CN109927893A - A kind of more helighros with floating air bag - Google Patents
A kind of more helighros with floating air bag Download PDFInfo
- Publication number
- CN109927893A CN109927893A CN201711414784.2A CN201711414784A CN109927893A CN 109927893 A CN109927893 A CN 109927893A CN 201711414784 A CN201711414784 A CN 201711414784A CN 109927893 A CN109927893 A CN 109927893A
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- China
- Prior art keywords
- air bag
- helighros
- floating air
- floating
- bracket
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- 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.)
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Abstract
A kind of more helighros with floating air bag.It is to connect by using the fixing piece between the direct setting fastening of force-supporting net or floating gasbag frame and bracket on bracket between more helighro rotors, be equipped with floating air bag.The lift as caused by floating air bag can directly increase the battery carrying amount and load capacity of more helighros, offset self weight.Therefore the battery power entrained by it can be a large amount of or be entirely used for forerunner's flight, increases the load capacity of more helighros with floating air bag, and hang time and voyage increase, so as to achieve the purpose that raising and expand its use scope.
Description
Technical field
The present invention relates to a kind of lighter-than-air flight device, especially a kind of more helighros with floating air bag.
Background technique
Currently, well known more helighros are because that can only use pure electricity by the lesser architectural limitation of rotor size
Power drive or the mode of the electric combination drive of oil, to provide lift and flying power.Its shortcoming is that: due to available battery
Energy density is smaller, to cause the load capacity very little of more helighros, the hang time is shorter with voyage, and then greatly limits
The expansion and popularization of its use scope are made.
Summary of the invention
In order to overcome existing more helighro load capacities small, hang time and the shorter deficiency of voyage, the present invention
A kind of more helighros with floating air bag are provided, more helighros with floating air bag, not only load capacity
Greatly, and hang time and voyage are also longer, can expand the use scope of more helighros.
The technical solution adopted by the present invention to solve the technical problems is: the bracket between more helighro rotors
On, it is connected by using the fixing piece between the direct setting fastening of force-supporting net or floating gasbag frame and bracket, floating air bag is installed.
The lift as caused by floating air bag can directly increase the battery carrying amount and load capacity of more helighros, offset
Self weight.Therefore the battery power entrained by it can be a large amount of or be entirely used for forerunner's flight, makes more rotors with floating air bag
The load capacity of helicopter increases, and hang time and voyage increase, so as to reach raising and expand the mesh of its use scope
's.
Beneficial effect
The invention has the advantages that providing, a kind of load capacity is big, and the hang time goes straight up to the longer more rotors of voyage
Aircraft, structure is simple, is readily produced popularization.
Detailed description of the invention
The present invention is further described with embodiment with reference to the accompanying drawing.
Fig. 1 is bottom view of the invention.
1 in figure, more helighros, 2, floating air bag, 3, rotor, 4, bracket.
Specific embodiment
In Fig. 1, on the bracket (4) between more helighro (1) rotors (3), by using the direct setting fastening of force-supporting net,
Or the fixing piece between floating air bag (2) skeleton and bracket (4) is connect, and is equipped with floating air bag (2).
Claims (1)
1. a kind of more helighros with floating air bag are the aircraft driven jointly using multiple rotors, it is characterized in that:
Floating air bag is installed on bracket between more helighro rotors.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711414784.2A CN109927893A (en) | 2017-12-19 | 2017-12-19 | A kind of more helighros with floating air bag |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711414784.2A CN109927893A (en) | 2017-12-19 | 2017-12-19 | A kind of more helighros with floating air bag |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109927893A true CN109927893A (en) | 2019-06-25 |
Family
ID=66984211
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711414784.2A Pending CN109927893A (en) | 2017-12-19 | 2017-12-19 | A kind of more helighros with floating air bag |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109927893A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112498674A (en) * | 2020-12-11 | 2021-03-16 | 太阳月亮（北京）新能源科技有限公司 | Inflatable full-electric rotary wing civil helicopter |
| CN114104277A (en) * | 2021-12-03 | 2022-03-01 | 西北工业大学 | Many rotors of improved generation helicopter of air bag is floated in area |
-
2017
- 2017-12-19 CN CN201711414784.2A patent/CN109927893A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112498674A (en) * | 2020-12-11 | 2021-03-16 | 太阳月亮（北京）新能源科技有限公司 | Inflatable full-electric rotary wing civil helicopter |
| CN114104277A (en) * | 2021-12-03 | 2022-03-01 | 西北工业大学 | Many rotors of improved generation helicopter of air bag is floated in area |
| CN114104277B (en) * | 2021-12-03 | 2024-02-27 | 西北工业大学 | Improved multi-rotor helicopter with floating air bag |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190625 |