one third to 1/5th, use
The weight and volume of engine itself can be greatly reduced as generator power source for gas turbine, be conducive to reduce unmanned plane certainly
Weight reduces energy consumption when unmanned plane during flying, improves the cruising ability of unmanned plane；
(4) after this programme is using miniature gas turbine starting, best efficiency point is worked in always, and revolving speed does not fly with unmanned plane
Row state change and change, can be improved the utilization rate of fuel oil, obtain higher fuel economy；
(5) generator is placed in miniature gas turbine by this programme, makes miniature gas turbine with the shared main shaft of generator, outside
Shell, support construction etc. can reduce space occupied by structure, mitigate complete machine self weight, be conducive to reduce unmanned plane self weight, reduce
Unmanned plane energy consumption；
(6) this programme is to utilize combustion gas thrust-drag margin as far as possible, and it is corresponding to obtain to be capable of the angle of adjustable jet tube as needed
Flying power, improve the utilization rate of fuel oil.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of this programme；
Fig. 2 is the structural schematic diagram of miniature gas turbine；
Fig. 3 is control planning schematic diagram；
Fig. 4 is that jet pipe turns to schematic diagram.
Wherein: 1- shell, 2- calm the anger wheel, 3- engine spindle, 4- coil windings, 41- permanent magnet, 5- jet pipe, 6- diffusion
Device, 7- ring support, 8- mounting blocks.
Specific embodiment
Below with reference to examples and drawings, the present invention is described in further detail, but embodiments of the present invention are not
It is limited to this.
Embodiment 1:
As shown in Figure 1 and Figure 2, in the present embodiment, a kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity, packet
Include shell 1, the wheel 2 of calming the anger that is rotatably arranged in shell 1, with calm the anger 2 transmission connection of wheel and with calm the anger 2 rotation centers of wheel coaxially simultaneously
Engine spindle 3 in shell 1 is arranged in the permanent magnet 41 calmed the anger on wheel 2 and is correspondingly arranged at shell 1 with permanent magnet 41
Interior coil windings 4, the coil windings 4 are connected with battery by the output module that generates electricity, and the shell 1 is close to calm the anger
One end of wheel 2 is communicated with gas turbine, and the other end of shell 1 is provided with the jet pipe 5 sprayed for gas.
In the present embodiment, the common knowledge and customary means that wheel 2 is those skilled in the art of calming the anger is specific
Structure does not repeat the specific structure and working principle of wheel 2 of calming the anger herein not as the improvement of this programme.
The shell 1 is mounted in unmanned aerial vehicle rack, and the fuel tank being connected to miniature gas turbine is arranged in unmanned plane machine
On frame, jet pipe 5 is set downward.It is miniature gas turbine fuel feeding using fuel tank, when miniature gas turbine starts, non-combusted fuels turn
It turns to mechanical work and pushes 2 rotation of wheel of calming the anger.
Wheel 2 of calming the anger drives permanent magnet rotation, so that coil windings 4 be made to rotate relative to permanent magnet 41 and cut permanent magnet 41
Magnetic induction line to generate induced electromotive force, electric energy can be exported by power generation output module with this, the electric energy of output can be used in
Unmanned plane load, extra electric energy is to charge the battery to be laid in.Unemployed combustion gas then can be downward by jet pipe 5
It sprays and generates the thrust for flying unmanned plane upwards, be conducive to make unmanned plane quickly to take off or fall-retarding.
Compared to battery identical in quality, miniature gas turbine is capable of providing more energy using fuel oil, to increase
The cruising ability of unmanned plane, in flight course, fuel oil can continue to consume, and be conducive to keep unmanned plane continuous during flight
Reduce self weight, to save energy consumption.
As shown in figure 3, miniature gas turbine is remotely controlled using the controller of unmanned plane in the present embodiment, and
And it is electrically connected with the controller power generation output module, it is convenient for being monitored the charging situation of battery with this.
In the present embodiment, diffuser 6 is provided in the shell 1.Pressurization can be played to combustion gas using diffuser 6
, be conducive to the utilization rate for improving combustion gas.
In the present embodiment, miniature gas turbine further includes the supporting structure for installing shell 1, the shell 1 and branch
The rotation connection of frame structure.The supporting structure is arranged in the rack of unmanned plane, as the installation foundation of miniature gas turbine,
It is rotatably installed in shell 1 on supporting structure, miniature gas turbine can be made to have the function of rotation, so as to adjustable jet tube
5 angle carrys out regulating gas from the direction that jet pipe 5 sprays with this, and can adjust the direction of unmanned plane during flying, improves combustion gas
Utilization rate.
As shown in figure 4, in the present embodiment, the supporting structure includes ring support 7 and two mounting blocks 8, described
Shell 1 is rotatably installed in ring support 7, and the ring support 7 is rotatably installed between two mounting blocks 8.Shell 1 is pacified
It in ring support 7, is supported using symmetrical support rod, can be improved the stability of miniature gas turbine.Make shell 1
Rotation center of the rotation center perpendicular to ring support 7 relative to mounting blocks 8 relative to ring support 7 utilizes two with this
Rotary freedom realizes miniature gas turbine multi-angle, multidirectional rotation in spatial dimension, and flies control linkage with unmanned plane
So that the flight control of unmanned plane is more convenient, bigger flying speed is provided in horizontal flight.
The ring support 7 or shell 1 is connected with the drive system of its rotation of driving accordingly, makes ring support with this
7 or shell 1 realize the function of rotation, in the present embodiment, the drive system is the prior art, those skilled in the art's root
The content recorded according to this programme selects suitable drive system to can be realized said effect, herein not to the specific knot of drive system
Structure and working principle are repeated.
It is electrically connected with the controller drive system, is convenient for remotely controlling driving using controller with this, it is remote with this
The rotation of journey adjustable jet tube 5.
In the present embodiment, other contents not described are same as the previously described embodiments, therefore do not repeat.
It is above-described, it is only presently preferred embodiments of the present invention, is not intended to limit the present invention in any form,
According to the technical essence of the invention, within the spirit and principles in the present invention, to the above embodiments any simply to repair
Change, equivalent replacement and improvement etc., fall within the scope of protection of the technical scheme of the present invention within.
Claims (4)
1. a kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity, it is characterised in that: set including shell (1), rotation
Set the wheel (2) of calming the anger in shell (1), with calm the anger wheel (2) transmission connection and with calm the anger wheel (2) rotation center it is coaxial and positioned at outside
Engine spindle (3) in shell (1), setting permanent magnet (41) on wheel (2) and are correspondingly arranged at permanent magnet (41) calming the anger
Coil windings (4) in shell (1), the coil windings (4) are connected with battery by the output module that generates electricity, and described is outer
Shell (1) is communicated with gas turbine close to the one end for wheel (2) of calming the anger, and the other end of shell (1) is provided with the spray sprayed for gas
It manages (5).
2. a kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity according to claim 1, it is characterised in that:
Diffuser (6) are provided in the shell (1).
3. a kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity according to claim 1, it is characterised in that:
It further include the supporting structure for installing shell (1), the shell (1) and supporting structure are rotatablely connected.
4. a kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity according to claim 3, it is characterised in that:
The supporting structure includes ring support (7) and two mounting blocks (8), and the shell (1) is rotatably installed in ring support
(7) in, the ring support (7) is rotatably installed between two mounting blocks (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910509286.9A CN110194268A (en) | 2019-06-13 | 2019-06-13 | A kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910509286.9A CN110194268A (en) | 2019-06-13 | 2019-06-13 | A kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110194268A true CN110194268A (en) | 2019-09-03 |
Family
ID=67754359
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910509286.9A Pending CN110194268A (en) | 2019-06-13 | 2019-06-13 | A kind of unmanned plane miniature gas turbine hybrid power apparatus of oil and electricity |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110194268A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113879547A (en) * | 2021-11-16 | 2022-01-04 | 西安觉天动力科技有限责任公司 | Rotary support of micro turbojet engine |
| CN113879546A (en) * | 2021-11-16 | 2022-01-04 | 西安觉天动力科技有限责任公司 | Aerial adjustable spray angle vortex spraying system |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201902263U (en) * | 2010-12-21 | 2011-07-20 | 湖南航天机电设备与特种材料研究所 | High-speed electrical generator complete equipment for minitype gas turbine |
| CN202754143U (en) * | 2012-07-26 | 2013-02-27 | 沈阳申蓝航空科技有限公司 | Rotating engine vertical take-off and landing aircraft |
| US20170015417A1 (en) * | 2014-08-29 | 2017-01-19 | Reference Technologies Inc | Multi-Propulsion Design for Unmanned Aerial Systems |
| CN107813948A (en) * | 2017-11-27 | 2018-03-20 | 大连理工大学 | Unmanned vehicle based on the full electric propulsion of miniature gas turbine |
| CN107813947A (en) * | 2017-11-27 | 2018-03-20 | 大连理工大学 | A kind of hybrid power unmanned vehicle using exhaust continuation of the journey |
| CN109356720A (en) * | 2018-10-21 | 2019-02-19 | 至玥腾风科技投资集团有限公司 | Miniature gas turbine generating set and unmanned plane |
-
2019
- 2019-06-13 CN CN201910509286.9A patent/CN110194268A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201902263U (en) * | 2010-12-21 | 2011-07-20 | 湖南航天机电设备与特种材料研究所 | High-speed electrical generator complete equipment for minitype gas turbine |
| CN202754143U (en) * | 2012-07-26 | 2013-02-27 | 沈阳申蓝航空科技有限公司 | Rotating engine vertical take-off and landing aircraft |
| US20170015417A1 (en) * | 2014-08-29 | 2017-01-19 | Reference Technologies Inc | Multi-Propulsion Design for Unmanned Aerial Systems |
| CN107813948A (en) * | 2017-11-27 | 2018-03-20 | 大连理工大学 | Unmanned vehicle based on the full electric propulsion of miniature gas turbine |
| CN107813947A (en) * | 2017-11-27 | 2018-03-20 | 大连理工大学 | A kind of hybrid power unmanned vehicle using exhaust continuation of the journey |
| CN109356720A (en) * | 2018-10-21 | 2019-02-19 | 至玥腾风科技投资集团有限公司 | Miniature gas turbine generating set and unmanned plane |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113879547A (en) * | 2021-11-16 | 2022-01-04 | 西安觉天动力科技有限责任公司 | Rotary support of micro turbojet engine |
| CN113879546A (en) * | 2021-11-16 | 2022-01-04 | 西安觉天动力科技有限责任公司 | Aerial adjustable spray angle vortex spraying system |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190903 |
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| RJ01 | Rejection of invention patent application after publication |