CN104828242A - Jetting system on tailpipe nozzle of jet airplane - Google Patents
Jetting system on tailpipe nozzle of jet airplane Download PDFInfo
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- CN104828242A CN104828242A CN201510234425.3A CN201510234425A CN104828242A CN 104828242 A CN104828242 A CN 104828242A CN 201510234425 A CN201510234425 A CN 201510234425A CN 104828242 A CN104828242 A CN 104828242A
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- jet
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- jet airplane
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Abstract
The invention discloses a jetting system on a tailpipe nozzle of a jet airplane. The jetting system capable of jetting gas toward various directions at any time according to demands is installed on the tailpipe nozzle of the jet airplane, and the sizes and directions of gas flows in the various directions can be continuously adjusted; the jetting system is composed of a high-temperature-resistant hard gas pipe, a soft gas pipe, a gas switch and a direction controller; the gas switch is used for controlling the sizes of the gas flows, the direction controller is used for controlling the directions of the gas flows. After the jetting system is installed on the jet airplane, the jet airplane can realize vertical takeoff and landing, slanting takeoff and landing, and runway takeoff and landing, and is capable of flying front, back, left and right, the balance performance in the air is good, and the security of the jet airplane is improved.
Description
Technical field
The invention belongs to aircraft field, the jet system particularly on a kind of jet airplane jet pipe.
Background technology
Jet airplane flying speed is fast, load carrying ability is large, can high-altitude flight, but it can not vertical lift, can only advance, can not retreat, can not fly, can not fly on the right side, low-altitude low-speed poor performance in a left side, can not revolve in the air and stop.This shortcoming limits its field of application.
Summary of the invention
The present invention is exactly in these cases, provides the jet system on a kind of jet airplane jet pipe.
In order to overcome the shortcoming of jet airplane, draw together its field of application large, increase its safety, the present invention has done following improvement: on the jet pipe of jet airplane, install one additional as required can at any time to the jet system that all directions are jet, and the size and Orientation of all directions air-flow can also continue to regulate as required; This jet system is made up of resistant to elevated temperatures strong-willed pipe, soft air pipe, gas switch, direction controller, the size of gas switch adjustment air-flow, the direction of direction controller adjustment air-flow.
Direction controller has three kinds: connecting rod direction controller, electromagnetism direction controller, gas direction controller.
The jet of this jet system has along spray and returns spray two kinds of forms.
Advantage of the present invention: load onto this jet system and aircraft vertical lifting, oblique lifting, runway lifting, rising or falling speed, flying speed, flying height, heading can be made arbitrarily to regulate; Its impact aloft by air-flow, wind and rain is little, can advance, retreat, left lateral, right lateral; Because its jet size and Orientation all can arbitrarily regulate as required, increase stationarity and the safety of aircraft, therefore it aloft can also revolve and stop.The aircraft loading onto this jet system is a kind of aircraft more outstanding than small bird, insect; People can untrammeledly aloft speed across the sky just as legendary angle.
Accompanying drawing explanation
Fig. 1, Fig. 2, Fig. 3 are that Fig. 4, Fig. 5, Fig. 6 are back jet system along jet system.They are all constructional drawing, do not represent the shape of jet system itself, size, length.
In figure, 1 is jet pipe, and 2 is gas switch, and 3 is resistant to elevated temperatures soft air pipe, 4 is the control stalk of connecting rod direction controller, 5 is operator's compartment, and 6 is the current switch of electromagnetism direction controller, and 7 is the gas switch of gas direction controller, 8,9 front and back are respectively along jet pipe, 10,11 be respectively left and right along jet pipe, 12 is lower to jet pipe, and 13,14 are respectively front and back returns jet pipe, 15,16 be respectively left and right and return jet pipe, 17 is jet pipe next time.
According to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, embodiments of the invention are elaborated below.
Detailed description of the invention
Fig. 1, Fig. 2, Fig. 3 are the suitable jet system be contained on jet airplane jet pipe, are made up of gas switch 2, resistant to elevated temperatures soft air pipe 3, strong-willed pipe and direction controller.System gas main front end is connected with jet airplane jet pipe, then along jet pipe 8 and direction controller thereof before loading onto successively, left and right is along jet pipe 10,11 and their direction controller, lower to jet pipe 12 and direction controller thereof, rear along jet pipe 9 and direction controller thereof.These three jet systems of Fig. 1, Fig. 2, Fig. 3 except direction controller difference, other identical.Gas switch 2 controls the size of air-flow, and direction controller controls the direction of air-flow.
Fig. 4, Fig. 5, Fig. 6 are time jet system be contained on jet airplane jet pipe, compared with Fig. 1, Fig. 2, Fig. 3, they are also made up of gas switch 2, resistant to elevated temperatures soft air pipe 3, strong-willed pipe and direction controller, the effect of each constituent elements is also identical respectively, different just jet pipe turned 180 degree curved, therefore its jet direction is also contrary with the jet direction of Fig. 1, Fig. 2, Fig. 3.
Connecting rod direction controller is that control stalk 4 is fixedly connected with terminal gas ejector pipe, owing to having one section of soft air pipe 3 in the middle of jet pipe, so can by change the mouth of pipe that control stalk 4 changes terminal gas ejector pipe towards, thus reach the object changing air flow line.
Irony for terminal gas ejector pipe, the middle jet pipe having again one section of soft air pipe 3, electromagnetism direction controller can also be adopted, by the current switch 6 of electromagnetism direction controller controls the presence or absence of electric current, size, direction change electromagnetic field presence or absence, size, direction, the mouth of pipe of the Magnetic Control terminal irony gas ejector pipe produced by electromagnetic field again towards, thus reach the object changing air flow line.
Gas direction controller loads onto side air jet system in the surrounding of terminal gas ejector pipe, the nozzle hole of side spray device of air faces terminal gas ejector pipe, because there is again one section of soft air pipe 3 centre, so it can control the size of side spray gas by the gas switch 7 of gas direction controller, again by the size control terminal gas ejector pipe of side spray gas the mouth of pipe towards, thus reach and change the object of air flow line.
As mentioned above; jet system on jet airplane jet pipe of the present invention; described embodiment and figure; the just implementation result in five directions of the present invention; be not be confined to the present invention; the present invention also comprises the jet system being contained in four direction on jet airplane jet pipe, three directions, two directions, a direction, and approximate, the identical person such as structure every and of the present invention, feature, all should belong to protection scope of the present invention.
Claims (2)
1. the jet system on a jet airplane jet pipe, it is characterized in that: on jet airplane jet pipe, load onto one can as required at any time to the jet system that all directions are jet, and the size of this system all directions air-flow, direction can also continue to regulate as required; This jet system is made up of resistant to elevated temperatures strong-willed pipe, soft air pipe, gas switch, direction controller; Gas switch controls the size of air-flow, and direction controller controls the direction of air-flow.
2. the jet system on jet airplane jet pipe according to claim 1 is included in the jet system in five directions that jet pipe is loaded onto, the jet system of four direction, the jet system in three directions, the jet system in two directions, the jet system in a direction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201510234425.3A CN104828242A (en) | 2015-05-03 | 2015-05-03 | Jetting system on tailpipe nozzle of jet airplane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201510234425.3A CN104828242A (en) | 2015-05-03 | 2015-05-03 | Jetting system on tailpipe nozzle of jet airplane |
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CN104828242A true CN104828242A (en) | 2015-08-12 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201510234425.3A Pending CN104828242A (en) | 2015-05-03 | 2015-05-03 | Jetting system on tailpipe nozzle of jet airplane |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107512386A (en) * | 2017-08-19 | 2017-12-26 | 中国矿业大学 | A kind of mine air power high-speed aircraft and control method |
Citations (6)
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CN2188544Y (en) * | 1994-04-09 | 1995-02-01 | 卢杲 | Flying disc |
US6105364A (en) * | 1989-10-11 | 2000-08-22 | Rolls-Royce Plc | Vstovl engines |
CN1405063A (en) * | 2002-11-11 | 2003-03-26 | 金洪奎 | Structure of controlling flying posture of aircraft |
CN1693691A (en) * | 2005-04-30 | 2005-11-09 | 张鸿元 | Air compression aeroengine |
CN101857085A (en) * | 2010-06-03 | 2010-10-13 | 刘春� | Aircraft |
CN203428023U (en) * | 2013-08-22 | 2014-02-12 | 李军红 | Taking-off and landing assistance device for shipboard aircraft |
-
2015
- 2015-05-03 CN CN201510234425.3A patent/CN104828242A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6105364A (en) * | 1989-10-11 | 2000-08-22 | Rolls-Royce Plc | Vstovl engines |
CN2188544Y (en) * | 1994-04-09 | 1995-02-01 | 卢杲 | Flying disc |
CN1405063A (en) * | 2002-11-11 | 2003-03-26 | 金洪奎 | Structure of controlling flying posture of aircraft |
CN1693691A (en) * | 2005-04-30 | 2005-11-09 | 张鸿元 | Air compression aeroengine |
CN101857085A (en) * | 2010-06-03 | 2010-10-13 | 刘春� | Aircraft |
CN203428023U (en) * | 2013-08-22 | 2014-02-12 | 李军红 | Taking-off and landing assistance device for shipboard aircraft |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107512386A (en) * | 2017-08-19 | 2017-12-26 | 中国矿业大学 | A kind of mine air power high-speed aircraft and control method |
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Application publication date: 20150812 |
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