CN201169384Y - Novel hovering airship - Google Patents
Novel hovering airship Download PDFInfo
- Publication number
- CN201169384Y CN201169384Y CNU2008200524914U CN200820052491U CN201169384Y CN 201169384 Y CN201169384 Y CN 201169384Y CN U2008200524914 U CNU2008200524914 U CN U2008200524914U CN 200820052491 U CN200820052491 U CN 200820052491U CN 201169384 Y CN201169384 Y CN 201169384Y
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- CN
- China
- Prior art keywords
- plenum chamber
- outer plenum
- type novel
- floating type
- novel airship
- 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.)
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Abstract
A hovering type novel airship relates to an inflatable flying vehicle which comprises an outer plenum chamber which has an oval-shaped shape, and also comprises an inner plenum chamber which has the same shape with the outer plenum chamber and is arranged in the outer plenum chamber, the center axes of the inner plenum chamber is in the same line with that of the outer plenum chamber; a high-pressure inflation circular tube is integrally arranged along the center line of the long shafts of the oval-shaped outer plenum chamber and the inner plenum chamber, the two ends, that is, the front and tail ends of the high-pressure inflation circular tube are respectively provided with an electrically driven fan; the outer plenum chamber, the inner plenum chamber and the high-pressure inflation circular tube all are sealed air bags; the shell of the flying vehicle, that is, the outer wall of the outer plenum chamber, is provided with an air inflation-suction double-purpose air compressor and is communicated with the inner plenum chamber in an sealing way; the shell of the flying vehicle, that is the outer wall of the outer plenum chamber, is provided with a drive center control chamber used for people to travel on and for arranging a control component; the inner plenum chamber is inflated with air and the outer plenum chamber and the high pressure inflation circular tube are inflated with helium gas. The hover type novel airship can fly, hover, advance and retreat as convenient as desired.
Description
Technical field
The utility model relates to a kind of inflatable aircraft.
Background technology
Fish are hovered in water freely, all because of the random air bladder of breathing is arranged in the empty stomach, and bionical thus research, the mankind have invented submarine, and can people aloft also realize hovering lifting freely so, and answer is sure.
The human at present aircraft of place in operation that takes place also, carrying out hovers all needs to consume big energy, and not flexible freely.
The utility model content
The utility model is intended to the above-mentioned deficiency at prior art, designs a kind of novel airship, and imitative air bladder design can be hovered, turns to, be advanced and retreat, and fly freely, and power consumption is extremely low.Be convenient to operation.
To achieve these goals, a kind of novel airship technical scheme of the utility model is:
The utility model comprises that profile is the outer plenum chamber of elliposoidal, also comprises the plenum chamber that is positioned among the outer plenum chamber, and the shape of interior plenum chamber is consistent with outer plenum chamber shape, the central axis of interior plenum chamber and the central axes of outer plenum chamber; The major axis line of centers of plenum chamber is integrated a high-pressure aerated pipe is installed in the outer plenum chamber of elliposoidal reaches, and the promptly preceding tail end in the two ends of described high-pressure aerated pipe is installed the electric fan that drives respectively; Outer plenum chamber, interior plenum chamber, high-pressure aerated pipe are all the leak free air bag; The outer wall of plenum chamber is installed and is filled the dual-purpose air compressor of bleeding outside the shell of dirigible is, the described valve that fills the dual-purpose air compressor of bleeding is communicated with interior plenum chamber sealing; Be provided with at the outer wall of the promptly outer plenum chamber of the shell of dirigible that the confession personnel take and the driving Central Control Room of installation and control member.
Plenum chamber fills with air in described.
Described outer plenum chamber and high-pressure aerated pipe fill with helium.
The valve of helium charging blower can be communicated with outer plenum chamber and the sealing of high-pressure aerated pipe.
Shell filling direction at the tail end of dirigible is adjusted cotton rope and motor.
At the front end and the tail end difference storage battery of dirigible, drive the electric fan that drives of fan and back for preceding electricity and use.
Fill the dual-purpose air compressor of bleeding, helium charging blower, direction adjust cotton rope and motor, preceding electricity drive fan and back electricity drive fan all with drive Central Control Room in control member be connected and control, chaufeur needs only operates the control corresponding part.
Before this dirigible begins to take off, dirigible is fastened admittedly with rope, air compressor cuts out.Start the helium charging blower the outer plenum chamber of dirigible is full of helium, because interior plenum chamber does not have pressure, be squeezed into the flat capsule that contracts by outer plenum chamber, start shipment air compressor interior plenum chamber be full of, simultaneously since interior plenum chamber pressure greater than outer plenum chamber, along with Peng of energy chamber is expanded, the space of outer plenum chamber is extruded a part, even this moment, dirigible was untied the bolt rope, the buoyancy that produces because of dirigible can not go up to the air less than chaufeur body weight and the dirigible sum of conducting oneself with dignity.
When taking off, chaufeur fills the dual-purpose air compressor counter-rotating of bleeding at operator's compartment with startup, and interior plenum chamber air is slowly extracted out, and along with the slowly flat of energy chamber contracts, dirigible is just slowly vertical to rise.
Owing to the variation along with height of the density of air changes, so certain height, the suffered buoyancy of dirigible also is certain, stops air-out like this as after the lift-off, just dirigible hovers in certain height, neither rise and also do not descend, electricity driving fan and back electricity drive and fan before starting this moment, and dirigible is just in the flight forward fast of a certain height, because in light weight, friction is little, and flying speed will substantially exceed the speed of magnetic suspension train.
The airduct of dirigible afterbody can change under the stay cord effect of four direction freely faces upward the deflecting direction of bowing, but preceding electricity drives fan and the back electricity drives also contrarotation of fan, and dirigible just can realize turning to advance and retreat freely.
Start during decline and fill the dual-purpose air compressor of bleeding, interior plenum chamber is bulging once more, and dirigible just safety descends lentamente.
Major advantage of the present utility model is:
1, flight, hover, free to advance or retreat;
2, energy consumption low (zero-lift energy consumption during flight);
3, safety, unreactable gas helium does not fire not quick-friedly, and the dirigible shell is made with the polyurethane high molecule material, and adopts many air chambers to piece together system, is not afraid of bob, is not afraid of and hits; As being used for military affairs, shell also can adopt the shellproof material of setting fire, and can realize " armsproof ";
4, applied range can be widely used in trip, tourism, advertisement, takes photo by plane, frontier defense patrol and military surveillance and strike.
Description of drawings
Fig. 1 is the utility model structural representation;
Fig. 2 is the utility model tail structure scheme drawing.
Among the figure: 1, outer plenum chamber, 2, interior plenum chamber, 3, high-pressure aerated pipe, 4, fill the dual-purpose air compressor of bleeding, 5, preceding electricity drives fan, and 6, the back electricity drives fan, 7, drive Central Control Room, 8, direction adjusts cotton rope, 9, storage battery, 10 equal power drag-line ropes, 11, video heads.
The specific embodiment
Below, introduce the specific embodiment of the present utility model in conjunction with the accompanying drawings.
As shown in the figure, the utility model comprises that profile is the outer plenum chamber 1 of elliposoidal, also comprise the plenum chamber 2 that is positioned among the outer plenum chamber 1, the shape of interior plenum chamber 2 is consistent with outer plenum chamber 1 shape, the central axes of the central axis of interior plenum chamber 2 and outer plenum chamber 1; The major axis line of centers of plenum chamber 2 is integrated a high-pressure aerated pipe 3 is installed in the outer plenum chamber 1 of elliposoidal reaches, and the promptly preceding tail end in the two ends of described high-pressure aerated pipe 3 is installed the electric fan 5,6 that drives respectively; Outer plenum chamber 1, interior plenum chamber 2, high-pressure aerated pipe 3 are all the leak free air bag; The outer wall of plenum chamber 1 is installed and is filled the dual-purpose air compressor 4 of bleeding outside the shell of dirigible is, the described valve that fills the dual-purpose air compressor 4 of bleeding is communicated with interior plenum chamber 2 sealings; Be provided with at the outer wall of the promptly outer plenum chamber 1 of the shell of dirigible that the confession personnel take and the driving Central Control Room 7 of installation and control member.
Plenum chamber 2 fills with air in described.
Described outer plenum chamber 1 and high-pressure aerated pipe 3 fill with helium.
The valve of helium charging blower can be communicated with outer plenum chamber 1 and 3 sealings of high-pressure aerated pipe.
The tail end installation direction of plenum chamber 1 outer wall is adjusted cotton rope 8 and motor outside the shell of dirigible tail end is.
Front end and tail end at high-pressure aerated pipe 3 are installed storage battery 9 respectively, drive the electric fan 6 that drives of fan 5 and back for preceding electricity and use.
Fill the dual-purpose air compressor 4 of bleeding, helium charging blower, direction adjust cotton rope 8 and motor, preceding electricity drive fan 5 and back electricity drive fan 6 all with drive Central Control Room 7 in control member be connected and control, chaufeur needs only operates the control corresponding part.
Described driving Central Control Room 7 is for filling the air bag with helium, and this air bag is communicated with the valve sealing of helium charging blower, and transparency window is set on it.
Driving 3 equal power drag-line ropes 10 of installation of Central Control Room 7 and high-pressure aerated pipe, be convenient to drive Central Control Room 7 location.
The front end of plenum chamber 1 outer wall also is provided with video heads 11 outside the front end of dirigible is.
Claims (9)
1, floating type novel airship, comprise that profile is the outer plenum chamber (1) of elliposoidal, it is characterized in that: also comprise the plenum chamber (2) that is positioned among the outer plenum chamber (1), the shape of interior plenum chamber (2) is consistent with outer plenum chamber (1) shape, the central axes of the central axis of interior plenum chamber 2 and outer plenum chamber (1); The major axis line of centers of plenum chamber (2) is integrated a high-pressure aerated pipe (3) is installed in the outer plenum chamber (1) of elliposoidal reaches, and the promptly preceding tail end in the two ends of described high-pressure aerated pipe (3) is installed electric fan (5), (6) of driving respectively; Outer plenum chamber (1), interior plenum chamber (2), high-pressure aerated pipe (3) are all the leak free air bag; The outer wall of plenum chamber (1) is installed and is filled the dual-purpose air compressor (4) of bleeding outside the shell of dirigible is, the described valve that fills the dual-purpose air compressor (4) of bleeding is communicated with interior plenum chamber (2) sealing; Be provided with at the outer wall of the promptly outer plenum chamber (1) of the shell of dirigible that the confession personnel take and the driving Central Control Room (7) of installation and control member.
2, the floating type novel airship of narrating according to claim 1 is characterized in that: plenum chamber (2) fills with air in described.
3, the floating type novel airship of narrating according to claim 1 is characterized in that: described outer plenum chamber 1 and high-pressure aerated pipe (3) fill with helium.
4, the floating type novel airship of narrating according to claim 1 is characterized in that: the valve of helium charging blower can be communicated with outer plenum chamber (1) and high-pressure aerated pipe (3) sealing.
5, the floating type novel airship of narrating according to claim 1 is characterized in that: the tail end installation direction of outer plenum chamber (1) outer wall is adjusted cotton rope (8) and motor.
6, the floating type novel airship of narrating according to claim 1 is characterized in that: front end and tail end at high-pressure aerated pipe (3) are installed storage battery (9) respectively.
7, the floating type novel airship of narrating according to claim 1 is characterized in that: described driving Central Control Room (7) is for filling the air bag with helium, and this air bag can be communicated with the valve sealing of helium charging blower, and transparency window also is set on it.
8, the floating type novel airship of narrating according to claim 1 is characterized in that: driving installation equal power drag-line rope (10) between Central Control Room (7) and high-pressure aerated pipe (3).
9, the floating type novel airship of narrating according to claim 1 is characterized in that: the front end of described outer plenum chamber (1) outer wall also is provided with video heads (11).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008200524914U CN201169384Y (en) | 2008-03-09 | 2008-03-09 | Novel hovering airship |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008200524914U CN201169384Y (en) | 2008-03-09 | 2008-03-09 | Novel hovering airship |
Publications (1)
Publication Number | Publication Date |
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CN201169384Y true CN201169384Y (en) | 2008-12-24 |
Family
ID=40208437
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CNU2008200524914U Expired - Fee Related CN201169384Y (en) | 2008-03-09 | 2008-03-09 | Novel hovering airship |
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CN (1) | CN201169384Y (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111340804A (en) * | 2020-04-09 | 2020-06-26 | 山东大学 | Unmanned airship-based air quality machine vision online monitoring system and method |
CN114313203A (en) * | 2022-01-27 | 2022-04-12 | 中国航发沈阳发动机研究所 | Unmanned floating airship |
-
2008
- 2008-03-09 CN CNU2008200524914U patent/CN201169384Y/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111340804A (en) * | 2020-04-09 | 2020-06-26 | 山东大学 | Unmanned airship-based air quality machine vision online monitoring system and method |
CN114313203A (en) * | 2022-01-27 | 2022-04-12 | 中国航发沈阳发动机研究所 | Unmanned floating airship |
CN114313203B (en) * | 2022-01-27 | 2024-05-24 | 中国航发沈阳发动机研究所 | Unmanned floating airship |
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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: 20081224 Termination date: 20120309 |