CN109305381A - A kind of quick power-assisted launching apparatus of unmanned plane cluster - Google Patents
A kind of quick power-assisted launching apparatus of unmanned plane cluster Download PDFInfo
- Publication number
- CN109305381A CN109305381A CN201811273488.XA CN201811273488A CN109305381A CN 109305381 A CN109305381 A CN 109305381A CN 201811273488 A CN201811273488 A CN 201811273488A CN 109305381 A CN109305381 A CN 109305381A
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- Prior art keywords
- unmanned plane
- launching apparatus
- assisted
- quick power
- cluster
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- 238000004146 energy storage Methods 0.000 claims abstract description 12
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 4
- 239000003990 capacitor Substances 0.000 claims description 4
- 238000005253 cladding Methods 0.000 claims description 4
- 229910052744 lithium Inorganic materials 0.000 claims description 4
- 238000012544 monitoring process Methods 0.000 claims description 3
- 238000004806 packaging method and process Methods 0.000 claims description 3
- 150000001875 compounds Chemical class 0.000 abstract description 3
- 230000010354 integration Effects 0.000 abstract 1
- 230000032258 transport Effects 0.000 description 8
- 238000000034 method Methods 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000003721 gunpowder Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 229910000976 Electrical steel Inorganic materials 0.000 description 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000010338 mechanical breakdown Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000037452 priming Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Classifications
-
- 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—Ground or aircraft-carrier-deck installations for launching aircraft
- B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
The invention discloses a kind of quick jato units of unmanned plane cluster of TEU (Twenty-foot Equivalent Unit), belong to the jato unit in the stage of taking off.When applied to extensive fixed-wing unmanned plane cluster work compound under the conditions of limited environment it is motor-driven, quickly take off.It mainly include ISO container (1), unmanned plane (2), the storage rack (3) for storing unmanned plane, the linear motor (5) for emitting unmanned plane, mobile high-energy-density energy-storage units (6), motor driver (7) and console (8) composition.The present invention realizes the integration of the storage of unmanned plane, transport, transmitting, can reach operating area by the apparatuss of transport fast reserve such as vehicle, ship and realize the quick continuous transmitting of unmanned plane, quickly form cluster, quickly carry out work compound task.
Description
Technical field
The invention belongs to aircraft power-assisted launching apparatus field, it is especially a kind of when being applied to unmanned plane cluster detect operation without
Man-machine rapid fire jato unit.
Background technique
With the fast development and civil field application popularization of unmanned air vehicle technique, the cost of unmanned plane is significantly dropped
Low, the application of unmanned plane Clustering has also obtained faster development, and cluster work compound tends to performance one-plus-one and is greater than two
Effect, the collaboration of unmanned plane cluster is with a wide range of applications in fields such as detection, operation, relayed communications, monitorings, in economy
Property, the advantages of also showing far superior to traditional means in terms of technical, convenience.In some applications, often face
Happen suddenly job requirements, it is desirable that unmanned plane cluster can quickly reach scene and dispose, such as earthquake centre area video, geographical letter after earthquake
Breath feedback, marine casualty personnel search, polluted information monitors etc., it is limited to unmanned plane voyage, unmanned plane has from a distance
It takes off without actuality and timeliness in the place of takeoff condition.
Traditional scheme first is that by apparatuss of transport such as car and boat by elastic, pneumatically or hydraulically etc. mechanical transmitter is transported to
Target area realizes that the power-assisted of unmanned plane is taken off by mechanical transmitter.Mechanical transmitter needs air compressor machine, gas cylinder, gas
The elastic strainer of cylinder or hydraulic cylinder, pulley speed increasing mechanism or complexity, weight weight big with volume, mechanical breakdown is more, emits
The disadvantages of operation interval time is long, and have certain requirement to the basis of transmitter site, space, it is often also needed when marching into the arena and arranging
A large amount of time is wanted, when Launch Operation also has biggish noise, and concealment is poor.After the completion of every sortie transmitting, often
It takes a long time and carries out energy storage, the flow charts such as resets, first and last sortie interval time of going up to the air is too long when group operation, does not have
The ability of standby quick multi rack time transmitting, further limits the operation time and range of cluster.Gunpowder help-fly is also common one
Length when the advantages of kind mode, gunpowder help-fly is rapid transmitting, transmission interval, but priming system has certain risk, and sends out
There is biggish acoustooptical effect when penetrating operation, concealment is poor.
Chinese patent CN106394924 proposes a kind of permanent-magnetism linear motor type electromagnetic launch technology of unmanned aerial vehicle device, this electromagnetism bullet
Unmanned plane is accelerated to takeoff speed using linear motor by emitter, and power-assisted is taken off.But these devices are in transport standardization, unmanned plane
Storage, size, energy storage, the unmanned unit frequency of transmitting etc. also have biggish deficiency.
Summary of the invention
The technical problem to be solved by the present invention is
A kind of quick power-assisted launching apparatus of unmanned plane cluster is provided, can not only improve unmanned plane multi rack time storage capacity,
The quick power-assisted launching apparatus structural compactness of unmanned plane cluster, unmanned plane emission rate and frequency, moreover it is possible to realize that power-assisted is taken off dress
The standardization set transports and improves the rodability and capability of fast response, timeliness of the quick power-assisted launching apparatus of unmanned plane cluster
Property.
In order to solve the above technical problems, technical solution of the present invention has the beneficial effect that with what is reached
The quick power-assisted launching apparatus of unmanned plane cluster specifically includes: linear motor, takes off multi rack time nothing for quick power-assisted
Man-machine takes off；Energy-storage units, for providing electric energy for linear motor；Driving is used to be linear motor as current inverter
The power supply of the waveform needed is provided；Console, for monitoring and operating the quick power-assisted launching apparatus of the unmanned plane cluster；It is described straight
Line motor is arranged, the quick power-assisted of unmanned plane cluster parallel using long primary, short secondary structure using more linear motors
Launching apparatus further includes storage rack, springboard, shelf tray and chain delivery structure of the storage rack with storage unmanned plane, institute
It states shelf tray and multi rack time unmanned plane is sequentially transmitted close to the position of springboard by the chain delivery structure, it will by springboard
Unmanned plane is transferred to linear motor power-assisted by the shelf tray of storage rack and takes off.Unmanned plane is stored using storage rack and wheeled construction
Transhipment improves the storage capacity of multi rack time unmanned plane, enables unmanned plane quickly to reach the erect-position that takes off, ensure that unmanned plane
The rapidity taken off；Using more directors primary short secondary linear electric motor in parallel axis depth direction size is further decreased, realizes
Device is compact, integrated level is high, noise is small, high reliablity, Launch Operation interval time are short.
The linear motor is taken off the angle of departure of multi rack time unmanned plane with reaching for quick power-assisted using being in tilted layout
Degree.
The linear motor has the pallet for loading unmanned plane, and pallet and linear motor are rigidly connected, and is used for nobody
It lifting when machine takes off and draws.
The quick power-assisted launching apparatus of the unmanned plane cluster, further includes container, and the container can be TEU (Twenty-foot Equivalent Unit),
Container top cladding plate described in packaging has opening, can be slidable skylight, outlet when taking off as unmanned plane.It is described
The quick power-assisted launching apparatus of unmanned plane cluster be arranged in the container, realize transport standardization, improve unmanned plane collection
Concealment, rodability and the timeliness of the quick power-assisted launching apparatus of group.
The energy-storage units are double cell form, the lithium battery of super capacitor and high-energy density with high power density
Combination, meet the power demand of repid discharge and the energy requirement of multi rack time unmanned plane transmitting.
This linear motor for the quick power-assisted launching apparatus of unmanned plane cluster is using long primary, short secondary knot
Structure, and arrange and improve tractive force, reduce axis depth direction length that there is structural compactness parallel using more linear motors.
Detailed description of the invention
A specific embodiment of the invention is described in further details with reference to the accompanying drawing:
Fig. 1 is outside drawing of the present invention
Fig. 2 is state when apparatus of the present invention unmanned plane flies out out of TEU (Twenty-foot Equivalent Unit)
Fig. 3 is internal structure chart in present invention storage and transport
Fig. 4 is the state that first unmanned plane reaches a standby for takeoff of taking off
Fig. 5 is during first unmanned plane takes off and the second frame unmanned plane is transported to the filling for position of taking off
Fig. 6 is linear motor three-dimensional structure view
Fig. 7 is linear motor cross-sectional view, i.e. the cross section, A-A of Fig. 6
Fig. 8 is the arrangement of storage and travel position unmanned plane in storage rack
Fig. 9 is that first unmanned plane wheel produces the state after storage rack
1 it is TEU (Twenty-foot Equivalent Unit) in attached drawing, 2 be unmanned plane, 3 be storage rack, 4 be springboard, 5 be linear motor, 6 is energy storage list
Member, 7 be driving, 8 be console, 9 be unmanned plane pallet, 10 be motor stator, 11 be electric motor stand, 12 be motor for the first time
Grade, 13 be motor second subprime, 14 be motor third it is secondary, 15 be draw hook, 16 be motor third it is primary, 17 be motor second
Primary, 18 are that motor third is primary.
Specific embodiment
Specific implementation of the invention is described further with reference to the accompanying drawing:
As shown in Figure 1, shape of the present invention is TEU (Twenty-foot Equivalent Unit) 1, can be transported by apparatuss of transport such as car and boat；As shown in Figure 2
The top cladding plate of TEU (Twenty-foot Equivalent Unit) 1 has slidable skylight, and unmanned plane 2 is flown out by the skylight and completes to go up to the air, the skylight
Also other hatch frames be can be replaced, there should be wing-folding function for the be above standard unmanned plane of container width of the span
Can, wing is unfolded after the TEU (Twenty-foot Equivalent Unit) 1 that flies out；Structure inside TEU (Twenty-foot Equivalent Unit) 1 is arranged as shown in figure 3, the present invention exists
Internal state when storage and transport as shown in figure 3, unmanned plane is stored on the shelf tray of storage rack 3, press by linear motor
According to the inclined arrangement of the best take-off angle of unmanned plane.It is illustrated in figure 4 state when unmanned plane standby for takeoff, at this time unmanned seat in the plane
In on unmanned plane pallet 9, unmanned plane lifting lever is tangled by draw hook 15.Operator's remote control sends the finger that takes off in console 8
It enables, the direct current energy for being stored in energy-storage units 6 is sent after driving 7 inversion modulation waveforms to linear electric motor primary 16,17 and 18.
Energy-storage units 6 be super capacitor and lithium battery group at double electric forms, super capacitor guarantees discharge power, lithium battery
Guarantee that stored electric energy can satisfy taking off at least ten sortie unmanned planes as main energetic storage equipment, is deposited in storage rack 3
The unmanned plane of storage all charge again after the completion by transmitting.The state being illustrated in figure 5 in first unmanned plane emission process, this
When the second frame unmanned plane started to be transported to the erect-position that takes off from the freight carrier of storage rack 3.When unmanned plane accelerates to takeoff speed
Afterwards, linear motor 5 is braked, and unmanned plane pallet 9 is drawn and is returned to position when lower end is taken off, prepare to the second frame without
It is man-machine to be emitted.
It is illustrated in figure 6 the three-dimensional structure view of linear motor 5, is illustrated in figure 7 the cross section view of linear motor 5, directly
Line motor 5 is primary by electric motor stand 11, first grade 12 of motor, motor second subprime 13, motor third secondary 14, motor third
16, the second primary of motor 17, motor third primary 18 etc. form.Primary iron core is formed by silicon steel plate stacking, using slotless winding
Structure, secondary are aluminium sheet.Unmanned plane pallet 9 and motor secondary are rigidly connected, and are connected in the form of sliding rail with the sliding of electric motor stand 11
It connects.
It is as shown in Figure 8, Figure 9 rotation process of the unmanned plane in storage rack 3, unmanned plane is placed on shelf tray, goods
Rack and support device realizes the displacement of unmanned plane by sprocket wheel or the displacement of other chain delivery structure drivens.A,B,C,D,E,F,G,H,
M, N is the unmanned plane being stored in storage rack 3, and unmanned plane realizes that wheel goes to jump in such a way that ranks are stacked with displaced counter-clockwise
Board position, Fig. 8 state are the transport and storage state before unmanned plane transmitting, and Fig. 9 is after first unmanned plane A wheel produces storage rack
State, unmanned plane B, C, D, E, F, G, H, M, N successively take turns the position gone in Fig. 8 where unmanned plane A, B, C, D, E, F, G, H, M
It sets.
Claims (7)
1. a kind of quick power-assisted launching apparatus of unmanned plane cluster, comprising:
Unmanned plane；
Linear motor takes off multi rack time unmanned plane for quick power-assisted；
Energy-storage units, for providing electric energy for linear motor；
Driving, as current inverter, for provided for the linear motor needs waveform power supply；
Console, for monitoring and operating the quick power-assisted launching apparatus of the unmanned plane cluster；
It is characterized in that, the quick power-assisted launching apparatus of unmanned plane cluster further includes storage rack, springboard, the storage rack has
The shelf tray and chain delivery structure of unmanned plane are stored, the shelf tray for being loaded with unmanned plane relies on the chain delivery knot
Multi rack time unmanned plane is sequentially transmitted close to the position of springboard by structure, is shifted unmanned plane by the shelf tray of storage rack by springboard
It takes off to linear motor power-assisted.
2. the quick power-assisted launching apparatus of unmanned plane cluster according to claim 1, which is characterized in that the linear motor inclines
Tiltedly arrangement.
3. the quick power-assisted launching apparatus of unmanned plane cluster according to claim 1, which is characterized in that the straight-line electric equipment
There is the pallet for loading unmanned plane, pallet and linear motor are rigidly connected.
4. the quick power-assisted launching apparatus of unmanned plane cluster according to claim 1, which is characterized in that further include standard packaging
Case, the standard container roof cladding plate have hatch frame, outlet when taking off as unmanned plane, the unmanned plane cluster
Quick power-assisted launching apparatus is arranged in the TEU (Twenty-foot Equivalent Unit).
5. the quick power-assisted launching apparatus of unmanned plane cluster according to claim 4, which is characterized in that the standard packaging
Box top hatch frame is with the skylight slidably opened.
6. a kind of energy-storage units for the quick power-assisted launching apparatus of unmanned plane cluster described in any one of claims 1 to 5,
It is characterized in that, the energy-storage units are double cell form, the energy-storage units are made of super capacitor and lithium battery, are met
The energy requirement of power demand and multi rack time unmanned plane transmitting of repid discharge.
7. a kind of TEU (Twenty-foot Equivalent Unit) for the quick power-assisted launching apparatus of unmanned plane cluster as claimed in claim 4, feature exist
In the standard container roof cladding plate has hatch frame, and the outlet when hatch frame takes off as unmanned plane is described
The quick power-assisted launching apparatus of unmanned plane cluster be arranged in the TEU (Twenty-foot Equivalent Unit).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811273488.XA CN109305381A (en) | 2018-10-30 | 2018-10-30 | A kind of quick power-assisted launching apparatus of unmanned plane cluster |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811273488.XA CN109305381A (en) | 2018-10-30 | 2018-10-30 | A kind of quick power-assisted launching apparatus of unmanned plane cluster |
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| Publication Number | Publication Date |
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| CN109305381A true CN109305381A (en) | 2019-02-05 |
Family
ID=65222110
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811273488.XA Pending CN109305381A (en) | 2018-10-30 | 2018-10-30 | A kind of quick power-assisted launching apparatus of unmanned plane cluster |
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| Country | Link |
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| CN (1) | CN109305381A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110887572A (en) * | 2019-12-02 | 2020-03-17 | 中国船舶工业系统工程研究院 | Temperature measurement-based boss device for inversion of solar radiation |
| CN111717408A (en) * | 2020-06-29 | 2020-09-29 | 山东科技大学 | Marine launching platform capable of bearing multiple unmanned aerial vehicles |
| CN112572817A (en) * | 2021-01-25 | 2021-03-30 | 南京航空航天大学 | Continuous automatic ejection device for fixed-wing unmanned aerial vehicle and control method thereof |
| CN114162483A (en) * | 2021-12-31 | 2022-03-11 | 安徽博微长安电子有限公司 | Unmanned aerial vehicle's storage and conveyer |
| CN114460962A (en) * | 2021-12-24 | 2022-05-10 | 合肥科技职业学院 | Unmanned aerial vehicle cluster cooperative control system |
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| CN108487735A (en) * | 2018-05-07 | 2018-09-04 | 西北工业大学 | A kind of underground intelligent garage based on the transmission of roller chain formula self-oscillate position |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110887572A (en) * | 2019-12-02 | 2020-03-17 | 中国船舶工业系统工程研究院 | Temperature measurement-based boss device for inversion of solar radiation |
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| CN111717408A (en) * | 2020-06-29 | 2020-09-29 | 山东科技大学 | Marine launching platform capable of bearing multiple unmanned aerial vehicles |
| CN112572817A (en) * | 2021-01-25 | 2021-03-30 | 南京航空航天大学 | Continuous automatic ejection device for fixed-wing unmanned aerial vehicle and control method thereof |
| CN112572817B (en) * | 2021-01-25 | 2022-05-24 | 南京航空航天大学 | Continuous automatic ejection device for fixed-wing unmanned aerial vehicle and control method thereof |
| CN114460962A (en) * | 2021-12-24 | 2022-05-10 | 合肥科技职业学院 | Unmanned aerial vehicle cluster cooperative control system |
| CN114162483A (en) * | 2021-12-31 | 2022-03-11 | 安徽博微长安电子有限公司 | Unmanned aerial vehicle's storage and conveyer |
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