CN108482696A - A kind of landing modes of fixed-wing unmanned plane - Google Patents
A kind of landing modes of fixed-wing unmanned plane Download PDFInfo
- Publication number
- CN108482696A CN108482696A CN201810226414.4A CN201810226414A CN108482696A CN 108482696 A CN108482696 A CN 108482696A CN 201810226414 A CN201810226414 A CN 201810226414A CN 108482696 A CN108482696 A CN 108482696A
- Authority
- CN
- China
- Prior art keywords
- fixed
- unmanned plane
- wing unmanned
- carriage
- track
- 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.)
- Withdrawn
Links
- 238000009434 installation Methods 0.000 claims abstract description 4
- 229920001971 elastomer Polymers 0.000 claims description 4
- 239000004816 latex Substances 0.000 claims description 3
- 229920000126 latex Polymers 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 239000010985 leather Substances 0.000 description 1
Classifications
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
- B64D45/06—Landing aids; Safety measures to prevent collision with earth's surface mechanical
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
A kind of landing modes of fixed-wing unmanned plane belong to fixed-wing unmanned plane and road device field, including two montants and fixed-wing unmanned plane；Two montants fix on the ground vertically, and supporting rack, rope, weight, fixed plate, track and carriage are equipped on montant；The track is transversely mounted on the upper end of montant, and carriage is partly wrapped in outside track；Carriage and supporting rack link together, the inner wall and rail contact of carriage；A piece elastic string is installed on supporting rack, the both ends of elastic string are separately connected two endpoints of supporting rack；There are two bayonet unit and two device for ejecting, two bayonet units to be separately mounted on the end of two wings of fixed-wing unmanned plane for installation on fixed-wing unmanned plane；Device for ejecting is mounted in the wing of fixed-wing unmanned plane, upon receipt of the signals, can be popped up one section of round bar and be connect the structure to form closure with bayonet unit.The landing modes of the fixed-wing unmanned plane of the present invention, are efficiently completed the descent of fixed-wing unmanned plane.
Description
Technical field
A kind of landing modes of fixed-wing unmanned plane belong to fixed-wing unmanned plane and road device field.
Background technology
Traditional fixed-wing unmanned plane landing needs runway to complete the process slowed down, and can occupy a large amount of resource in this way.
It there is also the case where can not landing under particular circumstances, existing fixed-wing unmanned plane landing lacks a kind of efficient landing
Mode.
Invention content
Present invention aim to address the above problems, provide a kind of landing modes of completely new fixed-wing unmanned plane.
A kind of landing modes of fixed-wing unmanned plane, including two montants and fixed-wing unmanned plane；Two montants are perpendicular
It directly fixes on the ground, supporting rack, rope, weight, fixed plate, track and carriage is installed on montant；The track
It is transversely mounted on the upper end of montant, carriage is partly wrapped in outside track, the both ends of track are equipped with bulge-structure, anti-sliding stop
Device skids off track；The carriage is in integrally concave character type structure, and carriage and supporting rack link together, carriage
Inner wall and rail contact, carriage can slide in orbit, and generate certain frictional force with track；The fixed plate peace
At the starting point end of track, the centre of fixed plate is equipped with circular hole；One end of the rope connects runner device, and the other end passes through
Circular hole among fixed plate is connected with weight；The U-shaped structure of support frame as described above is equipped with an elastic string, rubber on supporting rack
The both ends of leather rope are separately connected two endpoints of supporting rack；The elastic string is made with rubber and latex, has elongation
Greatly, the good feature of high tenacity, resilience；The setting distance of two elastic strings is less than the span-width of fixed-wing unmanned plane；
There are two bayonet unit and two device for ejecting, two bayonet units to be separately mounted to fix for installation on the fixed-wing unmanned plane
On the end of two wings of wing unmanned plane；Device for ejecting is mounted in the wing of fixed-wing unmanned plane, upon receipt of the signals,
One section of round bar can be popped up and connect the structure to form closure with bayonet unit.
Further, the elastic string may be replaced by common rope.
When fixed-wing unmanned plane needs landing, by way of being remotely controlled or positioning, make the landing of fixed-wing unmanned plane
By between two supporting racks, the position of carriage and supporting rack is located at the starting point of track one end in course line, fixed-wing nobody
The wing of machine directly knocks elastic string, elastic string elongation is big, under feature that high tenacity, resilience are good, elastic string is slided
Into in bayonet unit, while control terminal sends a signal to fixed-wing unmanned plane pop-up device for ejecting, and elastic string is made to lock in card
In buckle device, fixed-wing unmanned plane drags elastic string, and elastic string drives supporting rack and carriage, carriage to slide in orbit
Weight is dragged by rope while dynamic, the pulling force that weight generates runner device acts on fixation by supporting rack and elastic string
On wing unmanned plane, the frictional force that carriage and track generate is acted on by supporting rack and elastic string on fixed-wing unmanned plane,
The process that fixed-wing unmanned plane slows down is set to accelerate, until the end that square body slides into slideway is blocked, fixed-wing unmanned plane is completed
The process of landing.
A kind of landing modes of completely new fixed-wing unmanned plane of offer of the present invention, are efficiently completed fixed-wing unmanned plane
Descent.
Description of the drawings
Fig. 1 is the structural schematic diagram of fixed-wing unmanned plane；Structure when Fig. 2 is fixed-wing unmanned plane and supporting rack contact
Schematic diagram；Fig. 3 is fixed-wing unmanned plane and the structural schematic diagram in elastic string contact process；Fig. 4 is that fixed-wing unmanned plane is completed
Structural schematic diagram when landing；Fig. 5 is the structural schematic diagram of two montants；Fig. 6 be carriage, rope, fixed plate, track and
The combining structure schematic diagram of supporting rack.
In figure：1- montants, 11- supporting racks, 12- elastic strings, 13- carriages, 14- tracks, 15- ropes, 16- weights,
17- fixed plates, 2- fixed-wings unmanned plane, 21- bayonet units, 22- device for ejecting, 221- round bars.
Specific implementation mode
The present invention will be further described below in conjunction with the accompanying drawings：A kind of landing modes of fixed-wing unmanned plane, including two
Montant 1 and fixed-wing unmanned plane 2；Two montants perpendicular 1 directly fix on the ground, and supporting rack 11, rope are equipped on montant 1
Son 15, weight 16, fixed plate 17, track 14 and carriage 13；The track 14 is transversely mounted on the upper end of montant 1, in-orbit
Carriage 13 is partly wrapped in outside road 14, the both ends of track 14 are equipped with bulge-structure, prevent carriage 13 from skidding off track 14；Institute
It is in concave character type structure that it is whole, which to state carriage 13, and carriage 13 and supporting rack 11 link together, the inner wall of carriage 13
It is contacted with track 14, carriage 13 can slide on track 14, and generate certain frictional force with track 14；The fixed plate
17 are mounted at the starting point end of track 14, and the centre of fixed plate 17 is equipped with circular hole；One end of the rope 15 connects runner device
13, the other end passes through circular hole and the connection of weight 16 among fixed plate 17；11 U-shaped structure of support frame as described above, in supporting rack 11
On an elastic string 12 is installed, the both ends of elastic string 12 are separately connected two endpoints of supporting rack 11；The elastic string 12 is
It is made with rubber and latex, has the characteristics that elongation is big, high tenacity, resilience are good；The setting of two elastic strings 12
Distance is less than the span-width of fixed-wing unmanned plane 3；There are two bayonet unit 21 and two for installation on the fixed-wing unmanned plane 2
Device for ejecting 22, two bayonet units 21 are separately mounted on the end of two wings of fixed-wing unmanned plane 2；The pop-up dress
It sets 22 to be mounted in the wing of fixed-wing unmanned plane 2, upon receipt of the signals, one section of round bar 221 and bayonet unit 21 can be popped up
Connection forms the structure being closed.
When fixed-wing unmanned plane 3 needs landing, by way of being remotely controlled or positioning, make the drop of fixed-wing unmanned plane 2
Course line is fallen to pass through between two supporting racks 11, the position of carriage 13 and supporting rack 11 is located at the starting point of 14 one end of track,
The wing of fixed-wing unmanned plane 2 directly knocks elastic string 12, the elongation of elastic string 12 is big, high tenacity, resilience are good
Under feature, elastic string 12 slides into bayonet unit 21, while control terminal sends a signal to the pop-up pop-up dress of fixed-wing unmanned plane 2
22 are set, elastic string 12 is made to lock in bayonet unit 21, fixed-wing unmanned plane 2 drags elastic string 12, and elastic string 12 drives support
Frame 11 and carriage 13, carriage 13 drag weight 16 while being slided on track 14 by rope 15, and weight 16 is right
The pulling force that runner device 13 generates is acted on by supporting rack 11 and elastic string 12 on fixed-wing unmanned plane 2,13 He of carriage
The frictional force that track 14 generates is acted on by supporting rack 11 and elastic string 12 on fixed-wing unmanned plane 2, and fixed-wing unmanned plane 2 is made
The process of deceleration is accelerated, and until the end that square body 13 slides into slideway 14 is blocked, fixed-wing unmanned plane 2 completes the mistake of landing
Journey.
Claims (4)
1. a kind of landing modes of fixed-wing unmanned plane, it is characterised in that：Including two montants（1）With fixed-wing unmanned plane（2）；
Two montants are perpendicular（1）It directly fixes on the ground, in montant（1）On supporting rack is installed（11）, rope（15）, weight
（16）, fixed plate（17）, track（14）And carriage（13）；The track（14）It is transversely mounted on montant（1）Upper end,
Track（14）Partly it is wrapped in carriage outside（13）, track（14）Both ends be equipped with bulge-structure, prevent carriage（13）It is sliding
Errant（14）；The carriage（13）Whole is in concave character type structure, carriage（13）And supporting rack（11）It is connected to one
It rises, carriage（13）Inner wall and track（14）Contact, carriage（13）It can be in track（14）Upper sliding, and and track
（14）Generate certain frictional force；The fixed plate（17）Mounted on track（14）Starting point end at, fixed plate（17）Centre
Equipped with circular hole；The rope（15）One end connect runner device（13）, the other end is across fixed plate（17）Intermediate circular hole and
Weight（16）Connection；Support frame as described above（11）On an elastic string is installed（12）, elastic string（12）Both ends be separately connected branch
Support（11）Two endpoints；Two elastic strings（12）Setting distance be less than fixed-wing unmanned plane（3）Span-width；
The fixed-wing unmanned plane（2）There are two bayonet units for upper installation（21）With two device for ejecting（22）, two bayonet units
（21）It is separately mounted to fixed-wing unmanned plane（2）Two wings end on；The device for ejecting（22）Mounted on fixed-wing
Unmanned plane（2）Wing in, upon receipt of the signals, one section of round bar can be popped up（221）With bayonet unit（21）Connection is formed and is closed
The structure of conjunction.
2. a kind of landing modes of fixed-wing unmanned plane according to claim 1, it is characterised in that：Supporting rack（11）In U
Type structure.
3. a kind of landing modes of fixed-wing unmanned plane according to claim 1, it is characterised in that：The elastic string（12）
It is made with rubber and latex, has the characteristics that elongation is big, high tenacity, resilience are good.
4. a kind of landing modes of fixed-wing unmanned plane according to claim 1, it is characterised in that：The elastic string（12）
It also can be replaced common rope.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810226414.4A CN108482696A (en) | 2018-03-19 | 2018-03-19 | A kind of landing modes of fixed-wing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810226414.4A CN108482696A (en) | 2018-03-19 | 2018-03-19 | A kind of landing modes of fixed-wing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108482696A true CN108482696A (en) | 2018-09-04 |
Family
ID=63318411
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810226414.4A Withdrawn CN108482696A (en) | 2018-03-19 | 2018-03-19 | A kind of landing modes of fixed-wing unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108482696A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110001935A (en) * | 2019-05-07 | 2019-07-12 | 广州中国科学院沈阳自动化研究所分所 | A kind of unmanned plane is from active platform landing auxiliary device |
-
2018
- 2018-03-19 CN CN201810226414.4A patent/CN108482696A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110001935A (en) * | 2019-05-07 | 2019-07-12 | 广州中国科学院沈阳自动化研究所分所 | A kind of unmanned plane is from active platform landing auxiliary device |
| CN110001935B (en) * | 2019-05-07 | 2024-05-17 | 广州中国科学院沈阳自动化研究所分所 | Unmanned aerial vehicle takes off and land auxiliary device from initiative platform |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2440574A (en) | Aircraft barrier | |
| US2450328A (en) | Aircraft barrier | |
| CN105758609A (en) | Bridge pier collision impact test device based on ship anti-collision device and test method of test device | |
| CN206740961U (en) | A kind of radar lift adjustment and fixing device | |
| CN108482696A (en) | A kind of landing modes of fixed-wing unmanned plane | |
| CN105920841B (en) | Two safety structure of coupling type | |
| CN107863722A (en) | A kind of preliminary leading rope directly passes through formula releasing pulley | |
| CN205872041U (en) | Aerial passenger device seat range line mechanism | |
| CN105799729B (en) | Sliding train in inclined lane protector and its application method | |
| CN104890852A (en) | Hot air balloon experience device | |
| CN209274924U (en) | A kind of ejector coaster brake buffer unit | |
| CN105523191B (en) | Unmanned plane recycling network | |
| CN108454872A (en) | A kind of landing modes of the fixed-wing unmanned plane with weight | |
| CN204715247U (en) | Ascending/decending expressway tol lcollection is anti-rushes lever apparatus | |
| CN108408073A (en) | A kind of fixed-wing unmanned plane landing modes | |
| CN106401446A (en) | Telescopic screen window | |
| CN108482671A (en) | A kind of landing modes of unmanned plane | |
| CN101964502A (en) | Method for spreading initial guide rope with remote control fixed wing aircraft | |
| CN205524983U (en) | Push -button aircraft system | |
| CN205365560U (en) | Rubber wheel vehicle sports car protector | |
| CN108750883A (en) | Elevator with weightless ensuring equipment | |
| CN100529710C (en) | Method and system for speeding up combination of slope ejection for experiment of vehicle collision | |
| CN205327436U (en) | Carrier -borne aircraft elasticity tail hook | |
| CN208266736U (en) | A kind of high speed limit for height system | |
| US2927753A (en) | Aerial toy |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180904 |