CN105882958A - Novel freight transport unmanned aerial vehicle - Google Patents
Novel freight transport unmanned aerial vehicle Download PDFInfo
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- CN105882958A CN105882958A CN201510410874.9A CN201510410874A CN105882958A CN 105882958 A CN105882958 A CN 105882958A CN 201510410874 A CN201510410874 A CN 201510410874A CN 105882958 A CN105882958 A CN 105882958A
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- fuselage
- aerial vehicle
- unmanned plane
- wing
- vehicle body
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Abstract
The invention relates to a novel freight transport unmanned aerial vehicle which comprises an aerial vehicle body, an undercarriage, two or more fixed wings, two or more spiral wings, a drive propeller, a drive engine and a cargo compartment; the drive engine is located in the aerial vehicle body and connected with the spiral wings and the drive propeller through transmission shafts, the drive propeller is located right behind the aerial vehicle body, the spiral wings are embedded into the fixed wings, the fixed wings are hinged to the aerial vehicle body through an adjusting device, the fixed wings are symmetrically distributed on the two sides of the aerial vehicle body, the undercarriage is located under the aerial vehicle body and connected with the side surface of the aerial vehicle body, the lower surface of the aerial vehicle body is additionally provided with two or more positioning beams and two or more positioning electromagnets, and the aerial vehicle body is connected with the cargo compartment through the positioning beams and the positioning electromagnets. By means of the novel freight transport unmanned aerial vehicle, on one hand, the requirement for non-cargo transport with the unmanned aerial vehicle can be effectively met, on the other hand, the structure of the unmanned aerial vehicle can be adjusted flexibly, the fuel utilization rate is raised, and endurance capacity and survival capacity of the unmanned aerial vehicle are improved.
Description
Technical field
The present invention relates to a kind of unmanned plane equipment, be exactly a kind of Novel cargo unmanned plane.
Background technology
nullGet more and more now with the application of unmanned plane in the fields such as detection of taking photo by plane，And application requires more and more higher，Therefore the bearing capacity of unmanned plane is had higher requirement，And current nobody the most only possesses the ability carrying monitoring device of taking photo by plane，The farthest cannot meet the needs utilizing unmanned plane to carry out goods transport，In order to utilize unmanned plane to carry out the requirement of goods transport，Currently also have developed particle carrying capacity strong，The invention unmanned plane that volume strengthens，But the housing construction of this kind of unmanned plane is relatively fixed，Application flexibility is not enough，Especially under unmanned plane no-load condition，Its deadweight is the most relatively large，Cause bigger waste of fuel，And reduce the flying power of unmanned plane，Simultaneously，Current loading unmanned plane is also because structure is relatively fixed，Therefore when unmanned plane causes bearing capacity to decline because of fuel shortage or equipment fault in running，Effectively himself structure effectively cannot be adjusted，Thus cause the survival ability of unmanned plane relatively low，Safety in operation is not enough，Therefore for this present situation，In the urgent need to developing a kind of brand-new unmanned plane equipment，To meet actually used needs.
Summary of the invention
For not enough present on prior art, the present invention provides a kind of Novel cargo unmanned plane, this inventive structure is simple, rationally distributed, carrying capacity is strong, operation energy consumption is cheap, on the one hand the needs utilizing unmanned plane to carry out transport out of stock can effectively be met, improve practicality and the range of application of unmanned plane, on the other hand can flexibly the structure of unmanned plane be adjusted, thus effectively reduce the deadweight under unmanned plane Light Condition, improve fuel availability and flying power, simultaneously separately can be according to actual needs, running realizes to goods, undercarriages etc. separate, thus reach to reduce rapidly unmanned plane deadweight, improve the purpose of unmanned plane survival ability.
To achieve these goals, the present invention is to realize by the following technical solutions:
nullA kind of Novel cargo unmanned plane，Including fuselage、Undercarriage、Fixing wing、Spiral wing、Drive propeller、Drive engine and shipping cabin，Engine is wherein driven to be positioned at fuselage interior，And by power transmission shaft respectively with spiral wing、Driving propeller connects，Propeller is driven to be positioned at the dead astern of fuselage，And be coaxially distributed with fuselage，Spiral wing at least two is the most symmetrical with fuselage axis，Spiral wing is separately embedded in fixing wing，And spiral wing lower surface separately sets guide fluid grating with spiral wing corresponding position，Guide fluid grating is the most hinged with fixing wing，Fixing wing is hinged with fuselage by adjusting means，And fixing wing at least two，And it is symmetrically distributed in fuselage both sides，Undercarriage is positioned at immediately below fuselage，And be connected with fuselage side surface，Fuselage lower surface separately sets at least two positioning beam and at least two positioning electromagnet，Fuselage is separately connected with shipping cabin by positioning beam and positioning electromagnet，Wherein positioning beam includes two ends connecting rod，And connecting rod is L-shaped，Two connecting rod ends are hinged with fuselage，Front end is connected by junction button and electric magnet.
Further, described driving propeller separately can be located at fuselage dead ahead.
Further, described undercarriage connects by being connected knot that can be undone by a pull and electric magnet with between fuselage.
Further, described shipping cabin is separately set and is connected with the control circuit of fuselage by wire.
Present configuration is simple, rationally distributed, carrying capacity is strong, operation energy consumption is cheap, on the one hand the needs utilizing unmanned plane to carry out transport out of stock can effectively be met, improve practicality and the range of application of unmanned plane, on the other hand can flexibly the structure of unmanned plane be adjusted, thus effectively reduce the deadweight under unmanned plane Light Condition, improve fuel availability and flying power, simultaneously separately can be according to actual needs, running realizes to goods, undercarriages etc. separate, thus reach to reduce rapidly unmanned plane deadweight, improve the purpose of unmanned plane survival ability.
Accompanying drawing explanation
The present invention is described in detail below in conjunction with the accompanying drawings with detailed description of the invention；
Fig. 1 is present configuration schematic diagram；
Fig. 2 is positioning beam structural representation.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below in conjunction with detailed description of the invention, the present invention is expanded on further.
nullA kind of Novel cargo unmanned plane as described in Fig. 1 and 2，Including fuselage 1、Undercarriage 2、Fixing wing 3、Spiral wing 4、Drive propeller 5、Drive engine 6 and shipping cabin 7，Engine 6 is wherein driven to be positioned at fuselage interior，And by power transmission shaft respectively with spiral wing 4、Propeller 5 is driven to connect，Propeller 5 is driven to be positioned at the dead astern of fuselage 1，And be coaxially distributed with fuselage 1，Spiral wing 4 at least two is also distributed with fuselage 1 axisymmetrical，Spiral wing 4 is separately embedded in fixing wing 3，And spiral wing 3 lower surface separately sets guide fluid grating 8 with spiral wing 4 corresponding position，Guide fluid grating 8 is the most hinged with fixing wing 3，Fixing wing 3 is hinged with fuselage 1 by adjusting means，And fixing wing 3 at least two，And it is symmetrically distributed in fuselage 1 both sides，Undercarriage 2 is positioned at immediately below fuselage 1，And be connected with fuselage 1 side surface，Fuselage 1 lower surface separately sets at least two positioning beam 9 and at least two positioning electromagnet 10，Fuselage 1 is separately connected with shipping cabin 7 by positioning beam 9 and positioning electromagnet 10，Wherein positioning beam 9 includes two ends connecting rod 91，And connecting rod 91 is L-shaped，Two connecting rod 91 ends are hinged with fuselage 1，Front end is connected by junction button 11 and electric magnet 12.
In the present embodiment, described driving propeller 5 separately can be located at fuselage 1 dead ahead.
In the present embodiment, described undercarriage 2 connects by being connected knot that can be undone by a pull 11 and electric magnet 12 with between fuselage 1.
In the present embodiment, described shipping cabin 7 is separately set and is connected by the control circuit of wire 13 with fuselage 1.
Present configuration is simple, rationally distributed, carrying capacity is strong, operation energy consumption is cheap, on the one hand the needs utilizing unmanned plane to carry out transport out of stock can effectively be met, improve practicality and the range of application of unmanned plane, on the other hand can flexibly the structure of unmanned plane be adjusted, thus effectively reduce the deadweight under unmanned plane Light Condition, improve fuel availability and flying power, simultaneously separately can be according to actual needs, running realizes to goods, undercarriages etc. separate, thus reach to reduce rapidly unmanned plane deadweight, improve the purpose of unmanned plane survival ability.
The ultimate principle of the present invention and principal character and advantages of the present invention have more than been shown and described.Skilled person will appreciate that of the industry; the present invention is not restricted to the described embodiments; the principle that the present invention is simply described described in above-described embodiment and description; without departing from the spirit and scope of the present invention; the present invention also has various changes and modifications, and these changes and improvements both fall within scope of the claimed invention.Claimed scope is defined by appending claims and equivalent thereof.
Claims (4)
- null1. a Novel cargo unmanned plane，It is characterized in that: described Novel cargo unmanned plane includes fuselage、Undercarriage、Fixing wing、Spiral wing、Drive propeller、Drive engine and shipping cabin，Wherein said driving engine is positioned at fuselage interior，And by power transmission shaft respectively with spiral wing、Driving propeller connects，The wherein said dead astern driving propeller to be positioned at fuselage，And be coaxially distributed with fuselage，Described spiral wing at least two is the most symmetrical with fuselage axis，Described spiral wing is separately embedded in fixing wing，And spiral wing lower surface separately sets guide fluid grating with spiral wing corresponding position，Described guide fluid grating is the most hinged with fixing wing，Described fixing wing is hinged with fuselage by adjusting means，And fixing wing at least two，And it is symmetrically distributed in fuselage both sides，Described undercarriage is positioned at immediately below fuselage，And be connected with fuselage side surface，Described fuselage lower surface separately sets at least two positioning beam and at least two positioning electromagnet，Fuselage is separately connected with shipping cabin by positioning beam and positioning electromagnet，Wherein said positioning beam includes two ends connecting rod，And described connecting rod is L-shaped，Two described connecting rod ends are hinged with fuselage，Front end is connected by junction button and electric magnet.
- A kind of Novel cargo unmanned plane the most according to claim 1, it is characterised in that described driving propeller separately can be located at fuselage dead ahead.
- A kind of Novel cargo unmanned plane the most according to claim 1, it is characterised in that described undercarriage with between fuselage by being connected knot that can be undone by a pull and electric magnet connection.
- A kind of Novel cargo unmanned plane the most according to claim 1, it is characterised in that described shipping cabin is separately set and connected with the control circuit of fuselage by wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510410874.9A CN105882958A (en) | 2015-07-14 | 2015-07-14 | Novel freight transport unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510410874.9A CN105882958A (en) | 2015-07-14 | 2015-07-14 | Novel freight transport unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN105882958A true CN105882958A (en) | 2016-08-24 |
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| CN201510410874.9A Pending CN105882958A (en) | 2015-07-14 | 2015-07-14 | Novel freight transport unmanned aerial vehicle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106786139A (en) * | 2016-12-08 | 2017-05-31 | 北京国网富达科技发展有限责任公司 | A kind of tele-control system of transmission line of electricity fall coaster |
| WO2019112405A1 (en) * | 2017-12-05 | 2019-06-13 | Universite Internationale De Rabat | Drone having detachable landing gear |
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| US5174523A (en) * | 1989-01-09 | 1992-12-29 | Westland Helicopters Limited | Compound helicopter with engine shaft power output control |
| CN102126553A (en) * | 2010-01-12 | 2011-07-20 | 北京航空航天大学 | Vertically taking off and landing small unmanned aerial vehicle |
| CN103448910A (en) * | 2013-08-31 | 2013-12-18 | 西北工业大学 | Aircraft capable of vertically taking off and landing at high speed |
| CN203391991U (en) * | 2013-04-28 | 2014-01-15 | 唐粮 | Task load-oriented modularized unmanned helicopter |
| CN204037896U (en) * | 2014-08-12 | 2014-12-24 | 中国航空工业经济技术研究院 | A kind of logistics depopulated helicopter |
| CN104608923A (en) * | 2015-01-31 | 2015-05-13 | 中南大学 | Honeycomb-type six-rotor transport aircraft |
| CN204937495U (en) * | 2015-07-14 | 2016-01-06 | 成都育芽科技有限公司 | A kind of Novel cargo unmanned plane |
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2015
- 2015-07-14 CN CN201510410874.9A patent/CN105882958A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5174523A (en) * | 1989-01-09 | 1992-12-29 | Westland Helicopters Limited | Compound helicopter with engine shaft power output control |
| CN102126553A (en) * | 2010-01-12 | 2011-07-20 | 北京航空航天大学 | Vertically taking off and landing small unmanned aerial vehicle |
| CN203391991U (en) * | 2013-04-28 | 2014-01-15 | 唐粮 | Task load-oriented modularized unmanned helicopter |
| CN103448910A (en) * | 2013-08-31 | 2013-12-18 | 西北工业大学 | Aircraft capable of vertically taking off and landing at high speed |
| CN204037896U (en) * | 2014-08-12 | 2014-12-24 | 中国航空工业经济技术研究院 | A kind of logistics depopulated helicopter |
| CN104608923A (en) * | 2015-01-31 | 2015-05-13 | 中南大学 | Honeycomb-type six-rotor transport aircraft |
| CN204937495U (en) * | 2015-07-14 | 2016-01-06 | 成都育芽科技有限公司 | A kind of Novel cargo unmanned plane |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106786139A (en) * | 2016-12-08 | 2017-05-31 | 北京国网富达科技发展有限责任公司 | A kind of tele-control system of transmission line of electricity fall coaster |
| WO2019112405A1 (en) * | 2017-12-05 | 2019-06-13 | Universite Internationale De Rabat | Drone having detachable landing gear |
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Application publication date: 20160824 |