CN104908939A - Making method of helicopter flying and electricity generating dual-purpose airplane - Google Patents
Making method of helicopter flying and electricity generating dual-purpose airplane Download PDFInfo
- Publication number
- CN104908939A CN104908939A CN201410089850.3A CN201410089850A CN104908939A CN 104908939 A CN104908939 A CN 104908939A CN 201410089850 A CN201410089850 A CN 201410089850A CN 104908939 A CN104908939 A CN 104908939A
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- China
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- airplane
- main shaft
- flywheels
- flying
- wings
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Abstract
The invention relates to a making method of a helicopter flying and electricity generating dual-purpose airplane. The helicopter flying and generating dual-purpose airplane is characterized in that two airplane wings with engines rotate around a main shaft through bearing housings, the main shaft is connected with a cabin through a connecting shaft, flywheels driven by the wing engines are respectively arranged above and below the wings, and the flywheels are fixed on an electric generator adopting the main shaft as an axle center. The airplane flies after the two airplane wings with engines are started, the upper and lower flywheels are driven to reversely rotate in order to generate flying force for helping the flying of the airplane, exciting electricity generation of the electric generator fixed on the flywheels is realized, the two airplane wings are connected with the bearing housings on the airplane main shaft in a flying heliciform 180DEG angle manner, the two flywheels above and below each of the wings parallel to the wing and are provided with reverse rotation flying blades, and the flywheels are fixed on engine rotors rotating around the main shaft. Electric generator stators are fixed on the bearing housings rotating opposite to each other. The airplane main shaft is connected with the airplane cabin through the connecting shaft, and forward or backward 0-90DEG adjustment operation cane be realized with the connecting shaft as a summit.
Description
Technical field
The present invention relates to a kind of method for making of going straight up to the dual-purpose aircraft of flight generating; Originally go straight up to the dual-purpose aircraft of flight generating and can go straight up to flight, also can awing generate electricity; More can generate electricity when not flying.
Background technology
Also there is no the correlation technique that similar this kind of aircraft makes at present both at home and abroad; My a kind of method for making of vertical lift horizontal flight aircraft of declaring before this, rotate wing technology although also use, its major constituents and operation scheme therewith aircraft are different.
Summary of the invention
In order to overcome the deficiency of existing autogyro kind and technology, the invention provides a kind of method for making of going straight up to the dual-purpose aircraft of flight generating; This aircraft is rotated around the spindle by bear box by the airplane wings of two band driving engines, and main shaft is connected by adapter shaft with cabin, and wing respectively installs one up and down by the engine-driven flywheel of wing, and it is on the electrical generator in axle center that flywheel is fixed on according to main shaft.The airplane wings of two band driving engines starts rear aircraft and ascends to heaven, and also drives upper and lower flywheel contrarotation to produce lift and helps aircraft to ascend to heaven, and the electrical generator be fixed on flywheel can excitation generate electricity, and also can not excitation not generate electricity.
The technical solution adopted for the present invention to solve the technical problems is: the airplane wings of two band driving engines becomes 180 degree of angles to be connected with the bear box on aircraft main shaft according to spiral fashion of ascending to heaven, upper and lower two flywheels of wing are parallel with wing and contrarotation is housed ascends to heaven blade, and flywheel is fixed on and rotates around the spindle (or on stator) on the rotor of driving engine.Stator (or rotor) is fixed on the bear box of relative contrarotation.Aircraft main shaft and aircraft cabin are connected by adapter shaft and can are the adjustment operation that front and back 0 to an angle of 90 degrees is done on summit according to adapter shaft.
The invention has the beneficial effects as follows, the present invention can make up the deficiency of existing aircraft kind, and this aircraft takeoffs and landings is convenient, and generating of can flying, and even powerful laser equipment can be installed on this aircraft.This aircraft is more suitable for backcountry life, construction, frontier defense traffic and power supply.
Claims (2)
1. go straight up to a method for making for the dual-purpose aircraft of flight generating, this aircraft is rotated around the spindle by bear box by the airplane wings of two band driving engines, it is characterized in that: wing respectively installs one up and down by the engine-driven flywheel of wing.
2., according to this kind of method for making of going straight up to the dual-purpose aircraft of flight generating according to claim 1, it is characterized in that: be fixed on the electrical generator concentric with this aircraft main shaft by the engine-driven flywheel of wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410089850.3A CN104908939A (en) | 2014-03-12 | 2014-03-12 | Making method of helicopter flying and electricity generating dual-purpose airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410089850.3A CN104908939A (en) | 2014-03-12 | 2014-03-12 | Making method of helicopter flying and electricity generating dual-purpose airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104908939A true CN104908939A (en) | 2015-09-16 |
Family
ID=54078475
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410089850.3A Pending CN104908939A (en) | 2014-03-12 | 2014-03-12 | Making method of helicopter flying and electricity generating dual-purpose airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104908939A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3603700A (en) * | 1969-05-19 | 1971-09-07 | Michael Eskeli | Rotating circular wing |
| CN1511758A (en) * | 2002-12-26 | 2004-07-14 | 王立功 | Two stage air power changing method and its changing device for heli craft |
| CN1962361A (en) * | 2006-04-07 | 2007-05-16 | 赵钦 | Helicopter with rotary wing directly propelled by impetus |
| CN201183609Y (en) * | 2008-02-03 | 2009-01-21 | 王培学 | Aerocraft rotor with engine |
| CN203111501U (en) * | 2013-02-01 | 2013-08-07 | 中国航空工业集团公司西安飞机设计研究所 | Rotary type coaxial flight structure |
-
2014
- 2014-03-12 CN CN201410089850.3A patent/CN104908939A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3603700A (en) * | 1969-05-19 | 1971-09-07 | Michael Eskeli | Rotating circular wing |
| CN1511758A (en) * | 2002-12-26 | 2004-07-14 | 王立功 | Two stage air power changing method and its changing device for heli craft |
| CN1962361A (en) * | 2006-04-07 | 2007-05-16 | 赵钦 | Helicopter with rotary wing directly propelled by impetus |
| CN201183609Y (en) * | 2008-02-03 | 2009-01-21 | 王培学 | Aerocraft rotor with engine |
| CN203111501U (en) * | 2013-02-01 | 2013-08-07 | 中国航空工业集团公司西安飞机设计研究所 | Rotary type coaxial flight structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150916 |