CN103523232A - Top-arranged landing assistant parachutes of unmanned aerial vehicle - Google Patents
Top-arranged landing assistant parachutes of unmanned aerial vehicle Download PDFInfo
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- CN103523232A CN103523232A CN201310480512.8A CN201310480512A CN103523232A CN 103523232 A CN103523232 A CN 103523232A CN 201310480512 A CN201310480512 A CN 201310480512A CN 103523232 A CN103523232 A CN 103523232A
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- umbrella
- help
- fall
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- aerial vehicle
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Abstract
The invention relates to relates to a landing assistant device of an unmanned aerial vehicle, in particular to top-arranged landing assistant parachutes of the unmanned aerial vehicle. The top-arranged landing assistant parachutes of the unmanned aerial vehicle comprise an airframe, side wings are arranged on the two sides of the middle portion of the airframe, tail side wings are arranged on the two sides of the afterbody of the airframe, an empennage is arranged on the upper portion of the afterbody of the airframe, a rear landing assistant parachute cabin is formed in the afterbody of the airframe, a rear landing assistant parachute is arranged in the rear landing assistant parachute cabin, an upper landing assistant parachute cabin is formed in the upper portion of the airframe, and an upper landing assistant parachute is arranged in the upper landing assistant parachute cabin. When the top-arranged landing assistant parachutes of the unmanned aerial vehicle lose power in the air and form the state that the tail portion faces upwards and the head portion faces downwards, the upper landing assistant parachute in the upper landing assistant parachute cabin is unfolded to form upward tensile force on the airframe to enable the head portion of the airframe to be lifted upwards, the balance state of the airframe is recovered, the head portion of the unmanned aerial vehicle is prevented from falling to the ground when the unmanned aerial vehicle is landed, and the safety of the landing of the unmanned aerial vehicle is guaranteed.
Description
Technical field
The present invention relates to a kind of unmanned plane landing supplementary structure, especially a kind of unmanned plane overhead helps and falls umbrella.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft that utilizes radio robot and the process controller of providing for oneself to handle.On machine, without driving compartment, but the equipment such as autopilot, process controller are installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, to its follow the tracks of, location, remote control, remote measurement and digital communication.Can under radio telecommand, as conventional airplane, take off or launch with booster rocket, also can take aerial input to by machine tool and fly.During recovery, the available mode automatic Landing the same with conventional airplane landing mission, also can reclaim with parachute or block by remote control.
Because civilian unmanned plane does not generally have the landing runway of condition setting special use, so take off and land in the comparatively open areas such as general common square, vacant lot, especially when landing, owing to often there is no enough buffer distances, so generally fall umbrella auxiliary landing by helping of a postposition, generally be manual operation, when manual operation not at that time, unmanned plane can run out of steam when kiss the earth not yet, because afterbody helps, the auxiliary of umbrella falls, aircraft can first land by front end head when land, is unfavorable for the stable landing of unmanned plane, also easily unmanned plane is caused to damage.
Summary of the invention
The invention provides a kind of stable landing that is conducive to unmanned plane, guarantee unmanned plane safety unmanned plane overhead help and fall umbrella.
To achieve these goals, the present invention adopts following technical scheme:
Comprise a fuselage, described waist both sides are provided with flank, afterbody both sides are provided with tail flank, afterbody top is provided with empennage, after afterbody is provided with, help and fall umbrella storehouse, after help to fall after being provided with in umbrella storehouse and help and fall umbrella, its improvement is: described back is provided with to help and falls umbrella storehouse, above helps to fall to be provided with to help in umbrella storehouse and falls umbrella.
Preferably, on described, help and fall umbrella storehouse and be provided with Cang Gai.
Preferably, on described, help and fall umbrella storehouse to be located at fuselage upper surface anterior.
Preferably, on described, help and fall umbrella storehouse for circular.
Preferably, described Cang Gai is sphere.
Preferably, described sphere is with respect to fuselage upper surface outwardly convex.
Preferably, on described, help and fall umbrella and be connected with pilot-parachute on.
Preferably, after described, help and fall umbrella and be connected with a rear pilot-parachute.
Preferably, on described, help to fall after umbrella is greater than and help and fall umbrella.
Preferably, Cang Gai is movably connected on fuselage.
Owing to having adopted said structure, unmanned plane overhead of the present invention helps and falls umbrella and aloft run out of steam while forming afterbody towards state down of head portion, on help fall in umbrella storehouse on help and fall umbrella and open, formation to fuselage to upper pulling force, fuselage head is raised up, the state of equilibrium of replying fuselage, while avoiding unmanned plane to land, head lands, the safety while having guaranteed unmanned plane landing.
Accompanying drawing explanation
Fig. 1 is the perspective view of the embodiment of the present invention.
The specific embodiment
As shown in Figure 1, the unmanned plane overhead of the present embodiment helps and falls pack and draw together a fuselage 1, described fuselage 1 both sides, middle part are provided with flank 2, afterbody both sides are provided with tail flank 3, afterbody top is provided with empennage 4, after afterbody is provided with, helps and fall umbrella storehouse 5, after help to fall after being provided with in umbrella storehouse and help and fall umbrella, described back is provided with to help and falls umbrella storehouse 6, above helps to fall to be provided with to help in umbrella storehouse and falls umbrella.
In the present embodiment, help on described and fall umbrella storehouse 6 and be provided with storehouse lid 7.
In the present embodiment, help on described and fall umbrella storehouse 6 to be located at fuselage upper surface anterior.
In the present embodiment, help on described and fall umbrella storehouse 6 for circular.
In the present embodiment, described storehouse lid 7 is sphere.
In the present embodiment, described sphere is with respect to fuselage 1 upper surface outwardly convex.
In the present embodiment, help on described and fall umbrella and be connected with pilot-parachute on.
In the present embodiment, help after described and fall umbrella and be connected with a rear pilot-parachute.
In the present embodiment, help to fall after umbrella is greater than on described and help and fall umbrella.
In the present embodiment, storehouse lid 7 is movably connected on fuselage.
The foregoing is only the preferred embodiments of the present invention; not thereby limit the scope of the claims of the present invention; every equivalent structure or conversion of equivalent flow process that utilizes specification sheets of the present invention and accompanying drawing content to do; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present invention.
Claims (10)
1. unmanned plane overhead helps and falls umbrella, comprise a fuselage, described waist both sides are provided with flank, afterbody both sides are provided with tail flank, afterbody top is provided with empennage, after afterbody is provided with, helps and fall umbrella storehouse, after help to fall after being provided with in umbrella storehouse and help and fall umbrella, it is characterized in that: described back is provided with to help and falls umbrella storehouse, above help to fall to be provided with to help in umbrella storehouse and fall umbrella.
2. unmanned plane overhead as claimed in claim 1 helps and falls umbrella, it is characterized in that: on described, help and fall umbrella storehouse and be provided with Cang Gai.
3. unmanned plane overhead as claimed in claim 2 helps and falls umbrella, it is characterized in that: on described, help and fall umbrella storehouse to be located at fuselage upper surface anterior.
4. unmanned plane overhead as claimed in claim 3 helps and falls umbrella, it is characterized in that: on described, help and fall umbrella storehouse for circular.
5. unmanned plane overhead as claimed in claim 4 helps and falls umbrella, it is characterized in that: described Cang Gai is sphere.
6. unmanned plane overhead as claimed in claim 5 helps and falls umbrella, it is characterized in that: described sphere is with respect to fuselage upper surface outwardly convex.
7. unmanned plane overhead as claimed in claim 6 helps and falls umbrella, it is characterized in that: on described, help and fall umbrella and be connected with pilot-parachute on.
8. unmanned plane overhead as claimed in claim 7 helps and falls umbrella, it is characterized in that: after described, help and fall umbrella and be connected with a rear pilot-parachute.
9. unmanned plane overhead as claimed in claim 8 helps and falls umbrella, it is characterized in that: on described, help to fall after umbrella is greater than and help and fall umbrella.
10. unmanned plane overhead as claimed in claim 9 helps and falls umbrella, it is characterized in that: Cang Gai is movably connected on fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310480512.8A CN103523232A (en) | 2013-10-15 | 2013-10-15 | Top-arranged landing assistant parachutes of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310480512.8A CN103523232A (en) | 2013-10-15 | 2013-10-15 | Top-arranged landing assistant parachutes of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103523232A true CN103523232A (en) | 2014-01-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310480512.8A Pending CN103523232A (en) | 2013-10-15 | 2013-10-15 | Top-arranged landing assistant parachutes of unmanned aerial vehicle |
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Citations (8)
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|---|---|---|---|---|
| CN1256227A (en) * | 1999-11-29 | 2000-06-14 | 范军 | Multifunctional traffic means |
| JP2001120848A (en) * | 1999-10-25 | 2001-05-08 | Heikon Ryu | Safety device for radio-controlled model flying matter and radio-controlled model flying matter |
| KR20050109279A (en) * | 2005-10-28 | 2005-11-17 | 김정원 | Parachute for aircraft aircraft. Airbag |
| JP2006306264A (en) * | 2005-04-28 | 2006-11-09 | Mitsubishi Electric Corp | Parachute ejection device and unmanned aircraft |
| JP2009208674A (en) * | 2008-03-05 | 2009-09-17 | Mitsubishi Electric Corp | Mounting unmanned aircraft collecting device, and unmanned aircraft having the same |
| KR20100129143A (en) * | 2010-04-12 | 2010-12-08 | 서이환 | Landing apparatus by a parachute for unmanual aerial vehicle |
| CN201737159U (en) * | 2010-02-26 | 2011-02-09 | 任永斌 | Airplane protection system combined with multi-layered parachutes and airbags |
| CN202911951U (en) * | 2012-11-12 | 2013-05-01 | 东莞市科旺网络能源有限公司 | Protective device capable of slowing down speed of falling airplane |
-
2013
- 2013-10-15 CN CN201310480512.8A patent/CN103523232A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001120848A (en) * | 1999-10-25 | 2001-05-08 | Heikon Ryu | Safety device for radio-controlled model flying matter and radio-controlled model flying matter |
| CN1256227A (en) * | 1999-11-29 | 2000-06-14 | 范军 | Multifunctional traffic means |
| JP2006306264A (en) * | 2005-04-28 | 2006-11-09 | Mitsubishi Electric Corp | Parachute ejection device and unmanned aircraft |
| KR20050109279A (en) * | 2005-10-28 | 2005-11-17 | 김정원 | Parachute for aircraft aircraft. Airbag |
| JP2009208674A (en) * | 2008-03-05 | 2009-09-17 | Mitsubishi Electric Corp | Mounting unmanned aircraft collecting device, and unmanned aircraft having the same |
| CN201737159U (en) * | 2010-02-26 | 2011-02-09 | 任永斌 | Airplane protection system combined with multi-layered parachutes and airbags |
| KR20100129143A (en) * | 2010-04-12 | 2010-12-08 | 서이환 | Landing apparatus by a parachute for unmanual aerial vehicle |
| CN202911951U (en) * | 2012-11-12 | 2013-05-01 | 东莞市科旺网络能源有限公司 | Protective device capable of slowing down speed of falling airplane |
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Application publication date: 20140122 |