CN104071331B - The gyro-stabilized jet airship of a kind of employing - Google Patents
The gyro-stabilized jet airship of a kind of employing Download PDFInfo
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- CN104071331B CN104071331B CN201410285200.6A CN201410285200A CN104071331B CN 104071331 B CN104071331 B CN 104071331B CN 201410285200 A CN201410285200 A CN 201410285200A CN 104071331 B CN104071331 B CN 104071331B
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- airship
- storehouse
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- spray orifice
- gyro
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Abstract
The invention discloses the gyro-stabilized jet airship of a kind of employing, comprise annular carrying manipulation storehouse, driving engine, fan blade, flight stability gyro, flight control system, the center in annular carrying manipulation storehouse is provided with cylindricality air passage, annular carrying manipulation storehouse manipulates storehouse base plate with the carrying arranged thereunder and is connected, be dish-shaped high pressure gas storehouse between carrying manipulation storehouse base plate and airship base plate, air passage is connected with dish-shaped high pressure gas storehouse, driving engine is arranged in air passage, fan blade is positioned at air passage and is arranged on the upper output shaft of driving engine, flight stability gyro is arranged on the lower output shaft of driving engine, airship base plate is provided with lift spray orifice, and airship cylindrical is evenly provided with horizontal flight spray orifice, gas curtain spray orifice, lift spray orifice, horizontal flight spray orifice are connected with high pressure gas storehouse.This airship safety and stability, energy-conserving and environment-protective, can under complex space environment, particularly can do the actions such as up, down, left, right, before and after hovering in high and low sky or narrow, complex space and can stabilized flight.
Description
Technical field
The present invention relates to flight instruments, specifically the gyro-stabilized jet airship of a kind of employing.
Background technology
For a long time, the mankind to flight to find out enthusiasm lasting, the mankind served by the aircraft of the many types of innovation and creation.But these aircraft are very high to flight space environmental requirement, flight attitude is difficult to control and change, and therefore, there is very large flight limitation and potential safety hazard.Meanwhile, the aircraft that the current mankind commonly use is all carbon isotopes, is unfavorable for sustainable development.
Summary of the invention
The object of the invention is for the deficiencies in the prior art, and one safety and stability is more provided, energy-conserving and environment-protective, can under complex space environment, particularly can do the actions such as up, down, left, right, before and after hovering in high and low sky or narrow, complex space and can the gyro-stabilized jet airship of employing of stabilized flight.
The object of the invention is to be realized by following technical scheme:
The gyro-stabilized jet airship of a kind of employing, comprises annular carrying manipulation storehouse, driving engine, fan blade, flight stability gyro, flight control system,
The center in described annular carrying manipulation storehouse is provided with cylindricality air passage, annular carrying manipulation storehouse manipulates storehouse base plate with the carrying arranged thereunder and is connected, be dish-shaped high pressure gas storehouse between carrying manipulation storehouse base plate and airship base plate, air passage is connected with dish-shaped high pressure gas storehouse, driving engine is arranged in air passage, fan blade is positioned at air passage and is arranged on the upper output shaft of driving engine, flight stability gyro is arranged on the lower output shaft of driving engine, flight stability gyro is positioned at high pressure gas storehouse, the direction of rotation of flight stability gyro and fan blade during operation;
The cylindrical evenly densely covered gas curtain spray orifice of described airship base plate, airship base plate is provided with multiple lift spray orifice controlling to open, close, and airship cylindrical is evenly provided with the horizontal flight spray orifice that can control to open, close;
Described gas curtain spray orifice, lift spray orifice, horizontal flight spray orifice are connected with high pressure gas storehouse.
Emergency power storehouse is provided with in the top in described carrying manipulation storehouse.
Described emergency power storehouse internal memory emergency power parachute.
Described emergency power storehouse is annular bin.
Described airship base plate is provided with alighting gear.
Fan blade under the drive of driving engine in air passage high speed rotating, by the air above airship through the suction suitable for reading of central aeration road, make to form zone of negative pressure above flying saucer, the air sucked enters high pressure gas storehouse after fan blade pressurization, the gas curtain spray orifice ejection that part gas in high pressure gas storehouse is gathered by airship base plate cylindrical, airship base plate circumference is made to form one circular curtain, gas curtain forces the air accumulation sprayed through airship base plate lift spray orifice bottom airship, make to form partial high pressure bottom airship, like this, a maximum effective pressure is created poor between zone of negative pressure above the higher-pressure region of airship bottom and airship, and act on bottom whole airship.Bottom area due to airship is equivalent to the area of conter of airship, makes airship obtain maximum effective lift area, and therefore, this airship only need consume less power just can obtain larger lift, and this airship can be floated flight in atmosphere.This is aircraft most effective at present.Therefore, this airship very energy-saving and environmental protection.
Airship base plate evenly arranges controollable lift spray orifice, controls the open and close of corresponding site spray orifice, and what regulate spray orifice to open is large and small, can realize controlling stablizing of airship lifting and flight attitude.Control horizontal flight spray orifice on one side to open, airship will fly to reversing sense, because airship is evenly distributed in horizontal flight spray orifice, therefore, airship flight does not need to turn or turn around, only need control corresponding rightabout horizontal flight spray orifice to open and just can realize the flight of required any direction, flight maneuver is flexible, and can do the actions such as up, down, left, right, before and after hovering and energy stabilized flight in high and low sky or narrow, complex space.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment of the present invention.
In figure, 1. alighting gear 2. airship base plate 3. flight stability gyro 4. carrying manipulation base plate 5. driving engine 6. fan blade 7. air passage 8. emergency power storehouse 9., storehouse annular carrying manipulation storehouse 10. engine mount 11. high pressure gas storehouse 12. horizontal flight spray orifice 13. gas curtain spray orifice 14. lift spray orifice.
Detailed description of the invention
Below in conjunction with drawings and Examples, content of the present invention is further elaborated, but is not limitation of the invention.
Embodiment:
With reference to Fig. 1, the gyro-stabilized jet airship of a kind of employing, comprises annular carrying manipulation storehouse 9, driving engine 5, fan blade 6, flight stability gyro 3, flight control system,
The center in described annular carrying manipulation storehouse 9 is provided with cylindricality air passage 7, annular carrying manipulation storehouse 9 manipulates storehouse base plate 4 with the carrying arranged thereunder and is connected, be dish-shaped high pressure gas storehouse 11 between carrying manipulation storehouse base plate 4 and airship base plate 2, air passage 7 is connected with dish-shaped high pressure gas storehouse 11, driving engine 5 is arranged in air passage 7, fan blade 6 is positioned at air passage 7 and is arranged on the upper output shaft of driving engine 5, flight stability gyro 3 is arranged on the lower output shaft of driving engine 5, flight stability gyro 3 is positioned at high pressure gas storehouse 11, the direction of rotation of flight stability gyro 3 and fan blade 6 during operation, the moment of torsion produced when starting with cancel each other fan blade 6 and flight stability gyro 3 and accelerate, airship is made steadily to take off and accelerate.
The cylindrical evenly densely covered gas curtain spray orifice 13 of described airship base plate 2, airship base plate 2 is provided with multiple lift spray orifice 14 controlling to open, close, and airship cylindrical is evenly provided with the horizontal flight spray orifice 12 that can control to open, close;
Described gas curtain spray orifice 13, lift spray orifice 14, horizontal flight spray orifice 12 are connected with high pressure gas storehouse 11.
Emergency power storehouse 8 is provided with in the top in described carrying manipulation storehouse 9.
Described emergency power storehouse 8 internal memory emergency power parachute.
Described emergency power storehouse 8 is annular bin.
Described airship base plate 2 is provided with alighting gear 1.
The air passage of cylindricality described in this example 7 is cylindrical airway.
Described driving engine 5 is connected with fan blade 6, flight stability gyro 3 by change speed gear box.The optional electrical motor of driving engine 5, can adopt solar power to provide electric power; Driving engine 5 also can select engine fuel.
Schematically, represent the rotation direction of fan blade 6, flight stability gyro 3 respectively, all the other arrows schematically show the sense of motion of gas to the horizontal curved arrow at fan blade 6, flight stability gyro 3 place.
Driving engine 5 power be arranged on engine mount 10 passes to fan blade 6 and flight stability gyro 3 by change speed gear box.Fan blade 6 driving engine 5 under the drive of change speed gear box in central aeration road 7 high speed rotating, by the air above airship through central aeration road 7 suction suitable for reading, make to form zone of negative pressure above airship.The air sucked enters high pressure gas storehouse 11 after fan blade 6 pressurizes, and the part gas in high pressure gas storehouse 11 is sprayed by the gas curtain spray orifice 13 of airship base plate 2, makes airship base plate 2 excircle form one circular curtain.Gas curtain forces the air accumulation sprayed through airship base plate 2 lift spray orifice 14 bottom airship, make to form partial high pressure bottom airship, like this, a maximum effective pressure is created poor between zone of negative pressure above the higher-pressure region of airship bottom and airship, and act on bottom whole airship, make bottom whole airship, to become the lifting area obtaining effective lift.Bottom area due to airship is equivalent to the area of conter of airship, makes airship obtain maximum effective lift area.Therefore, this airship only need consume less power just can obtain larger lift, and this airship can be floated flight in atmosphere.
Controlled the spray orifice switch size of corresponding site lift spray orifice 14 by flight control system, can realize controlling airship and be elevated arbitrarily stablizing of flight and flight attitude.
Control airship horizontal flight spray orifice 12 on one side by flight control system to open, airship will fly to reversing sense.Because airship is evenly distributed in horizontal flight spray orifice 12, therefore, airship flight is without the need to turning or turning around, and only need control corresponding rightabout horizontal flight spray orifice 12 and open and just can realize required any direction and fly, flight maneuver is flexible.
In high pressure gas storehouse 11, driving engine 5 times output shafts are provided with the major diameter flight stability gyro 3 controlling airship flight stability attitude, when driving engine 5 starts or raises speed, power passes to flight stability gyro 3 by change speed gear box, drives flight stability gyro 3 to rotate opposite sense high speed rotating to fan blade 6.When driving engine 5 slows down or shuts down, flight stability gyro 3 is automatically separated with change-speed box under effect of inertia.Flight stability gyro 3 continues high speed rotating with inertia energy, continues to keep airship to stablize, and guarantees airship flight stability safety.
Due to the structure design of airship, can obtain very large lift in the more low-energy situation of consumption, this airship can be made to float in atmosphere flight, and therefore, it is a very energy-conservation environment-friendly products.Meanwhile, because this airship profile is round and smooth, outside any position all can flip, dab, and under the effect of flight stability gyro, flight attitude is highly stable, and can realize at any time up, down, left, right, before and after, fast, slow, stop, comprehensive any flight.Therefore, it can it by space in fly arbitrarily, i.e. accessible flight.This is that the existing vehicle of the current mankind cannot be accomplished, therefore it will finally become the mankind's main vehicle from now on.
Claims (5)
1. adopt a gyro-stabilized jet airship, it is characterized in that, comprise annular carrying manipulation storehouse, driving engine, fan blade, flight stability gyro, flight control system,
The center in described annular carrying manipulation storehouse is provided with cylindricality air passage, annular carrying manipulation storehouse manipulates storehouse base plate with the carrying arranged thereunder and is connected, be dish-shaped high pressure gas storehouse between carrying manipulation storehouse base plate and airship base plate, air passage is connected with dish-shaped high pressure gas storehouse, driving engine is arranged in air passage, fan blade is positioned at air passage and is arranged on the upper output shaft of driving engine, flight stability gyro is arranged on the lower output shaft of driving engine, flight stability gyro is positioned at high pressure gas storehouse, the direction of rotation of flight stability gyro and fan blade during operation;
The cylindrical evenly densely covered gas curtain spray orifice of described airship base plate, airship base plate is provided with multiple lift spray orifice controlling to open, close, and airship cylindrical is evenly provided with the horizontal flight spray orifice that can control to open, close;
Described gas curtain spray orifice, lift spray orifice, horizontal flight spray orifice are connected with high pressure gas storehouse.
2. jet airship according to claim 1, is characterized in that, is provided with emergency power storehouse in the top in described carrying manipulation storehouse.
3. jet airship according to claim 2, is characterized in that, described emergency power storehouse internal memory emergency power parachute.
4. jet airship according to claim 2, is characterized in that, described emergency power storehouse is annular bin.
5. jet airship according to claim 1, is characterized in that, described airship base plate is provided with alighting gear.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410285200.6A CN104071331B (en) | 2014-06-24 | 2014-06-24 | The gyro-stabilized jet airship of a kind of employing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410285200.6A CN104071331B (en) | 2014-06-24 | 2014-06-24 | The gyro-stabilized jet airship of a kind of employing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104071331A CN104071331A (en) | 2014-10-01 |
| CN104071331B true CN104071331B (en) | 2016-04-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201410285200.6A Expired - Fee Related CN104071331B (en) | 2014-06-24 | 2014-06-24 | The gyro-stabilized jet airship of a kind of employing |
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Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818965A (en) * | 2016-05-03 | 2016-08-03 | 谭燕斌 | Power and stability system of jet-propelled airship stabilized by gyroscopes |
| CN106428559A (en) * | 2016-11-30 | 2017-02-22 | 吴锜 | Disc type aircraft |
| CN111348185A (en) * | 2018-12-20 | 2020-06-30 | 胡桂平 | Dish-shaped aircraft |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101428687A (en) * | 2008-12-12 | 2009-05-13 | 吉风旺 | General dynamic flying disk |
| CN102069908A (en) * | 2010-01-20 | 2011-05-25 | 李海波 | Saucer type aircraft |
| CN102582833A (en) * | 2012-02-27 | 2012-07-18 | 李海波 | Flying saucer in shape of tai chi |
| CN102616377A (en) * | 2012-04-05 | 2012-08-01 | 李海波 | Tai chi flying saucer |
| CN203937857U (en) * | 2014-06-24 | 2014-11-12 | 谭燕斌 | The gyro-stabilized jet airship of a kind of employing |
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2014
- 2014-06-24 CN CN201410285200.6A patent/CN104071331B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101428687A (en) * | 2008-12-12 | 2009-05-13 | 吉风旺 | General dynamic flying disk |
| CN102069908A (en) * | 2010-01-20 | 2011-05-25 | 李海波 | Saucer type aircraft |
| CN102582833A (en) * | 2012-02-27 | 2012-07-18 | 李海波 | Flying saucer in shape of tai chi |
| CN102616377A (en) * | 2012-04-05 | 2012-08-01 | 李海波 | Tai chi flying saucer |
| CN203937857U (en) * | 2014-06-24 | 2014-11-12 | 谭燕斌 | The gyro-stabilized jet airship of a kind of employing |
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| CN104071331A (en) | 2014-10-01 |
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Address after: Diecui road Yangshuo County Guilin 541900 the Guangxi Zhuang Autonomous Region No. 35 Applicant after: Tan Yanbin Address before: 541004 the Guangxi Zhuang Autonomous Region mountain Guilin Qixing District Road No. 11-82 Applicant before: Tan Yanbin |
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