CN107985579A - A kind of cargo aircraft - Google Patents
A kind of cargo aircraft Download PDFInfo
- Publication number
- CN107985579A CN107985579A CN201711311975.6A CN201711311975A CN107985579A CN 107985579 A CN107985579 A CN 107985579A CN 201711311975 A CN201711311975 A CN 201711311975A CN 107985579 A CN107985579 A CN 107985579A
- Authority
- CN
- China
- Prior art keywords
- rotor
- forebody
- motor
- fuselage
- rear body
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Handcart (AREA)
Abstract
A kind of cargo aircraft, belongs to vehicle technology field, more particularly to a kind of cargo aircraft, including forebody, rear body, goods basket, supporting leg, jack-post, rotor and motor.The forebody in rear body with being furnished with control system and airborne equipment.Fuselage is divided into forebody and rear body by the goods basket on fuselage.The rotor fin is symmetrical and is distributed on fuselage.The forebody has five motors and rotor.The rear body has two motors and rotor.There are a motor and rotor at the forebody head.There are a pair of of rotor and a pair of of motor on two supporting legs of the forebody respectively.The leg structure formed objects are equally symmetrically distributed in fuselage both sides.The motor is separately fixed on respective supporting leg.The rotor is placed on motor.The jack-post connects two supporting legs through fuselage and each jack-post.The supporting leg bottom is equipped with wheel.A kind of cargo aircraft of the present invention, safety and stability is full-featured, can be transported in the air with land.
Description
Technical field
A kind of cargo aircraft, belongs to vehicle technology field, more particularly to a kind of cargo aircraft.
Background technology
Aircraft has come into the sight of people gradually with advances in technology, so that be exploited applied to cargo transport, but
It is that traditional aircraft can only carry out working at height, unmanned plane can only be transported in working at height once emergency occurs and needs to land
Sending can not realize at all.
The content of the invention
The purpose of the present invention is overcoming the above-mentioned deficiency of traditional aircraft, it is simple to invent a kind of structure of convenient control
The higher cargo aircraft of efficiency.
A kind of cargo aircraft, including forebody, rear body, goods basket, supporting leg, jack-post, rotor and motor.
The forebody in rear body with being furnished with control system and airborne equipment.Fuselage is divided into by the goods basket on fuselage
Forebody and rear body.The rotor fin is symmetrical and is distributed on fuselage.The forebody has five motors and rotor.Institute
Stating rear body has two motors and rotor.There are a motor and rotor at the forebody head.Two supporting legs of the forebody
It is upper to have a pair of of rotor and a pair of of motor respectively.The leg structure formed objects are equally symmetrically distributed in fuselage both sides.It is described
Motor is separately fixed on respective supporting leg.The rotor is placed on motor.The jack-post is connected through fuselage and each jack-post
Two supporting legs.The supporting leg bottom is equipped with wheel.
The working method of the cargo aircraft is:Filled in goods basket and drive rotor in departure place electric motor starting after cargo
Accelerate rotation to be raised to air transport, reach landing unloading behind appointed place, if also to move ahead a distance on ground, supporting leg will take turns
Son expenditure transported, after the completion of come back to the base in the same way.
A kind of cargo aircraft of the present invention, safety and stability is full-featured, can be transported in the air with land, saves
Production cost.
Brief description of the drawings
Fig. 1 is the schematic perspective view of cargo aircraft.
In figure, 1- forebodys, 2- rear bodies, 3- goods baskets, 4- supporting legs, 5- jack-posts, 6- rotors, 7- motors.
Embodiment
The present invention is illustrated in conjunction with attached drawing, a kind of cargo aircraft, including forebody 1, rear body 2, goods
Basket 3, supporting leg 4, jack-post 5, rotor 6 and motor 7.
The forebody 1 in rear body 2 with being furnished with control system and airborne equipment.The goods basket 3 is on fuselage by fuselage
It is divided into forebody 1 and rear body 2.6 fin of rotor is symmetrical and is distributed on forebody 1 and rear body 2.The forebody
1 has five motors 7 and rotor 6.The rear body 2 has two motors and rotor.Have at 1 head of forebody a motor 7 with
Rotor 6.There are a pair of of rotor 6 and a pair of of motor 7 on two supporting legs 4 of the forebody 1 respectively.4 structure of supporting leg is identical big
It is small to be equally symmetrically distributed in forebody 1 and 2 both sides of rear body.The motor 7 is separately fixed on respective supporting leg 4.The rotation
The wing 6 is placed on motor 7.The jack-post 5 connects two supporting legs 4 through fuselage and each jack-post 5.4 bottom of supporting leg is equipped with
Wheel.
The working method of the cargo aircraft is:Revolved after cargo is filled in goods basket 3 in the startup drive of departure place motor 7
The wing 6 accelerates rotation to be raised to air transport, reaches landing unloading behind appointed place, if also to move ahead a distance on ground, supporting leg 4
By wheel expenditure transported, after the completion of come back to the base in the same way.
A kind of cargo aircraft of the present invention, safety and stability is full-featured, can be transported in the air with land, saves
Production cost.
Claims (3)
- A kind of 1. cargo aircraft, it is characterised in that：Including forebody（1）, rear body（2）, goods basket（3）, supporting leg（4）, jack-post （5）, rotor（6）And motor（7）；The forebody（1）With rear body（2）It is interior to be furnished with control system and airborne equipment；The goods Basket（3）Fuselage is divided into forebody on fuselage（1）With rear body（2）；The rotor（6）Fin is symmetrical and is distributed in fuselage On；The forebody（1）There are five motors（7）With rotor（6）；The rear body（2）There are two motors（7）With rotor（6）；Institute State forebody（1）There is a motor at head（7）With rotor（6）；The forebody（1）Two supporting legs（4）It is upper to have a pair respectively Rotor（6）With a pair of of motor（7）；The supporting leg（4）Structure formed objects are equally symmetrically distributed in fuselage both sides；The motor （7）It is separately fixed at respective supporting leg（4）On；The rotor（6）It is placed on motor（7）On；The jack-post（5）Through fuselage and often A jack-post（5）Connect two supporting legs（4）.
- A kind of 2. cargo aircraft according to claim 1, it is characterised in that：Its working method is：In goods basket（3）It is interior Fill after cargo in departure place motor（7）Start and drive rotor（6）Accelerate rotation to be raised to air transport, dropped after reaching appointed place Fall unloading, if also to move ahead a distance on ground, supporting leg（4）By wheel expenditure transported, after the completion of return in the same way Go back to base.
- A kind of 3. cargo aircraft according to claim 1 or 2, it is characterised in that：The supporting leg（4）Bottom is equipped with wheel Son.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711311975.6A CN107985579A (en) | 2017-12-11 | 2017-12-11 | A kind of cargo aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711311975.6A CN107985579A (en) | 2017-12-11 | 2017-12-11 | A kind of cargo aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107985579A true CN107985579A (en) | 2018-05-04 |
Family
ID=62037637
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711311975.6A Pending CN107985579A (en) | 2017-12-11 | 2017-12-11 | A kind of cargo aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107985579A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107972859A (en) * | 2017-12-11 | 2018-05-01 | 王美航 | A kind of two-way aircraft |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104494818A (en) * | 2014-11-28 | 2015-04-08 | 吉林大学 | Novel four-rotor-wing amphibious robot |
| RU2577822C2 (en) * | 2014-07-02 | 2016-03-20 | Владимир Иванович Путинцев | Multicopter with linear arrangement of propeller sets |
| CN105905290A (en) * | 2016-05-30 | 2016-08-31 | 哈工大机器人集团有限公司 | Movable flight vehicle |
| CN106043696A (en) * | 2016-06-30 | 2016-10-26 | 天津曙光天成科技有限公司 | Flying system for unmanned aerial vehicle |
| CN206679253U (en) * | 2017-04-11 | 2017-11-28 | 王钦正 | Multipurpose supply rescue unmanned plane |
-
2017
- 2017-12-11 CN CN201711311975.6A patent/CN107985579A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2577822C2 (en) * | 2014-07-02 | 2016-03-20 | Владимир Иванович Путинцев | Multicopter with linear arrangement of propeller sets |
| CN104494818A (en) * | 2014-11-28 | 2015-04-08 | 吉林大学 | Novel four-rotor-wing amphibious robot |
| CN105905290A (en) * | 2016-05-30 | 2016-08-31 | 哈工大机器人集团有限公司 | Movable flight vehicle |
| CN106043696A (en) * | 2016-06-30 | 2016-10-26 | 天津曙光天成科技有限公司 | Flying system for unmanned aerial vehicle |
| CN206679253U (en) * | 2017-04-11 | 2017-11-28 | 王钦正 | Multipurpose supply rescue unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107972859A (en) * | 2017-12-11 | 2018-05-01 | 王美航 | A kind of two-way aircraft |
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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 | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180504 |