CN102126556A - Vertical take-off and landing small-sized airplane - Google Patents
Vertical take-off and landing small-sized airplane Download PDFInfo
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- CN102126556A CN102126556A CN2010102635114A CN201010263511A CN102126556A CN 102126556 A CN102126556 A CN 102126556A CN 2010102635114 A CN2010102635114 A CN 2010102635114A CN 201010263511 A CN201010263511 A CN 201010263511A CN 102126556 A CN102126556 A CN 102126556A
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Abstract
The invention discloses a vertical take-off and landing small-sized airplane which not only can vertically take off and land, but also utilizes the gliding of the wings of the airplane to save much kinetic energy, is high in speed and simple in driving and is safe, and the wings can be folded; and fan-shaped wings can be unfolded under the condition that the airplane stops suddenly during flying, thus the airplane can safely glide to the ground. According to the kinetic energy generated by propellers arranged on the wings of the airplane is utilized, and the angle between the wings of the airplane and the propeller is changed simultaneously, thus the airplane can vertically take off, land and fly forwards. The small-sized airplane provided by the invention has the advantages of novel design, reasonable structure, simplicity in operation, safety and practicability, is an ideal vehicle developed in the air in future, has better market prospects and is convenient to implement and popularize.
Description
Technical field
The present invention relates to a kind of blimp of energy vertical takeoff and landing
Background technology
Since aircraft and automobile have been arranged, bring great convenience with quick to people's trip.Though passenger plane speed is fast, can not vertical takeoff and landing, need very long airfield runway.Go straight up to the function vertical takeoff and landing, but speed not very fast, can not utilize the glide of wing can save a lot of kinetic energy.
Along with increasing of city vehicle, traffic jam also is the big obstacle that it is inconvenient that people go on a journey.
Summary of the invention
Of the present invention can vertical takeoff and landing blimp, can not only vertical takeoff and landing, do not need the airport way, also can utilize the glide of wing can save a lot of kinetic energy as passenger plane.And speed is fast, safety, driving are simple.Wing can also be folded up, and reduces to take up an area of the space.
Driving engine is shut down in emergency circumstances suddenly when aircraft flight, can launch fan type wing, has so just increased the area of wing, and aircraft just can be as the aerodone ground of more safely gliding.In today that Modern Traffic is blocked up, be a megatrend to aerial development.
The present invention realizes like this, two jiaos are equipped with attaching parts on behind the aircraft handling chamber, in the middle of going up angle connector and aircraft wing behind the operator's compartment turning cylinder is arranged, aircraft wing and screw propeller can be the center with the turning cylinder of centre like this, rotate aircraft wing and screw propeller simultaneously with 90 ° angles.Utilization is installed in the kinetic energy that the screw propeller on the aircraft wing produces, and changes the angle of aircraft wing and screw propeller simultaneously, so just can make aircraft vertical takeoff and landing and flight forward.
Modern design of the present invention, rational in infrastructure, safe and practical, simple to operate, be the following desirable vehicle to aerial development.Have good practical values and market outlook, be convenient to implement to promote.
Description of drawings
Fig. 1 is the front view of the present invention when flying.
Structural representation when Fig. 2 is a vertical takeoff and landing of the present invention.
Fig. 3 is the birds-eye view that the present invention opens up fan type wing.
Fig. 4 is the birds-eye view behind the folded wing of the present invention.
Fig. 5 is the left view behind the folded wing of the present invention.
The specific embodiment
Below in conjunction with accompanying drawing the present invention is further described.
With reference to accompanying drawing, the blimp of energy vertical takeoff and landing is by properller, turning cylinder, angle connector, aircraft wing and collapsible fan type wing are gone up in the aircraft handling chamber behind the operator's compartment, tail support behind the aircraft, empennage many parts are formed after aircraft vertical back empennage and the aircraft level.
Going up angle connector and turning cylinder and wing behind the operator's compartment is bonded assembly, and turning cylinder and wing are rotary, and can make aircraft wing and screw propeller like this is the center with the turning cylinder, rotates aircraft wing and screw propeller simultaneously with 90 ° angles.
When aircraft wing vertically downward the time, when properller rotated like this, aircraft just can vertical takeoff and landing.When aircraft wing was parallel with aircraft, when at this moment screw propeller rotated, aircraft will fly forward.
Screw propeller (1) is connected with aircraft wing (5) with turning cylinder (2).Going up angle connector (4) behind operator's compartment (3) and the operator's compartment is connected with turning cylinder (2).Wing (5) is connected with collapsible fan type wing (6).Back tail support (7) is installed in operator's compartment (3) back medium position.Vertical back empennage (8) is installed in tail support (7) afterbody top position, back.Empennage after the level (9) is installed in back tail support (7) tail position.
Claims (3)
1. blimp that can vertical takeoff and landing goes up angle connector behind the blimp of empennage and screw propeller, turning cylinder, the operator's compartment behind the tail support, the vertical back of aircraft empennage, aircraft level after by aircraft wing, aircraft handling chamber, aircraft and collapsible fan type wing many parts are formed.
2. vertical takeoff and landing blimp according to claim 1 is characterized in that the following and turning cylinder (2) that screw propeller (1) is installed in wing (5) is connected.Last angle connector (4) and wing (5) are bonded assemblys behind turning cylinder (2) and the operator's compartment, and turning cylinder (2) and wing (5) are rotary.The purpose that requires is exactly to make aircraft wing can change different angles simultaneously with screw propeller.
3. vertical takeoff and landing blimp according to claim 1 is characterized in that collapsible fan type wing (6) is installed in the two ends of aircraft wing (5).Its objective is in case of emergency and can launch at any time.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102635114A CN102126556A (en) | 2010-08-20 | 2010-08-20 | Vertical take-off and landing small-sized airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102635114A CN102126556A (en) | 2010-08-20 | 2010-08-20 | Vertical take-off and landing small-sized airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102126556A true CN102126556A (en) | 2011-07-20 |
Family
ID=44264903
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010102635114A Pending CN102126556A (en) | 2010-08-20 | 2010-08-20 | Vertical take-off and landing small-sized airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102126556A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102849211A (en) * | 2012-09-28 | 2013-01-02 | 宋新民 | Variable power vertical short-distance takeoff landing aircraft with fixed wings |
| CN107244410A (en) * | 2017-06-13 | 2017-10-13 | 昆明鞘翼科技有限公司 | A kind of method of wing coordinated flight state using imitative beetle elytrum |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6367736B1 (en) * | 1999-06-02 | 2002-04-09 | Agusta S.P.A. | Convertiplane |
| CN1458030A (en) * | 2003-05-26 | 2003-11-26 | 韩培洲 | Horizontal and vertical take-off and landing plane with tilted front rotary wing |
| CN1993264A (en) * | 2004-07-29 | 2007-07-04 | 贝尔直升机泰克斯特龙公司 | Method and apparatus for flight control of tiltrotor aircraft |
| CN200939356Y (en) * | 2006-08-22 | 2007-08-29 | 青岛天骄无人机遥感技术有限公司 | Small remote monitoring pilotless plane |
| KR20090101413A (en) * | 2009-08-21 | 2009-09-28 | 곽상호 | Vertical takedff and landingairplane |
-
2010
- 2010-08-20 CN CN2010102635114A patent/CN102126556A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6367736B1 (en) * | 1999-06-02 | 2002-04-09 | Agusta S.P.A. | Convertiplane |
| CN1458030A (en) * | 2003-05-26 | 2003-11-26 | 韩培洲 | Horizontal and vertical take-off and landing plane with tilted front rotary wing |
| CN1993264A (en) * | 2004-07-29 | 2007-07-04 | 贝尔直升机泰克斯特龙公司 | Method and apparatus for flight control of tiltrotor aircraft |
| CN200939356Y (en) * | 2006-08-22 | 2007-08-29 | 青岛天骄无人机遥感技术有限公司 | Small remote monitoring pilotless plane |
| KR20090101413A (en) * | 2009-08-21 | 2009-09-28 | 곽상호 | Vertical takedff and landingairplane |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102849211A (en) * | 2012-09-28 | 2013-01-02 | 宋新民 | Variable power vertical short-distance takeoff landing aircraft with fixed wings |
| CN107244410A (en) * | 2017-06-13 | 2017-10-13 | 昆明鞘翼科技有限公司 | A kind of method of wing coordinated flight state using imitative beetle elytrum |
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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 | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110720 |