CN202923886U - Plane with high safety - Google Patents
Plane with high safety Download PDFInfo
- Publication number
- CN202923886U CN202923886U CN 201220540643 CN201220540643U CN202923886U CN 202923886 U CN202923886 U CN 202923886U CN 201220540643 CN201220540643 CN 201220540643 CN 201220540643 U CN201220540643 U CN 201220540643U CN 202923886 U CN202923886 U CN 202923886U
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- China
- Prior art keywords
- screw propeller
- plane
- aircraft
- fuselage
- wing
- 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.)
- Expired - Fee Related
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Abstract
The utility model provides a plane with high safety. The plane comprises a plane body and wings on the two sides of the plane body, wherein the wings are respectively provided with a screw propeller, each screw propeller is controlled by an engine, the engines on two wings are connected through a shaft, and a control device is arranged on the shaft; and a screw propeller is arranged on the head of the plane body, and the screw propeller is connected with an engine in the plane body through a connecting device. The dangerous coefficient of the plane is low; when the two-side screw propellers of the plane are wrong, the screw propeller arranged on the head of the plane can play the role, so that the flying safety is guaranteed; and meanwhile, the plane is rapid to take off, and the plane can directly move ahead without slowly changing.
Description
Technical field
The utility model relates to a kind of aircraft, is specifically related to the high aircraft of a kind of safety performance.
Background technology
Osprey aircraft produced in USA is a more successful multipurpose aircraft, can take off vertically as helicopter, revolves and stops, also can horizontal flight as fixed-wing, be fit to complicated landing field landing, and the infantry delivers sharp weapon.But, because the osprey aircraft is first to take off, and then converting flight forward to, speed of response is slow; There is certain danger in the osprey aircraft in addition, and when the screw propeller on wing arbitrary limit damaged, aircraft can crash because of lack of equilibrium.
The utility model content
The utility model has designed the high aircraft of a kind of safety performance for above-mentioned shortcoming, and purpose is: improve the safety performance of aircraft, promote aircraft power.
Technical solution of the present utility model:
The aircraft that a kind of safety performance is high, comprise fuselage and fuselage both sides wing, screw propeller respectively is installed on wing, screw propeller passes through engine control, connect by axle between the driving engine of both sides, be provided with control setup on axle, it is characterized in that: described fuselage head is equipped with screw propeller, and described screw propeller is connected with driving engine in fuselage head by connecting device.
Described connecting device is drive link.
The beneficial effects of the utility model:
This aircraft danger coefficient is low, and when aircraft both sides screw propeller discovery fault, the screw propeller of aeroplane nose can play a role, and has guaranteed the safety of flight, and any machine et out of order does not affect aircraft landing.Originally take off simultaneously soon, do not need slowly to change again flight forward, can directly move ahead.
Description of drawings
Fig. 1 is the utility model structural representation.
The specific embodiment
Describe the utility model in detail below in conjunction with drawings and Examples.
As shown in Figure 1: the aircraft that a kind of safety performance is high, comprise fuselage 1 and fuselage both sides wing 2, screw propeller 3 and screw propeller 4 respectively are installed on wing 2, screw propeller 3 is controlled by driving engine 5, screw propeller 4 is controlled by driving engine 6, connects by axle 10 between driving engine 5 and driving engine 6, is provided with control setup on axle 10, described fuselage 1 head is equipped with screw propeller 7, and described screw propeller 7 is connected by the interior driving engine 8 of drive link 9 and fuselage 1 head.
The specific works process:
Embodiment 1:
When taking off, adjust axle 10 by control setup, make the screw propeller 3 of fuselage 1 both sides wing and screw propeller 4 in vertical direction, after aircraft flies to certain altitude, adjust axle 10 by control setup again, make screw propeller 3 and the screw propeller 4 of fuselage both sides wing be parallel direction, aircraft flies forward.Take up an official post on one side screw propeller et out of order of aircraft wing, at this moment, close the screw propeller of wing another side in flight course, starts simultaneously the screw propeller 7 of fuselage 1 head, and fuselage continues flight, has reduced danger coefficient.
Embodiment 2:
When taking off, adjust axle 10 by control setup, make the screw propeller 3 of fuselage both sides wing and screw propeller 4 in vertical direction, start simultaneously the screw propeller 7 of aeroplane nose, after aircraft flies to certain altitude, then adjust axle 10 by control setup, make screw propeller 3 and the screw propeller 4 of fuselage both sides wing be parallel direction, aircraft flies forward, and the screw propeller 7 of aeroplane nose has effectively increased the power of aircraft.If in flight course, take up an official post on one side screw propeller et out of order of aircraft wing, at this moment, close the screw propeller of wing another side, the screw propeller 7 by fuselage 1 head drives aircrafts and continues flight, has guaranteed the safety of flight.
In above-described embodiment, taking off and land can be according to different place, arbitrarily operation.
Claims (2)
1. aircraft that safety performance is high, comprise fuselage and fuselage both sides wing, screw propeller respectively is installed on the wing of both sides, screw propeller passes through engine control, connect by axle between the wing engine of both sides, control setup is installed on axle, it is characterized in that: described fuselage head is equipped with screw propeller, and described screw propeller is connected with driving engine in fuselage head by connecting device.
2. the high aircraft of a kind of safety performance as claimed in claim 1, it is characterized in that: described connecting device is drive link.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220540643 CN202923886U (en) | 2012-10-22 | 2012-10-22 | Plane with high safety |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220540643 CN202923886U (en) | 2012-10-22 | 2012-10-22 | Plane with high safety |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202923886U true CN202923886U (en) | 2013-05-08 |
Family
ID=48213873
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220540643 Expired - Fee Related CN202923886U (en) | 2012-10-22 | 2012-10-22 | Plane with high safety |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202923886U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103318408A (en) * | 2013-06-28 | 2013-09-25 | 李宏生 | Helicopter with main propeller leaning forward |
| CN105711831A (en) * | 2016-04-25 | 2016-06-29 | 长江大学 | Vertical take-off and landing type fixed-wing unmanned aerial vehicle |
| CN106275458A (en) * | 2015-06-23 | 2017-01-04 | 张怡月 | A kind of equipment not hindering aircraft |
| CN113184177A (en) * | 2021-05-17 | 2021-07-30 | 朱世友 | Tilt-rotor aircraft and power transmission device thereof |
-
2012
- 2012-10-22 CN CN 201220540643 patent/CN202923886U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103318408A (en) * | 2013-06-28 | 2013-09-25 | 李宏生 | Helicopter with main propeller leaning forward |
| CN106275458A (en) * | 2015-06-23 | 2017-01-04 | 张怡月 | A kind of equipment not hindering aircraft |
| CN105711831A (en) * | 2016-04-25 | 2016-06-29 | 长江大学 | Vertical take-off and landing type fixed-wing unmanned aerial vehicle |
| CN113184177A (en) * | 2021-05-17 | 2021-07-30 | 朱世友 | Tilt-rotor aircraft and power transmission device thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130508 Termination date: 20131022 |