CN106143909A - A kind of modularized combination type solar energy unmanned aerial vehicle design scheme - Google Patents
A kind of modularized combination type solar energy unmanned aerial vehicle design scheme Download PDFInfo
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- CN106143909A CN106143909A CN201610559395.8A CN201610559395A CN106143909A CN 106143909 A CN106143909 A CN 106143909A CN 201610559395 A CN201610559395 A CN 201610559395A CN 106143909 A CN106143909 A CN 106143909A
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- type solar
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- energy unmanned
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
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- Photovoltaic Devices (AREA)
Abstract
The present invention provides a kind of modularized combination type solar energy unmanned aerial vehicle design scheme, the program designs multiple modules, each module is equipped with motor, propeller, undercarriage and aerial docking structure, each module can independent takeoff and landing, after the lift-off of each module, flight is to low wind speed spatial domain, GPS or Beidou navigation and alignment system is utilized to determine the position of each module, the most each module merges the most in order, aerial docking structure ensures that modules stably docks combination, and the solar energy unmanned plane combined carries out climbing and cruising flight of more high altitude again.Helios based on this alternatives formulation, can effectively solve existing airport due to runway size limitation cannot the suffering of landing ultra-large type solar powered aircraft；Existing ground hangar can be utilized to deposit ultra-large type solar energy unmanned plane, flexible arrangement home port simultaneously；Multimode design adds system redundancy, it is achieved high reliability, it is achieved flight of leaving a blank time long.
Description
One, technical field:
The present invention provides a kind of modularized combination type solar energy unmanned aerial vehicle design scheme, belongs to new ideas aerospace vehicles system
System technical field.
Two, background technology:
Using solar energy as the supplementary energy of future aircraft even main energy sources, it is that human development has directivity and front
Important research target along property.Solar powered aircraft is to occur along with the reduction of solaode cost in the seventies in last century,
Owing to solar powered aircraft flight need not, from carrying fuel, create condition for flight during long boat.Therefore, many developed countries all cause
Power in using solar energy as the research and development of the HAE aircraft of energy source.
Current Helios owner solar-energy photo-voltaic cell to be used is as main power supply part, for obtaining more
Many solar energies, a feasible way is to increase the laying area of solar battery sheet, but this will certainly strengthen the sun
The overall dimensions of energy aircraft.But, the runway size on airport, the manufacture of solar powered aircraft often limit solar energy with transport and fly
The size of machine.
To this end, the present invention provides a kind of modularized combination type solar energy unmanned aerial vehicle design scheme.
Three, summary of the invention:
(1) purpose: the present invention provides a kind of modularized combination type solar energy unmanned aerial vehicle design scheme, uses program design
Solar energy unmanned plane, be to be docked the most in order by multiple modules to combine.Each module is independently taken off on ground, lift-off
After low wind speed spatial domain, utilize GPS or BDStar navigation system, determine the position of each module；Pass through path planning
Realizing the skyborne ordered pair of modules to engage also, form ultra-large type combination type solar unmanned plane, then this ultra-large type is too
Sun can realize climbing and cruising flight of more high altitude by unmanned plane again；After completing preplanned mission or arriving the predetermined area, this
Ultra-large type solar energy unmanned plane can drop to low wind speed spatial domain, carries out Ordered Decomposition, forms multiple module, and these multiple modules can be suitable
Sequence drops to predetermined airport.
(2) technical scheme: one modularized combination type solar energy unmanned aerial vehicle design scheme of the present invention, modularized combination type is too
Sun can be made up of multiple equal modules by unmanned plane, and each module uses high aspect ratio straight wing, and each module all cancels level
Empennage and vertical tail, the high aspect ratio straight wing of each module is arranged above reverse V-shaped wing, and reverse V-shaped trailing edge is
Movable control surface, each module is respectively provided with motor, undercarriage, propeller.
Wherein, described each module can realize independent takeoff and landing.
Wherein, described each module is take off can by reverse V-shaped trailing edge with the pitching in descent and yawing rotation
Dynamic control surface is handled.
Wherein, after each module is taken off, lift-off to low wind speed spatial domain, utilize GPS or Beidou navigation and alignment system, determine
The position of modules, the most aloft carries out sequential combination, forms modularized combination type solar energy unmanned plane.
Wherein, the pitching of described modularized combination type solar energy unmanned plane and yawing rotation are by the reverse V-shaped wing of modules
The movable control surface of trailing edge is combined controlling.
One modularized combination type solar energy unmanned aerial vehicle design scheme of the present invention, its basic design is as follows:
1) combine preset technical parameter and task parameters (include mission payload, airborne period, maximum flying speed and
Ceiling altitude etc.) and rise galassing weighing apparatus, push away resistance balance, energy balance principle, to modularized combination type solar energy unmanned plane
Carry out conceptual design, determine the original dimension of modules, formulate design, and design is proved and emulates
Checking and experimental verification；
2) according to design make modules, including wing, reverse V-shaped wing, the connection machinery of intermodule and
Other parts；
3) on the upside of wing, outside reverse V-shaped wing, lay solar battery sheet, and analyze its aerodynamic characteristic and whether meet and want
Ask；
4) energy-storage battery is installed, selects the battery of high-energy-density, according to the calculating process of the energy balance, rationally select storage
The weight of energy battery；
5) with step (4) simultaneously, the position of reasonable Arrangement lithium battery, it is ensured that the balance of fuselage；
6) the general assembly work of Helios individual module is carried out, including wing, reverse V-shaped wing, undercarriage, spiral
Oar, energy-storage battery etc.；
7) with step (6) simultaneously, the circuit of each inside modules is attached and carries out the compatible debugging of software and hardware,
Including aileron movement debugging, the debugging of reverse V-shaped wing control deflecting facet, motor and propeller joint debugging, the machine connect for intermodule
Tool device debugging；
8) last, make a flight test checking to modularized combination type solar energy unmanned plane.
(3) advantage and effect: one modularized combination type solar energy unmanned aerial vehicle design scheme of the present invention, has following excellent
Point.Troposphere circumstance complication is changeable, high aspect ratio solar energy unmanned plane in the environment or ultra-large type solar energy unmanned plane by
Relatively low in integral rigidity, structure is vulnerable to damage, and takes modularized design, allows each module of solar energy unmanned plane at troposphere liter
Sky, stratosphere combines, and owing to each module size is less, rigidity is enough, and this is to solving high aspect ratio solar energy unmanned plane or super
Large-sized solar unmanned plane troposphere lift-off difficult problem is a scheme very reliably；Energy due to solar energy unmanned plane
Deriving from the solar energy that solar battery sheet obtains, for obtaining more solar energy, an effective method is to increase solar energy
The laying area of cell piece, but this kind of method obviously can increase the overall dimensions of solar energy unmanned plane, for ultra-large type solar energy
Unmanned plane, cannot carry out landing under the conditions of existing airport, and modularized combination type solar energy unmanned plane scheme efficient solution
Certainly this problem, owing to each module size of composition solar energy unmanned plane is less, completely can be under the conditions of existing airport
Landing, then lift-off to low wind speed spatial domain is combined into ultra-large type solar energy unmanned plane, solves ultra-large type solar energy unmanned plane and exists
Existing airport cannot the problem of landing；System redundancy can be preferably accomplished in modular design, at severe troposphere environment
In lower take-off process, if certain module is taken off, lift-off is broken down, and can take off spare module, or solar energy unmanned plane is at sky
In middle flight course, certain module breaks down, and can carry out decomposition module in time, it is to avoid cause because of the fault of part of module
Whole ultra-large type solar energy unmanned plane crashes.
Four, accompanying drawing explanation:
Fig. 1 is the individual module outline drawing of the present invention a kind of modularized combination type solar energy unmanned aerial vehicle design scheme；
Fig. 2 is the three module integrated mode profile of the present invention a kind of modularized combination type solar energy unmanned aerial vehicle design scheme
Figure；
Fig. 3 is the three module combined front view of the present invention a kind of modularized combination type solar energy unmanned aerial vehicle design scheme；
Fig. 4 is the three module combination top view of the present invention a kind of modularized combination type solar energy unmanned aerial vehicle design scheme.
In figure, label is described as follows:
1. high aspect ratio straight wing 2. flaperon 3. wing of falling V
4. movable control surface 6. No. two modules of No. 5. modules
7. No. three module 8. undercarriage 9. propellers
Five, specific embodiments:
Do further below in conjunction with Fig. 1,2,3,4 pair one modularized combination type solar energy unmanned aerial vehicle design scheme of the present invention
Explanation.
The invention provides a kind of modularized combination type solar energy unmanned aerial vehicle design side based on aerial module docking technique
Case, the program can fully increase the irradiated area of sunlight, it is achieved solar energy unmanned plane is left a blank flight for a long time.Fig. 1 show
This solar energy unmanned plane individual module profile, this Helios individual module critical piece be high aspect ratio straight wing 1,
Reverse V-shaped wing 3, wherein, high aspect ratio straight wing 1 trailing edge is flaperon 2, reverse V-shaped wing 3 trailing edge for be responsible for elevating movement and
The control surface 4 of yawing rotation；The solar energy unmanned plane outline drawing that Fig. 2 is formed after showing three block combiner, a mould in Fig. 2
It is combined into a solar energy unmanned plane under the effect of 5, No. two modules 6 of block and No. three module 7 docking mechanisms aloft；In Fig. 3 respectively
The undercarriage 8 of individual module has a road clearance, prevents propeller 9 in Fig. 4 from contacting to earth during individual module take-off and landing.
Three independent modules, 5, No. two modules 6 of a module and No. three modules 7 are independently taken off on ground, go up to the air to the lowest
After wind speed spatial domain, utilize GPS or BDStar navigation system, determine the position of each module；Realized by path planning
Carry out ordered pair under the effect of 5, No. two modules 6 of a number module and No. three module 7 docking mechanisms aloft to engage also, form three moulds
Block combination type solar unmanned plane, then this three module combination type solar unmanned plane can realize climbing and patrolling of more high altitude again
Boat flight；After completing preplanned mission or arriving the predetermined area, this ultra-large type solar energy unmanned plane can drop to low wind speed spatial domain,
Aloft carry out Ordered Decomposition under the effect of docking mechanism, form 5, No. two modules 6 of a module and No. three modules 7, then one
Number 5, No. two modules 6 of module and No. three modules 7 can sequentially drop to predetermined airport.
One modularized combination type solar energy unmanned aerial vehicle design scheme of the present invention, its basic design is as follows:
1) combine preset technical parameter and task parameters (include mission payload, airborne period, maximum flying speed and
Ceiling altitude etc.) and rise galassing weighing apparatus, push away resistance balance, energy balance principle, to modularized combination type solar energy unmanned plane
Carry out conceptual design, determine the original dimension of modules, formulate design, and design is proved and emulates
Checking and experimental verification；
2) according to design make modules, including wing, reverse V-shaped wing, the connection machinery of intermodule and
Other parts；
3) on the upside of wing, outside reverse V-shaped wing, lay solar battery sheet, and analyze its aerodynamic characteristic and whether meet and want
Ask；
4) energy-storage battery is installed, selects the battery of high-energy-density, according to the calculating process of the energy balance, rationally select storage
The weight of energy battery；
5) with step (4) simultaneously, the position of reasonable Arrangement lithium battery, it is ensured that the balance of fuselage；
6) the general assembly work of Helios individual module is carried out, including wing, reverse V-shaped wing, undercarriage, spiral
Oar, energy-storage battery etc.；
7) with step (6) simultaneously, the circuit of each inside modules is attached and carries out the compatible debugging of software and hardware,
Including aileron movement debugging, the debugging of reverse V-shaped wing control deflecting facet, motor and propeller joint debugging, the machine connect for intermodule
Tool device debugging；
8) last, make a flight test checking to modularized combination type solar energy unmanned plane.
It should be pointed out that, the application process of this example only listing property explanation present invention, not for limiting the present invention.Any ripe
Know the personnel of this kind of use technology, all can without departing from the spirit and scope of the present invention above-described embodiment be modified.Cause
This, the scope of the present invention, should be as listed by claims.
Claims (6)
1. a modularized combination type solar energy unmanned aerial vehicle design scheme, it is characterised in that:
Using modularized design, solar energy unmanned plane is made up of multiple modules, and each module is equipped with power set, rises and falls
Frame, propeller, each module all can independent takeoff and landing, it is possible to independently rise to given area.
2. a modularized combination type solar energy unmanned aerial vehicle design scheme, it is characterised in that:
Each module all uses high aspect ratio straight wing, cancels tailplane and vertical tail, at high aspect ratio straight wing
Top, is provided with reverse V-shaped wing, reverse V-shaped wing and the triangle rock-steady structure of high aspect ratio straight wing.
3. a modularized combination type solar energy unmanned aerial vehicle design scheme, it is characterised in that:
The reverse V-shaped trailing edge of each module is provided with movable aerofoil, and this movable aerofoil serves as control surface, can replace tailplane
Elevating movement and yawing rotation is handled with vertical tail.
4. a modularized combination type solar energy unmanned aerial vehicle design scheme, it is characterised in that:
After modules rises to low wind speed spatial domain, by the navigation positioning system such as GPS or the Big Dipper, determine each module position,
Pass through path planning again, it is achieved the skyborne orderly merging of modules, be combined into a large-sized solar aircraft, then realize
Climbing and cruising flight of more high altitude.
5. a modularized combination type solar energy unmanned aerial vehicle design scheme, it is characterised in that:
During modules goes up to the air, if certain module breaks down, the spare module that can go up to the air immediately is replaced；As
Fruit is after modules merges in order, and certain module breaks down, and can aloft implement decomposition module, is thrown by malfunctioning module
From, remaining module reconsolidates into a large-sized solar aircraft.
6. a modularized combination type solar energy unmanned aerial vehicle design scheme, it is characterised in that:
Its basic design is as follows:
1) combine the technical parameter preset and task parameters (includes mission payload, airborne period, maximum flying speed and maximum
Flying height etc.) and rise galassing weighing apparatus, push away resistance balance, energy balance principle, modularized combination type solar energy unmanned plane is carried out
Conceptual design, determines the original dimension of modules, formulates design, and proves design and simulating, verifying
And experimental verification；
2) according to design make modules, including wing, reverse V-shaped wing, the connection machinery of intermodule and other
Parts；
3) on the upside of wing, outside reverse V-shaped wing, lay solar battery sheet, and analyze whether its aerodynamic characteristic meets requirement；
4) energy-storage battery is installed, selects the battery of high-energy-density, according to the calculating process of the energy balance, rationally select energy storage electricity
The weight in pond；
5) with step (4) simultaneously, the position of reasonable Arrangement lithium battery, it is ensured that the balance of fuselage；
6) the general assembly work of Helios individual module is carried out, including wing, reverse V-shaped wing, undercarriage, propeller, storage
Energy battery etc.；
7) with step (6) simultaneously, the circuit of each inside modules is attached and carries out the compatible debugging of software and hardware, including
Aileron movement debugging, the debugging of reverse V-shaped wing control deflecting facet, motor and propeller joint debugging, the machinery dress connect for intermodule
Put debugging；
8) last, make a flight test checking to modularized combination type solar energy unmanned plane.
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| CN201610559395.8A CN106143909B (en) | 2016-07-15 | 2016-07-15 | A kind of modularized combination type solar energy unmanned aerial vehicle design scheme |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107272721A (en) * | 2017-07-11 | 2017-10-20 | 北京昶远科技有限公司 | A kind of solar energy unmanned aerial vehicle flight path planing method flown based on day-night cycle |
| CN107450576A (en) * | 2017-07-24 | 2017-12-08 | 哈尔滨工程大学 | A kind of method of bridge machinery unmanned plane path planning |
| CN108216679A (en) * | 2017-12-26 | 2018-06-29 | 中国航天空气动力技术研究院 | A kind of solar energy unmanned plane population parameter determines method and system |
| CN110816806A (en) * | 2019-10-28 | 2020-02-21 | 西北工业大学 | Cluster type bionic solar unmanned aerial vehicle |
| CN112093026A (en) * | 2020-09-25 | 2020-12-18 | 中国空气动力研究与发展中心 | Combined aircraft layout and connecting mechanism |
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| CN107272721A (en) * | 2017-07-11 | 2017-10-20 | 北京昶远科技有限公司 | A kind of solar energy unmanned aerial vehicle flight path planing method flown based on day-night cycle |
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| CN112093026A (en) * | 2020-09-25 | 2020-12-18 | 中国空气动力研究与发展中心 | Combined aircraft layout and connecting mechanism |
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| CN106143909B (en) | 2019-10-29 |
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