CN104129503A - Multi-rotor-wing remote control air-drop helicopter - Google Patents
Multi-rotor-wing remote control air-drop helicopter Download PDFInfo
- Publication number
- CN104129503A CN104129503A CN201310159012.4A CN201310159012A CN104129503A CN 104129503 A CN104129503 A CN 104129503A CN 201310159012 A CN201310159012 A CN 201310159012A CN 104129503 A CN104129503 A CN 104129503A
- Authority
- CN
- China
- Prior art keywords
- rotor
- remote control
- air
- helicopter
- drop
- 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
Landscapes
- Toys (AREA)
Abstract
The invention provides a multi-rotor-wing remote control air-drop helicopter. The multi-rotor-wing helicopter is provided with a plurality of rotor wings. Tying ropes capable of being used for hanging air-drop goods is arranged on the lower portion of the multi-rotor-wing helicopter. A remote control receiver is mounted on the multi-rotor-wing helicopter. According to the multi-rotor-wing remote control air-drop helicopter, the goods transported in the air can be air-dropped to a destination; in the using process, the transported goods are hung on the tying ropes and can be air-dropped to an accurate place by means of remote control; the multi-rotor-wing remote control air-drop helicopter has the advantages of being accurate, safe and incapable of damaging the goods.
Description
Technical field
The present invention relates to a kind of device of remote control air-drop material, it is congenial that a kind of many rotors are gone straight up to Remote Control Air specifically.
Background technology
When transporting now material in the air and need drop, the general parachute that uses, be about to article and be suspended on parachute top, behind destination, air-conditioning drops to ground, because parachute is a kind of device of landing voluntarily, can be subject to the interference of the many factors such as strong wind and air-flow, cause the accuracy of air-conditioning to be difficult to grasp, and after landing, article are easy to unexpected clashing and breaking.
Summary of the invention
The object of the present invention is to provide a kind of many rotors to go straight up to Remote Control Air and speculate, can air-drop article be directly transported to destination by remote control mode, and be difficult for damage product.
The present invention includes heligyro, the technical scheme adopting is: used heligyro is arranged to several rotors, and below heligyro, be provided for hanging the tether that drops article, meanwhile, at the fuselage of heligyro, a receiver of remote-control sytem is installed.
The present invention passes through technique scheme, because heligyro arranges several rotors, the stability that can actv. increases integral body, during use, by remote control adjustment, accurate, the safe air-drop of conveying articles energy can be arrived to destination, efficiently solve present use parachute air-drop article and be difficult for grasping, cause poor accuracy and easy problems such as damage product, there is safety, efficient and throw in the features such as accurate.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described.
Fig. 1 is structural representation of the present invention.
The specific embodiment
Shown in Fig. 1: heligyro 1 is provided with several rotors 2, heligyro 1 below is provided with the tether 4 that can hang air-drop thing 5, and heligyro 1 is equipped with receiver of remote-control sytem 3.
Claims (1)
1. it is congenial that rotor more than a kind is gone straight up to Remote Control Air, comprise heligyro (1), it is characterized in that: described heligyro (1) is provided with several rotors (2), heligyro (1) below is provided with the tether (4) that can hang air-drop thing (5), and heligyro (1) is equipped with receiver of remote-control sytem (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310159012.4A CN104129503A (en) | 2013-05-03 | 2013-05-03 | Multi-rotor-wing remote control air-drop helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310159012.4A CN104129503A (en) | 2013-05-03 | 2013-05-03 | Multi-rotor-wing remote control air-drop helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104129503A true CN104129503A (en) | 2014-11-05 |
Family
ID=51802438
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310159012.4A Pending CN104129503A (en) | 2013-05-03 | 2013-05-03 | Multi-rotor-wing remote control air-drop helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104129503A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105599900A (en) * | 2016-01-20 | 2016-05-25 | 清华大学合肥公共安全研究院 | Low-altitude positioning load air-drop method based on multi-rotor unmanned aerial vehicle |
-
2013
- 2013-05-03 CN CN201310159012.4A patent/CN104129503A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105599900A (en) * | 2016-01-20 | 2016-05-25 | 清华大学合肥公共安全研究院 | Low-altitude positioning load air-drop method based on multi-rotor unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB201212922D0 (en) | Unarmed aerial vehicle and method of launching | |
| GB2556843A (en) | Systems and methods of delivering products with unmanned delivery aircrafts | |
| WO2017048336A3 (en) | Devices and methods for in flight transition vtol/fixed wing hybrid aircraft structures and flight modes | |
| WO2017078044A1 (en) | Transportation device | |
| MX2018010512A (en) | Unmanned aircraft systems with a customer interface system and methods of delivery utilizing unmanned aircraft systems. | |
| GB2557154A (en) | Package release system for use in delivery packages, and methods of delivering packages | |
| WO2016053739A3 (en) | Nose attitude control of a rotary wing aircraft | |
| EP3119673A4 (en) | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades | |
| WO2014204550A3 (en) | Helicopter-mediated system and method for launching and retrieving an aircraft | |
| WO2016018486A3 (en) | Vtol aircraft | |
| WO2017131834A3 (en) | Pivoting wing system for vtol aircraft | |
| SG10201806915VA (en) | Vertical takeoff and landing (vtol) air vehicle | |
| EP3119674A4 (en) | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades | |
| WO2009072754A3 (en) | Taking off and landing airplane using variable rotary wings | |
| WO2008154066A3 (en) | Methods and apparatus for aircraft | |
| CN202609086U (en) | Downwards-throwing popup type parachute opening device of unmanned plane | |
| CN104554695B (en) | The accurate aerial delivery system of long-distance remote control formula | |
| CN204452941U (en) | A kind of simple and fast delivery device for model plane load-carrying air-drop | |
| CN104129503A (en) | Multi-rotor-wing remote control air-drop helicopter | |
| WO2016109490A8 (en) | Terreplane transportation system | |
| CN204399462U (en) | A kind of magnetic force torsion spring for umbrella hatchcover | |
| CN204452914U (en) | The accurate aerial delivery system of long-distance remote control formula | |
| CN207683774U (en) | A kind of unmanned plane having air bag of saving oneself | |
| RU2013115878A (en) | METHOD FOR MANAGING, STABILIZING AND CREATING AN ADDITIONAL AIRCRAFT LIFTING POWER | |
| CN104548616B (en) | A kind of telecontrolled aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20141105 |