CN106853867A - Helium balloon multiaxis combines aircraft - Google Patents
Helium balloon multiaxis combines aircraft Download PDFInfo
- Publication number
- CN106853867A CN106853867A CN201510899459.4A CN201510899459A CN106853867A CN 106853867 A CN106853867 A CN 106853867A CN 201510899459 A CN201510899459 A CN 201510899459A CN 106853867 A CN106853867 A CN 106853867A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- helium balloon
- cockpit
- multiaxis
- rotary wings
- 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
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
-
- 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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Types And Forms Of Lifts (AREA)
Abstract
Combine aircraft the present invention relates to a kind of helium balloon multiaxis, comprising：Helium balloon (1), lifting rope (2), rotary wings (3), connecting rod (4), cockpit (5), helium balloon (1) is connected by lifting rope (2) with cockpit (5), rotary wings (3) are connected by connecting rod (4) with cockpit (5), cockpit (5) is positioned at bottom, helium balloon (1) integrally provides most of lift for aircraft, and rotary wings (3) for aircraft is provided the attached power for helping lift and motion.
Description
Technical field
The present invention relates to a kind of helium balloon multiaxis joint aircraft, belong to aircraft field.
Background technology
Currently, aircraft species is more, and form is different, is then flown using single mode mostly, and in gyroplane, Multi-axis aircraft has has a smooth flight, the advantage of safety, but needs to consume mass energy during its flight, while load-carrying also very little.
The content of the invention
The present invention relates to a kind of balloon multiaxis joint aircraft, to realize taking out more weight body or manned purpose using smaller power.
To realize above-mentioned purpose, the present invention is adopted the following technical scheme that：
A kind of balloon multiaxis combines aircraft, comprising：Helium balloon (1), lifting rope (2), rotary wings (3), connecting rod (4), cockpit (5)；As shown in Figure 1.
Below in conjunction with accompanying drawing, technical construction of the invention and method are illustrated：Helium balloon (1) is connected by lifting rope (2) with cockpit (5), rotary wings (3) are connected by connecting rod (4) with cockpit (5), cockpit (5) is positioned at bottom, helium balloon (1) integrally provides most of lift for aircraft, and rotary wings (3) for aircraft is provided it is attached help lift and motion power, in flight, the lift that each kilogram of Multi-axis aircraft relies on rotary wings (3) and produces propulsive thrust to air, to consume the energy as cost, and use helium balloon (1), on the one hand for integral device provides prevailing lift, it is not only cheap, and be safe, when Multi-axis aircraft is because of unexpected forfeiture power, aircraft will not fall suddenly, but slowly land, this is especially to manned vehicle, it is particularly important.
Beneficial effects of the present invention：Simple structure, low cost can be used for manned low-speed operations, be applicable the special applications such as tourism.
Brief description of the drawings：
Accompanying drawing 1 is structural representation of the invention.
Specific embodiment：
In order that technical scheme becomes more apparent, below in conjunction with drawings and Examples, the present invention is described in more detail, instantiation described herein, is only used to explain the present invention, is not intended to limit the invention.
Embodiment：
Refer to shown in accompanying drawing 1, helium balloon (1) is connected by lifting rope (2) with cockpit (5), rotary wings (3) are connected by connecting rod (4) with cockpit (5), cockpit (5) is positioned at bottom, helium balloon (1) integrally provides most of lift for aircraft, and rotary wings (3) for aircraft is provided the attached power for helping lift and motion.
Claims (1)
1. a kind of helium balloon multiaxis combines aircraft, comprising：Helium balloon (1), lifting rope (2), rotary wings (3), connecting rod (4), cockpit (5)；It is characterized in that：Helium balloon (1) is connected by lifting rope (2) with cockpit (5), rotary wings (3) are connected by connecting rod (4) with cockpit (5), cockpit (5) is positioned at bottom, helium balloon (1) integrally provides most of lift for aircraft, and rotary wings (3) for aircraft is provided the attached power for helping lift and motion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510899459.4A CN106853867A (en) | 2015-12-09 | 2015-12-09 | Helium balloon multiaxis combines aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510899459.4A CN106853867A (en) | 2015-12-09 | 2015-12-09 | Helium balloon multiaxis combines aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106853867A true CN106853867A (en) | 2017-06-16 |
Family
ID=59132771
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510899459.4A Pending CN106853867A (en) | 2015-12-09 | 2015-12-09 | Helium balloon multiaxis combines aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106853867A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444629A (en) * | 2017-08-11 | 2017-12-08 | 广州光使者科技应用有限公司 | A kind of unmanned plane electric power system and unmanned plane |
-
2015
- 2015-12-09 CN CN201510899459.4A patent/CN106853867A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444629A (en) * | 2017-08-11 | 2017-12-08 | 广州光使者科技应用有限公司 | A kind of unmanned plane electric power system and unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |