CN204507264U - A kind of safe manned craft - Google Patents
A kind of safe manned craft Download PDFInfo
- Publication number
- CN204507264U CN204507264U CN201520182153.2U CN201520182153U CN204507264U CN 204507264 U CN204507264 U CN 204507264U CN 201520182153 U CN201520182153 U CN 201520182153U CN 204507264 U CN204507264 U CN 204507264U
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- aircraft
- aircraft body
- manned
- screw propeller
- safe
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Abstract
The utility model discloses a kind of safe manned craft, comprise screw propeller and aircraft body, screw propeller is provided with above described aircraft body, described screw propeller bottom is provided with driving device, described driving device bottom is connected with motor, described aircraft body interior is provided with a freely movable surge bunker, the inside of described surge bunker is provided with manned capsule, described aircraft body both sides are provided with wing, described wing is provided with rotating parachute, described aircraft body lower part is provided with support wheel, this safe manned craft, by arranging a rotating parachute above wing, during normal flight, rotating parachute rotates by the effect of driving engine and transmission shaft, thus play a part lifting aircraft own wt and promote aircraft to advance, once run into fault or other extraordinary circumstances, rotating parachute just plays a part parachute, aircraft is made to be unlikely to decline with very fast speed, protect so layer by layer, slow down impulsive force, make the people in manned storehouse very safe.
Description
Technical field
The utility model relates to vehicle technology field, is specially a kind of safe manned craft.
Background technology
Existing aircraft, no matter how advanced it has, safety performance is one all the time major issue to be solved, once flight. and having there is fault aloft in device, self will dissolve, the tragedy of fatal crass will occur without handful.This be due to the design of current aircraft be more consider it whether fly more scientific rationally, speed whether sooner, whether more economize energy, whether more luxurious, comfortable etc.As for the problem of safety, not that designer does not consider, but the guiding theory that they consider does not jump out the circle of existing conventional aircraft all the time, does not do large change, therefore fundamentally can not solve the safety problem of current aircraft to the principle of aircraft, large structure.
Utility model content
The purpose of this utility model is to provide a kind of safe manned craft, to solve the problem proposed in above-mentioned background technology.
For achieving the above object, the utility model provides following technical scheme: a kind of safe manned craft, comprise screw propeller and aircraft body, screw propeller is provided with above described aircraft body, described screw propeller bottom is provided with driving device, described driving device bottom is connected with motor, described aircraft body interior is provided with a freely movable surge bunker, the inside of described surge bunker is provided with manned capsule, described manned capsule is connected with surge bunker by hinge, described aircraft body both sides are provided with wing, described wing is provided with rotating parachute, described aircraft body lower part is provided with support wheel.
Preferably, described rotating parachute top is provided with wind groove, makes it have the function of screw propeller, is provided with blinker wind groove is other, and when rotating parachute stops operating, blinker groove of keeping watch covers.
Preferably, described wing top can also be provided with the solar panels for providing power.
Compared with prior art, the beneficial effects of the utility model are: this safe manned craft, by arranging a rotating parachute above wing, during normal flight, rotating parachute rotates by the effect of driving engine and transmission shaft, thus play a part lifting aircraft own wt and promote aircraft to advance, once run into fault or other extraordinary circumstances, rotating parachute just plays a part parachute, aircraft is made to be unlikely to decline with very fast speed, aircraft and earth surface be support wheel, filled again in aircraft one completely can be freely movable wherein surge bunker, manned storehouse is hung upside down with universal coupling again at the inner face top of surge bunker, it has lifting aircraft own wt and promotes the effect of aircraft advance, run into extraordinary circumstances and can play a part parachute again, again surge bunker is housed in aircraft, protect so layer by layer, slow down impulsive force layer by layer, make the people in manned storehouse very safe.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation.
In figure: 1 screw propeller, 2 drivings device, 3 motors, 4 aircraft bodies, 5 universal couplings, 6 surge bunkers, 7 manned capsules, 8 support wheels, 9 wings, 10 rotating parachutes.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Refer to Fig. 1, the utility model provides a kind of technical scheme: a kind of safe manned craft, comprise screw propeller 1 and aircraft body 4, screw propeller 1 is provided with above aircraft body 4, screw propeller 1 bottom is provided with driving device 2, driving device 2 bottom is connected with motor 3, aircraft body 4 inside is provided with a freely movable surge bunker 6, the inside of surge bunker 6 is provided with manned capsule 7, manned capsule 7 is connected with surge bunker 6 by hinge, aircraft body 4 both sides are provided with wing 9, wing 9 is provided with rotating parachute 10, rotating parachute 10 top is provided with wind groove, make it have the function of screw propeller, on wind groove side, blinker is installed, when rotating parachute stops operating, wing 9 top can also be provided with the solar panels for providing power, aircraft body 4 bottom is provided with support wheel 8.
Principle of work: by arranging a rotating parachute 10 above wing 9, during normal flight, rotating parachute 10 rotates by the effect of driving engine 3 and transmission shaft 2, thus play a part lifting aircraft own wt and promote aircraft to advance, once run into fault or other extraordinary circumstances, rotating parachute 9 just plays a part parachute, aircraft is made to be unlikely to decline with very fast speed, aircraft and earth surface be support wheel 8, filled again in aircraft one completely can be freely movable wherein surge bunker 6, manned storehouse 7 is hung upside down with universal coupling 5 again at the inner face top of surge bunker 6, it has lifting aircraft own wt and promotes the effect of aircraft advance, run into extraordinary circumstances and can play a part parachute again, in aircraft, surge bunker 6 is housed again, protect so layer by layer, slow down impulsive force layer by layer, make the people in manned storehouse very safe.
Although illustrate and described embodiment of the present utility model, for the ordinary skill in the art, be appreciated that and can carry out multiple change, amendment, replacement and modification to these embodiments when not departing from principle of the present utility model and spirit, scope of the present utility model is by claims and equivalents thereof.
Claims (3)
1. a safe manned craft, comprise screw propeller and aircraft body, it is characterized in that: above described aircraft body, be provided with screw propeller, described screw propeller bottom is provided with driving device, described driving device bottom is connected with motor, described aircraft body interior is provided with a freely movable surge bunker, the inside of described surge bunker is provided with manned capsule, described manned capsule is connected with surge bunker by hinge, described aircraft body both sides are provided with wing, described wing is provided with rotating parachute, and described aircraft body lower part is provided with support wheel.
2. the safe manned craft of one according to claim 1, is characterized in that: described rotating parachute top is provided with wind groove, makes it have the function of screw propeller, is provided with blinker on wind groove side.
3. the safe manned craft of one according to claim 1, is characterized in that: described wing top can also be provided with the solar panels for providing power.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520182153.2U CN204507264U (en) | 2015-03-27 | 2015-03-27 | A kind of safe manned craft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520182153.2U CN204507264U (en) | 2015-03-27 | 2015-03-27 | A kind of safe manned craft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204507264U true CN204507264U (en) | 2015-07-29 |
Family
ID=53705257
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520182153.2U Expired - Fee Related CN204507264U (en) | 2015-03-27 | 2015-03-27 | A kind of safe manned craft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204507264U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892099A (en) * | 2017-03-15 | 2017-06-27 | 深圳市雷凌广通技术研发有限公司 | A kind of strong energy-saving unmanned plane of endurance |
| CN106892096A (en) * | 2017-03-08 | 2017-06-27 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being easy to safe flight |
-
2015
- 2015-03-27 CN CN201520182153.2U patent/CN204507264U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892096A (en) * | 2017-03-08 | 2017-06-27 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being easy to safe flight |
| CN106892096B (en) * | 2017-03-08 | 2019-02-01 | 黑龙江美来天鹰科技服务有限公司 | A kind of Intelligent unattended machine convenient for safe flight |
| CN106892099A (en) * | 2017-03-15 | 2017-06-27 | 深圳市雷凌广通技术研发有限公司 | A kind of strong energy-saving unmanned plane of endurance |
| CN106892099B (en) * | 2017-03-15 | 2019-01-29 | 广东创意双星科技股份有限公司 | A kind of energy-saving unmanned plane that cruising ability is strong |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150729 Termination date: 20160327 |