CN106516115A - Micro-power aircraft and system - Google Patents
Micro-power aircraft and system Download PDFInfo
- Publication number
- CN106516115A CN106516115A CN201611267853.7A CN201611267853A CN106516115A CN 106516115 A CN106516115 A CN 106516115A CN 201611267853 A CN201611267853 A CN 201611267853A CN 106516115 A CN106516115 A CN 106516115A
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- Prior art keywords
- micro power
- power aircraft
- aircraft
- micro
- acceleration
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- 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.)
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- 230000001133 acceleration Effects 0.000 claims abstract description 32
- 238000005183 dynamical system Methods 0.000 claims description 10
- 238000002360 preparation method Methods 0.000 claims description 9
- 238000005516 engineering process Methods 0.000 abstract description 7
- 238000010586 diagram Methods 0.000 description 5
- 238000004642 transportation engineering Methods 0.000 description 5
- 108010022579 ATP dependent 26S protease Proteins 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Launching or towing gear
Abstract
The invention discloses a micro-power aircraft and system and belongs to the field of transport means. The micro-power aircraft comprises micro-power aircraft bodies 1 and acceleration transit systems 2. The micro-power aircraft bodies 1 can be loaded with cargoes and can fly in the space. The acceleration transit systems 2 can drive the micro-power aircraft bodies 1to move, provide energy for the micro-power aircraft bodies 1, and can be used for conducting relay acceleration and stop on the micro-power aircraft bodies 1. According to the micro-power aircraft and system, the electromagnetic acceleration technology is used for aviation logistics, a main power does not need to be additionally installed on the micro-power aircraft, an aviation logistics system is established rapidly in this way, the logistics speed is increased, and the transport cost is lowered.
Description
Technical field
The present invention relates to means of transport field, in particulars relate to a kind of micro power aircraft and system.
Background technology
Electromagnetism speed technology is mainly used in military field, such as magnetic artillery etc. at this stage, and present electromagnetism speed technology is
Reach its maturity.Current logistics transportation instrument, such as aircraft, automobile etc., are all by power engine and energy module and main frame
Put together, a big chunk energy is so accomplished by for transporting electromotor and energy module, especially aircraft, such as
The electromotor and Aviation Fuel of aircraft is accomplished by consuming the substantial amounts of energy with aircraft flight.If electromagnetism speed technology is used
To logistics field, especially for use on aircraft, it will improve the conevying efficiency of aircraft to a certain extent.The present invention is disclosed
Electromagnetism speed technology is used for Air Logistics by a kind of micro power aircraft and system, the technical scheme, and aircraft itself need not
Install main power source additional, set up quick Aviation Logistics, logistics speed will be accelerated, reduce cost of transportation.
The content of the invention
In order to realize setting up quick Aviation Logistics, accelerate logistics speed, reduce the purpose of cost of transportation, the present invention
A kind of micro power aircraft and system are disclosed, and the invention includes micro power aircraft, accelerates transferring system, and micro power aircraft can
To load goods, and can accelerate transferring system that micro power aircraft can be driven to move in space flight, be that micro power flies
The flight of row device provides energy, and micro power aircraft can be carried out relaying acceleration and only be stopped.
Preferably, the micro power aircraft is provided with navigation system, and navigation system can determine micro power aircraft
Particular location, navigates to flight path.
Preferably, the micro power aircraft is provided with and slides wing, slide wing can increase the flight of aircraft away from
From, and slide wing and can be folded, pack up when micro power aircraft is entered accelerates transferring system and slide wing, when micro-
Power aerial vehicle leaves after acceleration transferring system reaches maximum height and launches to slide wing.
Preferably, the micro power aircraft is provided with tuning dynamical system, and tuning dynamical system can coordinate navigation system
System is adjusted to micro power aircraft flight attitude, is controlled the flight path of micro power aircraft, also may be used under special circumstances
Think that micro power aircraft supplements certain energy.
Preferably, the acceleration transferring system is provided with micro power aircraft receiving terminal, the micro power flight of airflight
Device can be entered by micro power aircraft receiving terminal and accelerate transferring system, and micro power aircraft receiving terminal can be stablized micro power and fly
The flight path and flight speed of row device.
Preferably, the acceleration transferring system is provided with transfer distribution control section, and transfer distribution control section can be according to micro-
The concrete needs of power aerial vehicle, carry out accelerating to micro power aircraft, slow down, shunting control.
Preferably, the acceleration transferring system is provided with micro power aircraft outfan, and the micro power after acceleration flies
Row device is flown out by micro power aircraft outfan, the different flight line of different micro power aircraft outfan correspondences.
Preferably, the acceleration transferring system is provided with micro power aircraft input, and the micro power for having loaded goods flies
Row device is entered by micro power aircraft input and accelerates transferring system, by micro power after transfer distribution control section tuning accelerates
Aircraft outfan flies out.
Preferably, the acceleration transferring system is provided with micro power aircraft stoppage in transit end, and having arrived at a station needs the micro- of unloading
Power aerial vehicle is assigned to micro power aircraft stoppage in transit end, the goods in micro power aircraft after being slowed down by transfer distribution control section
Shunting is unloaded at micro power aircraft stoppage in transit end.
Preferably, base of making preparation for dropping is provided between first Transferring Base for accelerating transferring system to be located and the second Transferring Base
Ground, makes preparation for dropping base and breaks down for landing or cause do not have what enough kinetic energy arrived at the destination because of external resistance increase
Micro power aircraft.
By above-mentioned technical proposal, the micro power aircraft and system can be realized setting up quick Aviation Logistics, plus
Fast logistics speed, reduces the purpose of cost of transportation.
Other features and advantages of the present invention will be described in detail in subsequent specific embodiment part.
Description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.Accompanying drawing is for providing to the further of the present invention
Understand, and constitute a part for description, be used for explaining the present invention together with detailed description below, but do not constitute
Limitation of the present invention.
In the accompanying drawings：
Fig. 1 is micro power aircraft and system integral layout schematic diagram；
Fig. 2 is that micro power aircraft and system slide wing operation principle schematic diagram；
Fig. 3 is micro power aircraft and system storing bin part-structure schematic diagram；
Fig. 4 is to accelerate transferring system section layout schematic diagram；
Fig. 5 is base scheme schematic diagram of making preparation for dropping.
Description of reference numerals
1st, micro power aircraft；101st, navigation system；102nd, slide wing；103rd, tuning dynamical system；104th, storing bin；2nd, add
Fast transferring system；2a, the first Transferring Base；2b, base of making preparation for dropping；2c, the second Transferring Base；201st, micro power aircraft is received
End；202nd, transfer distribution control section；203rd, micro power aircraft outfan；204th, micro power aircraft input；205th, fine motion
Power aircraft stoppage in transit end.
Specific embodiment
The specific embodiment of the present invention is described in detail below in conjunction with accompanying drawing.It should be appreciated that this place is retouched
The specific embodiment stated is merely to illustrate and explains the present invention, is not limited to the present invention.
In the present invention, in the case where contrary explanation is not made, the noun of locality for using such as " upper and lower, top, bottom " typically pin
It is for direction shown in the drawings or for each part mutual alignment relation on vertical, vertical or gravity direction
Description word.The noun of locality for using such as " left and right " refers to the left and right orientation in accompanying drawing.
As shown in figure 1, the invention provides a kind of micro power aircraft and system, the invention include micro power aircraft 1,
Accelerate transferring system 2, micro power aircraft 1 load goods, and can accelerate the transferring system 2 can be with space flight
Drive micro power aircraft 1 to move, energy is provided for the flight of micro power aircraft 1, and micro power aircraft 1 can be carried out
Relaying accelerates and only stops.Accelerate transferring system 2 preferably to apply active force using electromagnetic technique to micro power aircraft 1, order about
Micro power aircraft 1 is moved.
As shown in Fig. 2 micro power aircraft 1 is provided with navigation system 101, navigation system 101 can determine that micro power flies
The particular location of row device 1, navigates to its flight path.Micro power aircraft 1 is provided with and slides wing 102, slides wing
102 flying distances that can increase aircraft, and slide wing 102 and can be folded, enter when micro power aircraft 1 plus
Pack up during fast transferring system 2 and slide wing 102, open up when micro power aircraft 1 is left after acceleration transferring system 2 reaches maximum height
Open and slide wing 102, can so increase the flying distance of micro power aircraft 1.Micro power aircraft 1 is provided with tuning dynamical system
System 103, tuning dynamical system 103 can coordinate navigation system 101 to be adjusted 1 flight attitude of micro power aircraft, control
The flight path of micro power aircraft 1, can supplement certain energy for micro power aircraft 1 under special circumstances.Due to adjusting
1 flight attitude of micro power aircraft is only intended to dynamical system 103 to be adjusted, and the dynamic of main power source is provided relative to aircraft
Power part and energy module, the power part and energy module needed for tuning dynamical system 103 are very little.
As shown in figure 3, micro power aircraft 1 is provided with storing bin 104, storing bin 104 is used for shipping goods.Due to fine motion
The electromotor and attached energy module that active force is provided need not be installed on power aircraft 1 additional, this allows for micro power aircraft 1
There are more space planning storing bins 104 so that the effective of micro power aircraft 1 uses space than larger.
As shown in figure 4, accelerating transferring system 2 to be provided with micro power aircraft receiving terminal 201, aerial micro power aircraft
1 can enter acceleration transferring system 2 by micro power aircraft receiving terminal 201, and micro power aircraft receiving terminal 201 can stablize micro-
The flight path and flight speed of power aerial vehicle 1.Transferring system 2 is accelerated to be provided with transfer distribution control section 202, transfer distribution
Control section 202 can be carried out accelerating to micro power aircraft 1, be slowed down according to the concrete needs of micro power aircraft 1, shunting control
System.Transferring system 2 is accelerated to be provided with micro power aircraft outfan 203, the micro power aircraft 1 after acceleration is by micro power
Aircraft outfan 203 flies out, the different flight line of the different correspondences of micro power aircraft outfan 203.Transfer from one department to another in acceleration
System 2 is provided with micro power aircraft input 204, has loaded the micro power aircraft 1 of goods by micro power aircraft input
204 enter acceleration transferring system 2, are flown by micro power aircraft outfan 203 after transfer 202 tuning of distribution control section accelerates
Go out.Accelerate transferring system 2 be provided with micro power aircraft stoppage in transit end 205, arrived at a station need unloading micro power aircraft 1 by
Transfer distribution control section 202 is assigned to micro power aircraft stoppage in transit end 205 after slowing down, and the goods in micro power aircraft 1 is micro-
Unload shunting in power aerial vehicle stoppage in transit end 205.
As shown in figure 5, being provided with standby between the first Transferring Base 2a and the second Transferring Base 2c at acceleration transferring system 2 place
Drop base 2b, makes preparation for dropping base 2b and breaks down for landing or cause do not have enough kinetic energy to reach because of external resistance increase
The micro power aircraft 1 of destination.Make preparation for dropping base 2b set up can increase to the full extent micro power aircraft 1 flight peace
Full reliability.
For the clearer 26S Proteasome Structure and Function for reacting the micro power aircraft and system, presently describe this kind of micro power and fly
The course of work of row device and system, this citing are only the one kind in multiple choices scheme, are not limitations of the present invention.
First, it would be desirable to which freight puts into storing bin 104, micro power aircraft 1 is input into by micro power aircraft
End 204 enters and accelerates transferring system 2, by micro power aircraft outfan 203 after transfer 202 tuning of distribution control section accelerates
Fly out, launch to slide wing 102 when micro power aircraft 1 is left after acceleration transferring system 2 reaches maximum height, can so increase
Plus the flying distance of micro power aircraft 1, tuning dynamical system 103 can coordinate navigation system 101 to micro power aircraft 1 fly
Row attitude is adjusted, and controls the flight path of micro power aircraft 1, can also be micro power aircraft 1 under special circumstances
The certain energy of supplement, after micro power aircraft 1 is close to destination, micro power aircraft 1 is packed up and slides wing 102, then
Entered by micro power aircraft receiving terminal 201 and accelerate transferring system 2, micro power aircraft receiving terminal 201 stablize micro power
The flight path and flight speed of aircraft 1, can be in transfer point according to the difference of 1 load destination of micro power aircraft
Select to unload into micro power aircraft stoppage in transit end 205 with control section 202, it is also possible to select into micro power aircraft outfan
203 continue to repeat to fly, when midway is broken down, it is impossible to which, when reaching original destination, micro power aircraft 1 can be selected nearby
The base 2b that makes preparation for dropping lands, and thus can increased the reliability of whole system to a certain extent.
By above-mentioned technical proposal, the micro power aircraft and system can be realized setting up quick Aviation Logistics, plus
Fast logistics speed, reduces the purpose of cost of transportation.
The preferred embodiment of the present invention is described in detail above in association with accompanying drawing, but, the present invention is not limited to above-mentioned reality
The detail in mode is applied, in the range of the technology design of the present invention, various letters can be carried out to technical scheme
Monotropic type and function integrity, these simple variants and function integrity belong to protection scope of the present invention.
Claims (10)
1. a kind of micro power aircraft and system, it is characterised in that the invention includes micro power aircraft（1）, transfer from one department to another in acceleration
System（2）, micro power aircraft（1）Goods can be loaded, and transferring system can be accelerated in space flight（2）Can drive
Micro power aircraft（1）Motion, is micro power aircraft（1）Flight provides energy, and can be to micro power aircraft（1）Enter
Row relaying accelerates and only stops.
2. a kind of micro power aircraft according to claim 1 and system, it is characterised in that the micro power aircraft
（1）It is provided with navigation system（101）, navigation system（101）The particular location of micro power aircraft 1 is can determine, which is flown
Navigated in path.
3. a kind of micro power aircraft according to claim 1 and system, it is characterised in that the micro power aircraft
（1）It is provided with and slides wing（102）, slide wing（102）The flying distance of aircraft can be increased, wing is slided（102）Can
To be folded, when micro power aircraft（1）Into acceleration transferring system（2）When pack up and slide wing（102）, when micro power flies
Row device（1）Leave acceleration transferring system（2）Launch to slide wing after reaching maximum height（102）.
4. a kind of micro power aircraft according to claim 1 and system, it is characterised in that the micro power aircraft
（1）It is provided with tuning dynamical system（103）, tuning dynamical system（103）Navigation system can be coordinated（101）Micro power is flown
Device（1）Flight attitude is adjusted, and controls micro power aircraft（1）Flight path, can also be fine motion under special circumstances
Power aircraft（1）The certain energy of supplement.
5. a kind of micro power aircraft according to claim 1 and system, it is characterised in that the acceleration transferring system
（2）It is provided with micro power aircraft receiving terminal（201）, the micro power aircraft of airflight（1）Can be by micro power aircraft
Receiving terminal（201）Into acceleration transferring system（2）, micro power aircraft receiving terminal（201）Micro power aircraft can be stablized（1）
Flight path and flight speed.
6. a kind of micro power aircraft according to claim 1 and system, it is characterised in that the acceleration transferring system
（2）It is provided with transfer distribution control section（202）, transfer distribution control section（202）Can be according to micro power aircraft（1）It is concrete
Need, to micro power aircraft（1）Carry out accelerating, slow down, shunting control.
7. a kind of micro power aircraft according to claim 1 and system, it is characterised in that the acceleration transferring system
（2）It is provided with micro power aircraft outfan（203）, the micro power aircraft after acceleration（1）It is defeated by micro power aircraft
Go out end（203）Fly out, different micro power aircraft outfans（203）The different flight line of correspondence.
8. a kind of micro power aircraft according to claim 1 and system, it is characterised in that the acceleration transferring system
（2）It is provided with micro power aircraft input（204）, loaded the micro power aircraft of goods（1）It is defeated by micro power aircraft
Enter end（204）Into acceleration transferring system（2）, distribute control section through transfer（202）By micro power aircraft after tuning acceleration
Outfan（203）Fly out.
9. a kind of micro power aircraft according to claim 1 and system, it is characterised in that the acceleration transferring system
（2）It is provided with micro power aircraft stoppage in transit end（205）, having arrived at a station needs the micro power aircraft of unloading（1）Distributed by transfer
Control section（202）Micro power aircraft stoppage in transit end is assigned to after deceleration（205）, the goods in micro power aircraft 1 is in micro power
Aircraft stoppage in transit end（205）Unload shunting.
10. a kind of micro power aircraft according to claim 1 and system, it is characterised in that the acceleration transferring system
（2）The first Transferring Base being located（2a）With the second Transferring Base（2c）Between be provided with base of making preparation for dropping（2b）, base of making preparation for dropping（2b）
The micro power aircraft broken down for landing（1）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611267853.7A CN106516115A (en) | 2016-12-31 | 2016-12-31 | Micro-power aircraft and system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611267853.7A CN106516115A (en) | 2016-12-31 | 2016-12-31 | Micro-power aircraft and system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106516115A true CN106516115A (en) | 2017-03-22 |
Family
ID=58336482
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611267853.7A Withdrawn CN106516115A (en) | 2016-12-31 | 2016-12-31 | Micro-power aircraft and system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106516115A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101549693A (en) * | 2009-05-07 | 2009-10-07 | 徐林波 | Gravity conveying method, system and tool and application |
| CN101659324A (en) * | 2009-05-05 | 2010-03-03 | 徐林波 | Novel transportation method, and transportation system, tool and application thereof |
| CN105173106A (en) * | 2015-09-18 | 2015-12-23 | 上海长语信息科技有限公司 | External power source electric aircraft aerial platform launching method and device |
-
2016
- 2016-12-31 CN CN201611267853.7A patent/CN106516115A/en not_active Withdrawn
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101659324A (en) * | 2009-05-05 | 2010-03-03 | 徐林波 | Novel transportation method, and transportation system, tool and application thereof |
| CN101549693A (en) * | 2009-05-07 | 2009-10-07 | 徐林波 | Gravity conveying method, system and tool and application |
| CN105173106A (en) * | 2015-09-18 | 2015-12-23 | 上海长语信息科技有限公司 | External power source electric aircraft aerial platform launching method and device |
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| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170322 |