CN104163240A - Fast helicopter - Google Patents
Fast helicopter Download PDFInfo
- Publication number
- CN104163240A CN104163240A CN201310201652.7A CN201310201652A CN104163240A CN 104163240 A CN104163240 A CN 104163240A CN 201310201652 A CN201310201652 A CN 201310201652A CN 104163240 A CN104163240 A CN 104163240A
- Authority
- CN
- China
- Prior art keywords
- helicopter
- fast
- turn
- fast helicopter
- screw propeller
- 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
- 230000005484 gravity Effects 0.000 claims description 4
- 238000005265 energy consumption Methods 0.000 abstract 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
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- Toys (AREA)
Abstract
The invention discloses a fast helicopter. A technical scheme of the invention comprises that a forward pushing force is applied to the existing helicopter so that a flight speed is improved. A pushing device is applied to the rear part of the existing helicopter so that the fast helicopter is obtained. The pushing device comprises a pushing engine and a propeller. The fast helicopter can substantially improve a helicopter flight speed in air, shorten flight time, reduce energy consumption, prolong a propeller wing mechanism service life and realize flexible and convenient direction-change, and is an ideal air transport tool.
Description
Technical field:
The present invention relates to one goes straight up to
machine, is specifically related to a kind of fast helicopter.
Background technology:
The outstanding wing to the High Rotation Speed of helicopter dependence at present aloft flies, although buoyancy is very large, the speed of its flight is slow, causes aerial running time long, low with regard to flight efficiency like this, consumes energy high.
Summary of the invention:
The present invention is in order to overcome above the deficiencies in the prior art, and a kind of flying speed helicopter is faster provided, and its technical scheme adopting is: in order to improve flying speed, increase the strength promoting forward to original helicopter.A specifically fast helicopter, is to increase thruster at the rear portion of original helicopter, it is characterized by: described thruster comprises, the screw propeller of trust engine and back, power, by turning cylinder, makes screw propeller High Rotation Speed produce thrust forward, makes the progressive speed of helicopter faster.The outstanding wing of described original helicopter moves to the center of gravity place of fast helicopter backward, and described thruster is fixed on below its center of gravity place, on the rotating disk can level turning to, and has deflecting bar.The present invention has the following advantages compared with existing helicopter: (1) flying speed significantly improves, and work efficiency is high; (2) shorten the flight time, fuel oil reduces relatively; (3) relatively extended outstanding wing mechanism service life; (4) turn to more flexible.
The invention will be further described below to use drawings and Examples
Brief description of the drawings:
Figure is fast helicopter schematic diagram
Description of reference numerals:
1, trust engine 2, screw propeller 3, deflecting bar
Detailed description of the invention:
The mode of fast helicopter flight is:
First start outstanding wing driving engine, it starts lift-off then actuate thrust motor
1, its tail undercarriage
2high Rotation Speed, produces thrust forward, and now, fast helicopter, in lift-off, flies forward fast.
In the time flying to certain altitude, can suitably reduce the delivery quality of outstanding wing driving engine, make fast helicopter no longer increase but still move ahead fast.
In the time need turning to the left or to the right, pull deflecting bar
3trust engine is turned to along level, and screw propeller is by transferring to left back or right abaft to dead aft, and now fast helicopter just turns to the left or to the right, after turning to, pull immediately positive thrust driving engine, and fixing, and fast helicopter just continues to fly fast to dead ahead.While landing, first close trust engine, then the ground of slowly landing.
By finding out above this kind of fast helicopter, flying speed is very fast forward, operates easylier, is desirable air communication transportation means.
Claims (3)
1. a fast helicopter, increases thruster by original helicopter and rear portion and forms, and it is characterized by: described thruster comprises the screw propeller of trust engine and back, and power makes screw propeller High Rotation Speed produce thrust forward by turning cylinder.
2. by fast helicopter claimed in claim 1, it is characterized by: described thruster is fixed on the rotating disk can level turning to below its center of gravity place, and has deflecting bar, need turn to time, can turn to the left or to the right, while not needing to turn to, can be fixed as to dead ahead.
3. by fast helicopter claimed in claim 1, it is characterized by: be the center of gravity place that the outstanding original helicopter wing is moved to backward to fast helicopter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310201652.7A CN104163240A (en) | 2013-05-19 | 2013-05-19 | Fast helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310201652.7A CN104163240A (en) | 2013-05-19 | 2013-05-19 | Fast helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104163240A true CN104163240A (en) | 2014-11-26 |
Family
ID=51907268
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310201652.7A Pending CN104163240A (en) | 2013-05-19 | 2013-05-19 | Fast helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104163240A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120012693A1 (en) * | 2010-07-13 | 2012-01-19 | Eurocopter | Method and an aircraft provided with a swiveling tail rotor |
| WO2012026839A1 (en) * | 2010-08-26 | 2012-03-01 | Shulim Semenovich Shvidler | Helicopter |
| CN102556345A (en) * | 2012-01-18 | 2012-07-11 | 朱晓义 | Aircraft power device |
| CN102700708A (en) * | 2012-06-08 | 2012-10-03 | 朱清华 | Speed-increasing tail device of helicopter |
-
2013
- 2013-05-19 CN CN201310201652.7A patent/CN104163240A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120012693A1 (en) * | 2010-07-13 | 2012-01-19 | Eurocopter | Method and an aircraft provided with a swiveling tail rotor |
| WO2012026839A1 (en) * | 2010-08-26 | 2012-03-01 | Shulim Semenovich Shvidler | Helicopter |
| CN102556345A (en) * | 2012-01-18 | 2012-07-11 | 朱晓义 | Aircraft power device |
| CN102700708A (en) * | 2012-06-08 | 2012-10-03 | 朱清华 | Speed-increasing tail device of helicopter |
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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: 20141126 |