CN106081125A - A kind of parachute construction of unmanned plane - Google Patents
A kind of parachute construction of unmanned plane Download PDFInfo
- Publication number
- CN106081125A CN106081125A CN201610709369.9A CN201610709369A CN106081125A CN 106081125 A CN106081125 A CN 106081125A CN 201610709369 A CN201610709369 A CN 201610709369A CN 106081125 A CN106081125 A CN 106081125A
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- unmanned plane
- steering wheel
- parachute
- velcro
- fuselage
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- 238000010276 construction Methods 0.000 title claims abstract description 34
- 238000009434 installation Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 26
- 108010066278 cabin-4 Proteins 0.000 description 6
- 230000037237 body shape Effects 0.000 description 4
- 239000006185 dispersion Substances 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005259 measurement Methods 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
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
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Abstract
The present invention discloses the parachute construction of a kind of unmanned plane, including unmanned plane body, parachute and steering wheel, it is provided with cabin and hatch door on described unmanned plane body, described unmanned plane body and hatch door are articulated and connected, it is provided with through hole between described cabin and hatch door, it is provided with steering wheel on described steering wheel, described hatch door is spacing by steering wheel, it is provided with the first VELCRO on described unmanned plane body, gathering sill, second VELCRO and coupler body, described parachute is connected with connection rope, described connection rope passes sequentially through through hole, first VELCRO, gathering sill, second VELCRO and coupler body in cabin above unmanned plane body；The parachute construction using effect of this unmanned plane is good.
Description
Technical field
The present invention relates to the parachute construction of a kind of unmanned plane.
Background technology
UAV is called for short " unmanned plane ", is to utilize radio robot and the presetting apparatus provided for oneself to handle
The most manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus is installed.On ground, naval vessels or
Machine tool remote control station personnel by the equipment such as radar, it be tracked, position, remote control, remote measurement and Digital Transmission.Can be at radio
Take off as conventional airplane under remote control or launch with booster rocket, it is possible to being taken to by machine tool and throw in flight in the air.Reclaim
Time, available mode automatic Landing as conventional airplane landing mission, it is possible to reclaimed by remote control parachute or block.Can
Repetitiousness uses repeatedly.Be widely used in aerial reconnaissance, monitor, communicate, antisubmarine, electronic interferences and taking photo by plane.
Current most unmanned plane all uses parachute, but current parachute construction using effect is the best, difficult
To meet the demand of unmanned plane fan.
Summary of the invention
The technical problem to be solved in the present invention is to provide the parachute construction of the good unmanned plane of a kind of using effect.
For solving the problems referred to above, the present invention adopts the following technical scheme that
The parachute construction of a kind of unmanned plane, including unmanned plane body, parachute and steering wheel, described unmanned plane body is provided with
Cabin and hatch door, described unmanned plane body and hatch door are articulated and connected, and are provided with through hole, described steering wheel between described cabin and hatch door
On be provided with steering wheel, described hatch door is spacing by steering wheel, described unmanned plane body is provided with the first VELCRO, gathering sill, the
Two VELCRO and coupler body, described parachute be connected with connection rope, described connection rope pass sequentially through through hole, the first VELCRO, gathering sill,
Second VELCRO and coupler body in cabin above unmanned plane body.
As preferably, described unmanned plane body includes fuselage, host wing, tailplane, vertical tail, motor and reception
Machine, described gathering sill is positioned at fuselage tail end, and described first VELCRO is positioned at fuselage lower surface, and described second VELCRO is positioned at vertically
The side of empennage, can play good guide effect, is possible to prevent parachute to connect rope in use and strikes vertical tail.
As preferably, described coupler body is positioned at fuselage upper surface, and described coupler body is provided with 4, described coupler body rectangular array
Distribution, described connection rope includes main rope and branch line, and described branch line is provided with 4, and described branch line is connected with coupler body respectively, works as fall
Umbrella 4 branch lines in use that fall constitute triangle body shape, are possible not only to play the effect of outstanding dispersion stress, but also can carry
Rise the unmanned plane body stability when landing.
As preferably, described steering wheel is embedded in fuselage lower surface, Stability Analysis of Structures, connects reliable, and does not results in air
Resistance.
As preferably, described through hole is that triangular shape is arranged, and connects rope and is close on the angle of through hole, have certain guiding and
Locating effect.
As preferably, parallel with vertical tail in the bottom surface of described gathering sill, can play good guide effect, permissible
Prevent from the balance of unmanned plane body is caused large effect.
As preferably, described fuselage being provided with installing hole, described coupler body inserts in installing hole, and described coupler body glues with fuselage
Close, Stability Analysis of Structures, connect reliable.
As preferably, described steering wheel removably connects with steering wheel, user can be facilitated to install and change.
As preferably, described steering wheel and steering wheel are provided with 2, it is provided that two spacing stress points so that spacing more
Add stable.
As preferably, described first VELCRO and the second VELCRO are all fixing with fuselage to be connected, and Stability Analysis of Structures, connection can
Lean on, be possible to prevent unmanned plane body the first VELCRO and second VELCRO in flight course to drop.
The invention have the benefit that compared with the parachute construction of traditional unmanned plane, by employ through hole, first
VELCRO, gathering sill, the second VELCRO and coupler body preset the movement locus connecting rope, it is therefore prevented that when using parachute
Connecting rope to strike unmanned plane body and cause unmanned plane body disequilibrium, using effect is good, and success rate is high, adds use
Steering wheel and steering wheel control the unlatching of hatch door, compared with the parachute construction of traditional unmanned plane, have more controllability, additionally,
Unmanned plane body includes fuselage, host wing, tailplane, vertical tail, motor and receiver, and gathering sill is positioned at fuselage tail
End, the first VELCRO is positioned at unmanned plane body lower surface, and the second VELCRO is positioned at the side of vertical tail, can play good
Guide effect, is possible to prevent parachute to connect rope in use and strikes vertical tail, and coupler body is positioned at fuselage upper surface, and coupler body sets
Be equipped with 4, coupler body rectangular array be distributed, connect rope include main rope and branch line, branch line is provided with 4, branch line respectively with hook
Body connects, and when parachute 4 branch lines in use constitute triangle body shape, is possible not only to play the effect of outstanding dispersion stress,
But also the unmanned plane body stability when landing can be promoted, steering wheel is embedded in fuselage lower surface, Stability Analysis of Structures, and connection can
Leaning on, and do not result in air drag, through hole is that triangular shape is arranged, and connects rope and is close on the angle of through hole, has certain leading
To and locating effect, paralleling with vertical tail in the bottom surface of gathering sill, can play good guide effect, be possible to prevent nothing
The balance of man-machine body causes large effect, and fuselage is provided with installing hole, and coupler body inserts in installing hole, coupler body and fuselage
Bonding, Stability Analysis of Structures, connect reliable, steering wheel removably connects with steering wheel, user can be facilitated to install and change, steering wheel and rudder
Machine is provided with 2, it is provided that two spacing stress points so that spacing more stable, the first VELCRO and the second VELCRO
All fixing with fuselage is connected, Stability Analysis of Structures, connects reliable, be possible to prevent unmanned plane body in flight course the first VELCRO with
Second VELCRO drops.
Accompanying drawing explanation
For the technical scheme being illustrated more clearly that in the embodiment of the present invention, in embodiment being described below required for make
Accompanying drawing be briefly described, it should be apparent that, below describe in accompanying drawing be only some embodiments of the present invention, for
From the point of view of those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain other according to these accompanying drawings
Accompanying drawing.
Fig. 1 is the structural representation of the unmanned plane body of the parachute construction of a kind of unmanned plane of the present invention；
Fig. 2 is the bottom surface partial structurtes schematic diagram of the fuselage of the parachute construction of a kind of unmanned plane of the present invention；
Fig. 3 is the partial structurtes schematic diagram of the fuselage tail end of the parachute construction of a kind of unmanned plane of the present invention；
Fig. 4 is the partial top view of the unmanned plane body of the parachute construction of a kind of unmanned plane of the present invention；
Fig. 5 is the structural representation in the cabin of the parachute construction of a kind of unmanned plane of the present invention.
Detailed description of the invention
Embodiment 1
As Figure 1-5, the parachute construction of a kind of unmanned plane, including unmanned plane body 1, parachute 2 and steering wheel 3, described nothing
Being provided with cabin 4 and hatch door 5 on man-machine body 1, described unmanned plane body 1 and hatch door 5 are articulated and connected, described cabin 4 and hatch door 5
Between be provided with through hole 6, described steering wheel 3 is provided with steering wheel 7, described hatch door 5 is spacing by steering wheel 7, described unmanned plane body 1
On be provided with the first VELCRO 8, gathering sill the 9, second VELCRO 10 and coupler body 11, described parachute 2 be connected with connection rope 12, described
Connect rope 12 and pass sequentially through through hole the 6, first VELCRO 8, gathering sill the 9, second VELCRO 10 and coupler body 11 in cabin 4 around nothing
Above man-machine body 1, compared with the parachute construction of traditional unmanned plane, by employing through hole the 6, first VELCRO 8, guiding
Groove the 9, second VELCRO 10 and coupler body 11 preset the movement locus connecting rope 12, it is therefore prevented that when using parachute 2 even
Splicing 12 strikes unmanned plane body 1 and causes unmanned plane body 1 disequilibrium, adds and employs steering wheel 3 and steering wheel 7 controls
The unlatching of hatch door 5, compared with the parachute construction of traditional unmanned plane, has more controllability.
The present embodiment have the beneficial effect that compared with the parachute construction of traditional unmanned plane, by employ through hole,
One VELCRO, gathering sill, the second VELCRO and coupler body preset the movement locus connecting rope, it is therefore prevented that using parachute
Time connect rope and strike unmanned plane body and cause unmanned plane body disequilibrium, using effect is good, and success rate is high, adds and makes
Control the unlatching of hatch door with steering wheel and steering wheel, compared with the parachute construction of traditional unmanned plane, have more controllability.
Embodiment 2
As Figure 1-5, the parachute construction of a kind of unmanned plane, including unmanned plane body 1, parachute 2 and steering wheel 3, described nothing
Being provided with cabin 4 and hatch door 5 on man-machine body 1, described unmanned plane body 1 and hatch door 5 are articulated and connected, described cabin 4 and hatch door 5
Between be provided with through hole 6, described steering wheel 3 is provided with steering wheel 7, described hatch door 5 is spacing by steering wheel 7, described unmanned plane body 1
On be provided with the first VELCRO 8, gathering sill the 9, second VELCRO 10 and coupler body 11, described parachute 2 be connected with connection rope 12, described
Connect rope 12 and pass sequentially through through hole the 6, first VELCRO 8, gathering sill the 9, second VELCRO 10 and coupler body 11 in cabin 4 around nothing
Above man-machine body 1, described unmanned plane body 1 includes fuselage 13, host wing 14, tailplane 15, vertical tail 16, motor
(not shown) and receiver (not shown), described gathering sill 9 is positioned at fuselage 13 tail end, and described first VELCRO 8 is positioned at fuselage 13
Lower surface, described second VELCRO 10 is positioned at the side of vertical tail 16, can play good guide effect, is possible to prevent fall
The umbrella 2 that falls connects rope 11 in use and strikes vertical tail 16, and described coupler body 11 is positioned at fuselage 13 upper surface, and described coupler body 11 sets
Being equipped with 4, described coupler body 11 rectangular array is distributed, and described connection rope 12 includes main rope (not shown) and branch line (is not schemed
Show), described branch line 18 is provided with 4, and described branch line 18 is connected with coupler body 11 respectively, when parachute 4 branch line structures in use
Become triangle body shape, be possible not only to play the effect of outstanding dispersion stress, but also unmanned plane body 1 can be promoted when landing
Stability, described steering wheel 3 is embedded in fuselage 13 lower surface, Stability Analysis of Structures, connects reliable, and does not results in air drag,
Described through hole 6 is arranged in triangular shape, connects rope 12 and is close on the angle of through hole 6, has certain guiding and locating effect, described
Paralleling with vertical tail 16 in the bottom surface of gathering sill 9, can play good guide effect, is possible to prevent unmanned plane body 1
Balance cause large effect, described fuselage 13 is provided with installing hole (not shown), described coupler body 11 inserts installing hole
In, described coupler body 11 bonds with fuselage 13, Stability Analysis of Structures, connects reliable, and described steering wheel 3 removably connects with steering wheel 7, Ke Yifang
Just user is installed and is changed, and described steering wheel 7 and steering wheel 3 are provided with 2, it is provided that two spacing stress points so that limit
Position is more stable, and described first VELCRO 8 and the second VELCRO 10 are all fixing with fuselage 13 to be connected, and Stability Analysis of Structures connects reliable,
It is possible to prevent unmanned plane body 1 first VELCRO 8 and second VELCRO 10 in flight course to drop, with traditional unmanned plane
Parachute construction is compared, and comes in advance by employing through hole the 6, first VELCRO 8, gathering sill the 9, second VELCRO 10 and coupler body 11
Set the movement locus connecting rope 12, it is therefore prevented that connect rope 12 when using parachute 2 and strike unmanned plane body 1 and cause nothing
Man-machine body 1 disequilibrium, adds and employs steering wheel 3 and steering wheel 7 controls the unlatching of hatch door 5, with the fall of traditional unmanned plane
The umbrella structure that falls is compared, and has more controllability.
The present embodiment have the beneficial effect that compared with the parachute construction of traditional unmanned plane, by employ through hole,
One VELCRO, gathering sill, the second VELCRO and coupler body preset the movement locus connecting rope, it is therefore prevented that using parachute
Time connect rope and strike unmanned plane body and cause unmanned plane body disequilibrium, using effect is good, and success rate is high, adds and makes
Control the unlatching of hatch door with steering wheel and steering wheel, compared with the parachute construction of traditional unmanned plane, have more controllability, unmanned
Machine body includes fuselage, host wing, tailplane, vertical tail, motor and receiver, and gathering sill is positioned at fuselage tail end, the
One VELCRO is positioned at unmanned plane body lower surface, and the second VELCRO is positioned at the side of vertical tail, can play good guiding
Effect, is possible to prevent parachute to connect rope in use and strikes vertical tail, and coupler body is positioned at fuselage upper surface, and coupler body is provided with
4, coupler body rectangular array is distributed, and connects rope and includes main rope and branch line, and branch line is provided with 4, and branch line is respectively with coupler body even
Connect, when parachute 4 branch lines in use constitute triangle body shape, be possible not only to play the effect of outstanding dispersion stress, and
Can also promote the unmanned plane body stability when landing, steering wheel is embedded in fuselage lower surface, Stability Analysis of Structures, connects reliable,
And do not result in air drag, through hole be triangular shape arrange, connect rope is close on the angle of through hole, have certain guiding and
Locating effect, paralleling with vertical tail in the bottom surface of gathering sill, can play good guide effect, be possible to prevent unmanned plane
The balance of body causes large effect, and fuselage is provided with installing hole, and coupler body inserts in installing hole, and coupler body glues with fuselage
Closing, Stability Analysis of Structures, connect reliable, steering wheel removably connects with steering wheel, user can be facilitated to install and change, steering wheel and steering wheel
It is provided with 2, it is provided that two spacing stress points so that spacing more stable, the first VELCRO and the second VELCRO are equal
Fixing with fuselage is connected, Stability Analysis of Structures, connects reliably, be possible to prevent unmanned plane body first VELCRO and the in flight course
Two VELCRO drop.
The above, the only detailed description of the invention of the present invention, but protection scope of the present invention is not limited thereto, and any
The change expected without creative work or replacement, all should contain within protection scope of the present invention.
Claims (10)
1. a parachute construction for unmanned plane, including unmanned plane body, parachute and steering wheel, described unmanned plane body is arranged
Cabin and hatch door, described unmanned plane body and hatch door is had to be articulated and connected, it is characterised in that: it is provided with between described cabin and hatch door
Through hole, described steering wheel is provided with steering wheel, and described hatch door is spacing by steering wheel, and described unmanned plane body is provided with the first magic
Patch, gathering sill, the second VELCRO and coupler body, described parachute is connected with connection rope, and described connection rope passes sequentially through through hole, the first evil spirit
Art patch, gathering sill, the second VELCRO and coupler body in cabin above unmanned plane body.
The parachute construction of unmanned plane the most according to claim 1, it is characterised in that: described unmanned plane body comprises organic
Body, host wing, tailplane, vertical tail, motor and receiver, described gathering sill is positioned at fuselage tail end, described first magic
Patch is positioned at fuselage lower surface, and described second VELCRO is positioned at the side of vertical tail.
The parachute construction of unmanned plane the most according to claim 2, it is characterised in that: described coupler body is positioned at table on fuselage
Face, described coupler body is provided with 4, and described coupler body rectangular array is distributed, and described connection rope includes main rope and branch line, described
Rope is provided with 4, and described branch line is connected with coupler body respectively.
The parachute construction of unmanned plane the most according to claim 3, it is characterised in that: described steering wheel is embedded in fuselage following table
Face.
The parachute construction of unmanned plane the most according to claim 4, it is characterised in that: described through hole is that triangular shape is arranged.
The parachute construction of unmanned plane the most according to claim 5, it is characterised in that: the bottom surface of described gathering sill is with vertical
Empennage is parallel.
The parachute construction of unmanned plane the most according to claim 6, it is characterised in that: it is provided with installation on described fuselage
Hole, described coupler body inserts in installing hole, and described coupler body bonds with fuselage.
The parachute construction of unmanned plane the most according to claim 7, it is characterised in that: described steering wheel detachably connects with steering wheel
Connect.
The parachute construction of unmanned plane the most according to claim 8, it is characterised in that: described steering wheel and steering wheel are provided with
2.
The parachute construction of unmanned plane the most according to claim 9, it is characterised in that: described first VELCRO and second
VELCRO is all fixing with fuselage to be connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610709369.9A CN106081125A (en) | 2016-08-24 | 2016-08-24 | A kind of parachute construction of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610709369.9A CN106081125A (en) | 2016-08-24 | 2016-08-24 | A kind of parachute construction of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106081125A true CN106081125A (en) | 2016-11-09 |
Family
ID=57225567
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610709369.9A Pending CN106081125A (en) | 2016-08-24 | 2016-08-24 | A kind of parachute construction of unmanned plane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108177783A (en) * | 2017-12-28 | 2018-06-19 | 陕西中科博亿电子科技有限公司 | A kind of training type unmanned plane |
| CN113643607A (en) * | 2021-09-15 | 2021-11-12 | 西南石油大学 | Model solid rocket bomb umbrella system |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201086826Y (en) * | 2007-08-03 | 2008-07-16 | 西安大地测绘工程有限责任公司 | Back pushing type veil opening device of minitype pilotless plane |
| CN203946278U (en) * | 2014-06-11 | 2014-11-19 | 江苏数字鹰科技发展有限公司 | The parachuting umbrella cabin of unmanned plane |
| RU2592961C2 (en) * | 2014-12-31 | 2016-07-27 | Дмитрий Сергеевич Шаров | Method of parachute landing drone aircraft and parachute system of landing drone aircraft |
| CN206031796U (en) * | 2016-08-24 | 2017-03-22 | 广州朱雀航空科技有限公司 | Unmanned aerial vehicle's parachute structure |
-
2016
- 2016-08-24 CN CN201610709369.9A patent/CN106081125A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201086826Y (en) * | 2007-08-03 | 2008-07-16 | 西安大地测绘工程有限责任公司 | Back pushing type veil opening device of minitype pilotless plane |
| CN203946278U (en) * | 2014-06-11 | 2014-11-19 | 江苏数字鹰科技发展有限公司 | The parachuting umbrella cabin of unmanned plane |
| RU2592961C2 (en) * | 2014-12-31 | 2016-07-27 | Дмитрий Сергеевич Шаров | Method of parachute landing drone aircraft and parachute system of landing drone aircraft |
| CN206031796U (en) * | 2016-08-24 | 2017-03-22 | 广州朱雀航空科技有限公司 | Unmanned aerial vehicle's parachute structure |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108177783A (en) * | 2017-12-28 | 2018-06-19 | 陕西中科博亿电子科技有限公司 | A kind of training type unmanned plane |
| CN113643607A (en) * | 2021-09-15 | 2021-11-12 | 西南石油大学 | Model solid rocket bomb umbrella system |
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Application publication date: 20161109 |
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