CN204937495U - A kind of Novel cargo unmanned plane - Google Patents
A kind of Novel cargo unmanned plane Download PDFInfo
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- CN204937495U CN204937495U CN201520507026.5U CN201520507026U CN204937495U CN 204937495 U CN204937495 U CN 204937495U CN 201520507026 U CN201520507026 U CN 201520507026U CN 204937495 U CN204937495 U CN 204937495U
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- fuselage
- unmanned plane
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- screw propeller
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Abstract
The utility model relates to a kind of Novel cargo unmanned plane, comprise fuselage, alighting gear, fixed wing, spiral wing, drive screw propeller, drive engine and shipping cabin, engine is wherein driven to be positioned at fuselage interior, and by transmission shaft respectively with spiral wing, driving screw propeller connects, screw propeller is driven to be positioned at the dead aft of fuselage, at least two, spiral wing, spiral wing is separately embedded in fixed wing, fixed wing by control apparatus and fuselage hinged, and fixed wing at least two, and be symmetrically distributed in fuselage both sides, alighting gear is positioned at immediately below fuselage, and be connected with fuselage side surface, fuselage lower surface separately establishes at least two positioning beam and at least two positioning electromagnets, fuselage is separately connected with shipping cabin with positioning electromagnet by positioning beam.The utility model on the one hand can meet the needs utilizing unmanned plane to carry out transport out of stock by actv., can adjust the structure of unmanned plane flexibly on the other hand, improves fuel utilization and flying power and unmanned plane viability.
Description
Technical field
The present invention relates to a kind of unmanned plane equipment, is exactly a kind of Novel cargo unmanned plane.
Background technology
Get more and more along with in the application of unmanned plane in the fields such as detection of taking photo by plane at present, and application requires more and more higher, therefore the load-carrying capacity of unmanned plane is had higher requirement, and current nobody often only possesses the ability of carrying watch-dog of taking photo by plane, therefore the needs utilizing unmanned plane to carry out goods transport cannot far be met, in order to the requirement utilizing unmanned plane to carry out goods transport, it is current that also to 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 fixing, application flexibility is not enough, especially under unmanned plane no-load condition, its deadweight is still relatively large, cause larger waste of fuel, and reduce the flying power of unmanned plane, simultaneously, current loading unmanned plane is also because structure is relatively fixing, therefore when unmanned plane causes load-carrying capacity to decline because of lack of fuel or breakdown of equipment in operational process, actv. adjustment cannot be carried out by actv. to himself structure, thus cause the viability 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, with the needs that satisfied reality uses.
Summary of the invention
For the deficiency that prior art exists, the invention provides a kind of Novel cargo unmanned plane, this invention structure is simple, rationally distributed, carrying capacity is strong, operation energy consumption is cheap, the needs utilizing unmanned plane to carry out transport out of stock can be met by actv. on the one hand, improve practicality and the field of application of unmanned plane, can adjust the structure of unmanned plane flexibly on the other hand, thus the deadweight effectively reduced under unmanned plane light condition, improve fuel utilization and flying power, simultaneously separately can be according to actual needs, realize in operational process goods, alighting gears etc. are separated, thus reach reduction unmanned plane deadweight rapidly, improve the object of unmanned plane viability.
To achieve these goals, the present invention realizes by the following technical solutions:
A kind of Novel cargo unmanned plane, comprise fuselage, alighting gear, fixed wing, spiral wing, drive screw propeller, drive engine and shipping cabin, engine is wherein driven to be positioned at fuselage interior, and by transmission shaft respectively with spiral wing, driving screw propeller connects, screw propeller is driven to be positioned at the dead aft of fuselage, and coaxially distribute with fuselage, at least two, spiral wing is also symmetrical with fuselage axis, spiral wing is separately embedded in fixed wing, and guide fluid grating is separately established in spiral wing lower surface and spiral wing corresponding position, guide fluid grating is another and fixed wing is hinged, fixed wing by control apparatus and fuselage hinged, and fixed wing at least two, and be symmetrically distributed in fuselage both sides, alighting gear is positioned at immediately below fuselage, and be connected with fuselage side surface, fuselage lower surface separately establishes at least two positioning beam and at least two positioning electromagnets, fuselage is separately connected with shipping cabin with positioning electromagnet by positioning beam, wherein positioning beam comprises two ends pipe link, and pipe link is in " L " type, two pipe link ends and fuselage hinged, front end is connected by junction button and electromagnet.
Further, described driving screw propeller separately can be positioned at fuselage dead ahead.
Further, described alighting gear with between fuselage by being connected knot that can be undone by a pull and electromagnet connects.
Further, described shipping cabin is separately established and is communicated with the control circuit of fuselage by wire.
Structure of the present invention is simple, rationally distributed, carrying capacity is strong, operation energy consumption is cheap, the needs utilizing unmanned plane to carry out transport out of stock can be met by actv. on the one hand, improve practicality and the field of application of unmanned plane, can adjust the structure of unmanned plane flexibly on the other hand, thus the deadweight effectively reduced under unmanned plane light condition, improve fuel utilization and flying power, simultaneously separately can be according to actual needs, realize in operational process goods, alighting gears etc. are separated, thus reach reduction unmanned plane deadweight rapidly, improve the object of unmanned plane viability.
Accompanying drawing explanation
The present invention is described in detail below in conjunction with the drawings and specific embodiments;
Fig. 1 is structural representation of the present invention;
Fig. 2 is positioning beam structural representation.
Detailed description of the invention
The technological means realized for making the present invention, creation characteristic, reaching object and effect is easy to understand, below in conjunction with detailed description of the invention, setting forth the present invention further.
A kind of Novel cargo unmanned plane as described in Fig. 1 and 2, comprise fuselage 1, alighting gear 2, fixed wing 3, spiral wing 4, drive screw propeller 5, drive engine 6 and shipping cabin 7, engine 6 is wherein driven to be positioned at fuselage interior, and by transmission shaft respectively with spiral wing 4, screw propeller 5 is driven to connect, screw propeller 5 is driven to be positioned at the dead aft of fuselage 1, and coaxially distribute with fuselage 1, 4 at least two, spiral wing also distributes with fuselage 1 axisymmetrical, spiral wing 4 is separately embedded in fixed wing 3, and guide fluid grating 8 is separately established in spiral wing 3 lower surface and spiral wing 4 corresponding position, guide fluid grating 8 is another and fixed wing 3 is hinged, fixed wing 3 by control apparatus and fuselage 1 hinged, and fixed wing 3 at least two, and be symmetrically distributed in fuselage 1 both sides, alighting gear 2 is positioned at immediately below fuselage 1, and be connected with fuselage 1 side surface, fuselage 1 lower surface separately establishes at least two positioning beam 9 and at least two positioning electromagnets 10, fuselage 1 is separately connected with shipping cabin 7 with positioning electromagnet 10 by positioning beam 9, wherein positioning beam 9 comprises two ends pipe link 91, and pipe link 91 is in " L " type, two pipe link 91 ends and fuselage 1 hinged, front end is connected by junction button 11 and electromagnet 12.
In the present embodiment, described driving screw propeller 5 separately can be positioned at fuselage 1 dead ahead.
In the present embodiment, described alighting gear 2 with between fuselage 1 by being connected knot that can be undone by a pull 11 and electromagnet 12 connects.
In the present embodiment, described shipping cabin 7 is separately established and is communicated with by the control circuit of wire 13 with fuselage 1.
Structure of the present invention is simple, rationally distributed, carrying capacity is strong, operation energy consumption is cheap, the needs utilizing unmanned plane to carry out transport out of stock can be met by actv. on the one hand, improve practicality and the field of application of unmanned plane, can adjust the structure of unmanned plane flexibly on the other hand, thus the deadweight effectively reduced under unmanned plane light condition, improve fuel utilization and flying power, simultaneously separately can be according to actual needs, realize in operational process goods, alighting gears etc. are separated, thus reach reduction unmanned plane deadweight rapidly, improve the object of unmanned plane viability.
More than show and describe groundwork of the present invention and principal character and advantage of the present invention.The technical personnel of the industry should be understood; the present invention is not restricted to the described embodiments; what describe in above-described embodiment and specification sheets just illustrates principle of the present invention; 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 all fall in the claimed scope of the invention.Application claims protection domain is defined by appending claims and equivalent thereof.
Claims (4)
1. a Novel cargo unmanned plane, it is characterized in that: described Novel cargo unmanned plane comprises fuselage, alighting gear, fixed wing, spiral wing, drive screw propeller, drive engine and shipping cabin, wherein said driving engine is positioned at fuselage interior, and by transmission shaft respectively with spiral wing, driving screw propeller connects, wherein said driving screw propeller is positioned at the dead aft of fuselage, and coaxially distribute with fuselage, at least two described, spiral wing is also symmetrical with fuselage axis, described spiral wing is separately embedded in fixed wing, and guide fluid grating is separately established in spiral wing lower surface and spiral wing corresponding position, described guide fluid grating is another and fixed wing is hinged, described fixed wing by control apparatus and fuselage hinged, and fixed wing at least two, and be symmetrically distributed in fuselage both sides, described alighting gear is positioned at immediately below fuselage, and be connected with fuselage side surface, described fuselage lower surface separately establishes at least two positioning beam and at least two positioning electromagnets, fuselage is separately connected with shipping cabin with positioning electromagnet by positioning beam, wherein said positioning beam comprises two ends pipe link, and described pipe link is in " L " type, two described pipe link ends and fuselage hinged, front end is connected by junction button and electromagnet.
2. a kind of Novel cargo unmanned plane according to claim 1, is characterized in that, described driving screw propeller separately can be positioned at fuselage dead ahead.
3. a kind of Novel cargo unmanned plane according to claim 1, is characterized in that, described alighting gear with between fuselage by being connected knot that can be undone by a pull and electromagnet connects.
4. a kind of Novel cargo unmanned plane according to claim 1, is characterized in that, described shipping cabin is separately established and is communicated with the control circuit of fuselage by wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520507026.5U CN204937495U (en) | 2015-07-14 | 2015-07-14 | A kind of Novel cargo unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520507026.5U CN204937495U (en) | 2015-07-14 | 2015-07-14 | A kind of Novel cargo unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204937495U true CN204937495U (en) | 2016-01-06 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520507026.5U Expired - Fee Related CN204937495U (en) | 2015-07-14 | 2015-07-14 | A kind of Novel cargo unmanned plane |
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| Country | Link |
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| CN (1) | CN204937495U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105857594A (en) * | 2016-05-31 | 2016-08-17 | 聂平利 | Super-low-altitude aircraft |
| CN105882958A (en) * | 2015-07-14 | 2016-08-24 | 成都育芽科技有限公司 | Novel freight transport unmanned aerial vehicle |
| CN105947711A (en) * | 2016-06-21 | 2016-09-21 | 衢州市依科达节能技术有限公司 | Unmanned plane cargo delivery system |
| CN109878725A (en) * | 2019-03-31 | 2019-06-14 | 拓攻（南京）机器人有限公司 | A kind of fixed-wing logistics unmanned plane |
| CN113665823A (en) * | 2021-08-16 | 2021-11-19 | 航天时代飞鹏有限公司 | Hybrid type freight unmanned aerial vehicle and cargo transportation method |
-
2015
- 2015-07-14 CN CN201520507026.5U patent/CN204937495U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882958A (en) * | 2015-07-14 | 2016-08-24 | 成都育芽科技有限公司 | Novel freight transport unmanned aerial vehicle |
| CN105857594A (en) * | 2016-05-31 | 2016-08-17 | 聂平利 | Super-low-altitude aircraft |
| CN105947711A (en) * | 2016-06-21 | 2016-09-21 | 衢州市依科达节能技术有限公司 | Unmanned plane cargo delivery system |
| CN105947711B (en) * | 2016-06-21 | 2018-05-04 | 衢州市依科达节能技术有限公司 | A kind of unmanned plane cargo transport system |
| CN109878725A (en) * | 2019-03-31 | 2019-06-14 | 拓攻（南京）机器人有限公司 | A kind of fixed-wing logistics unmanned plane |
| CN113665823A (en) * | 2021-08-16 | 2021-11-19 | 航天时代飞鹏有限公司 | Hybrid type freight unmanned aerial vehicle and cargo transportation method |
| CN113665823B (en) * | 2021-08-16 | 2024-05-10 | 航天时代飞鹏有限公司 | Hybrid freight unmanned aerial vehicle and freight transportation method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160106 Termination date: 20160714 |