CN102085910A - Airship and application thereof - Google Patents
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- CN102085910A CN102085910A CN2009102290027A CN200910229002A CN102085910A CN 102085910 A CN102085910 A CN 102085910A CN 2009102290027 A CN2009102290027 A CN 2009102290027A CN 200910229002 A CN200910229002 A CN 200910229002A CN 102085910 A CN102085910 A CN 102085910A
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Abstract
The invention discloses an airship and application thereof. The airship has good maneuverability, higher air sounding altitude and very long air residence time, and can provide an energy-saving and reliable aerial platform. The airship is provided with an 'air bag', wherein the air in the 'air bag' is taken out to a certain extent and then the air bag is set to have a vacuum or low atmospheric pressure relative to the outside air to a certain extent according to needs. The shape or volume of the 'air bag' of the airship is maintained or adjusted under the action of a supporter. The 'air bag' is inflated while the supporter is extending, a tubular network of an 'air bag' wall is inflated or the 'air bag' is plumped and hardened under the combined action of compounds, and then the air in the 'air bag' is taken out, so that the buoyant force makes the airship float in the air. The airship can be applied to solar electrical energy generation, wind power generation, radio communication or broadcasting, aircrafts or spacecrafts and satellite launching, and can be used as a platform or a tool and the like for performing high-altitude scientific experiments, breeding, remote metering and navigation, cloud layer making to rain, personnel or material transportation and air control.
Description
Affiliated technical field
The present invention relates to a kind of latent empty ship and application thereof.
Background technology
At present, all kinds of dirigibles all need fill gases such as hydrogen or helium, and its maneuvering performance is poor, and the sounding height is lower, and aerial length of the halt is limited.
Summary of the invention
All need fill gases such as hydrogen or helium in order to overcome present all kinds of dirigible, its maneuvering performance is poor, the sounding height is lower, problems such as aerial length of the halt is limited, the invention provides a kind of latent empty ship and application thereof, this empty ship maneuvering performance of diving is better, and the sounding height is higher, aerial length of the halt can be very long, and it can provide energy-conservation failure-free aerial platform.
The technical solution adopted in the present invention is: the key distinction of dive empty ship and present all kinds of dirigibles is, it has " air bag ", but be filled with gases such as a large amount of hydrogen or helium in its " air bag " unlike the air bag of present all kinds of dirigibles, the air in " air bag " of the empty ship of diving is taken away to a certain extent and is configured to a certain degree the vacuum or the infrabar of extraneous air relatively as required.The main effect of " air bag " of latent empty ship is to intercept extraneous air to enter " air bag " inside.The shape of " air bag " of latent empty ship or volume are kept under the effect of upholder or are regulated." air bag " of above-mentioned latent empty ship or the air bag that causes lift or buoyancy of other dirigibles or aircraft are made or are partly made by it by aerogel.The forms such as locations of structures of " air bag " upholder of empty ship of diving can be designed to can be as required and controlled." air bag " upholder of latent empty ship can adopt following technical scheme to realize: scheme one, to form by lightweight frame, and this framework both can adopt with " air bag " separable design also can adopt the design that combines together with " air bag "; Scheme two, by constituting of the cmpd that invests " air bag " wall or itself and lightweight frame, this cmpd can be arbitrarily can be under the effect of the chemical reaction of air or light, electricity, heat or other materials etc. can the hardening or the material that relative position is difficult to change between it that becomes; Scheme three, by constituting of the tubulose network that invests " air bag " wall or itself and lightweight frame, this tubulose network can fill gas or liquid; Scheme four is by constituting of such scheme.All kinds of technical scheme implementations of above-mentioned " air bag " upholder all be applicable to existing dirigible, balloon or other aircraft the air bag that causes lift or buoyancy design and belong to the claimed content of the present invention.Such as, the shape of " air bag " of empty ship or the maintenance or the adjusting of volume can so realize diving: in " air bag " of the empty ship of diving telescopic main support rod is arranged, with the main support rod vertical plane surface on have the secondary strut bars of many group ring-types to link to each other with main support rod, thereby it can drive the secondary strut bar of each ring-type and make " air bag " that the empty ship of diving is propped up in corresponding motion when main support rod stretches, in this process " air bag " thus also can constantly inflate fully and heave.When " air bag " when volume is suitable, main support rod stops to stretch, at this moment, can fill gas or liquid by the tubulose network that invests " air bag " wall, under the gas that the cmpd of its tubulose network duct wall transmits in its pipeline or the effect of liquid, or hardening under illumination or the galvanic action, in addition, gas or liquid itself full in the tubulose network pipeline also can play the support fixation effect to " air bag ".When " air bag " heaved and when macroscopic view hardens to appropriate level, then the air in " air bag " is taken away to a certain extent and made " air bag " be configured to a certain degree the vacuum or the infrabar of extraneous air relatively as required, so air lift force can float on the empty ship of diving in the air.Above-mentioned feature is applicable to the design of the air bag that causes lift or buoyancy of existing dirigible, balloon or other aircraft and upholder thereof and belongs to the claimed content of the present invention.The air bag of above-mentioned latent empty ship or all kinds of dirigibles or hull surface all can be installed solar cell or be coated solar electrical energy generation coating or load onto the utensil that other can utilize solar power.Above-mentioned latent empty ship combines with other kinds aircraft and all belongs to content of the present invention.Above-mentioned latent empty ship can combine with " novel flying disc type aircraft ", becomes the latent empty ship of the good high-mobility, multipurpose, wheeled vehicle of maneuvering performance.The gross area that " novel flying disc type aircraft " described herein is meant its rotor from the ratio of the length of the rotor center of turn corresponding ratio much larger than existing helicopter, makes it present the aircraft of the form that is similar to flying saucer on the whole with respect to rotor one end distance when far away the sight.Its rotor both can have been regarded the screw propeller of huge area as, also can regard the big huge screw of extremely lacking length of the big amplitude variation of area of screw thread as.Thereby its rotor can be positioned at the outside that fuselage is bordering on same horizontal surface in the horizontal direction around fuselage, and its each rotor degree of dip with respect to the horizontal plane can be adjusted rapidly at any time respectively as required, makes it obtain the flight optimization characteristic.Above-mentioned latent empty ship can be to make existing " air bag " and the upholder thereof that possesses the empty ship feature of diving of the latent empty ship of high-mobility, multipurpose, wheeled vehicle that the rotor that possesses " novel flying disc type aircraft " ship feature be arranged again with the mode of " novel flying disc type aircraft " combination.The present invention includes the following application of dive empty ship or the latent empty ship of high-mobility, multipurpose, wheeled vehicle: one, latent empty ship or the latent empty ship of high-mobility, multipurpose, wheeled vehicle are applied to solar electrical energy generation.Can receive on the mounted on surface of sunshine solar cell or coat solar electrical energy generation coating or load onto the utensil that other can utilize solar power in its any part.The parts of also extensible its surface or ad hoc reception solar power increase the sunshine receiver area.Two, latent empty ship or the latent empty ship of high-mobility, multipurpose, wheeled vehicle are applied to wind power generation, especially aerial wind-power electricity generation, this method is meant a plurality of resistance-type wind turbines is connected with cable etc., and make the one end system empty ship (also can have only a resistance-type wind turbine and make the one end system empty ship of diving) of diving, make it can float or fly in the air, and the other end can bolt on the ground or on the water surface object or on another empty ship of diving or not bolt on other objects, a plurality of latent empty ships also can be arranged between a plurality of resistance-type wind turbines, a plurality of resistance-type wind turbines also can be designs itself that take itself and the empty ship of diving to combine together, each resistance-type wind turbine can not all be set up electrical generator separately and can be concentrated to the somewhere to the rotational kinetic energy that is driven by wind again by generator for electricity generation through transmission, thereby alleviates its weight.The mode of transmission kinetic energy can be that each wind turbine is set up wheel flutter, and drives long-chain by wheel flutter, is transmitted kinetic energy step by step and is finally combined in place generating by long-chain.Three, latent empty ship or the high-mobility, multipurpose, wheeled vehicle empty ship of diving is combined with satellite or spacecraft and is applied to the space method for electric generation using solar energy, the space solar power that satellite or spacecraft handle are collected transfers on it.Four, latent empty ship or the latent empty ship of high-mobility, multipurpose, wheeled vehicle are applied to radio communication or broadcasting.Five, dive empty ship or the high-mobility, multipurpose, wheeled vehicle empty ship of diving is applied to the emission of aircraft or spacecraft, satellite.The present invention proposes and claimed aerial emission spacecraft or aerocraft method; promptly; the spacecraft of needs emission or aerocraft are placed (or inner) on the skyborne parent aircraft; realize to need continuing to circle round and quickening to make it before the parent aircraft is left in emission, obtain bigger speed of the spacecraft of emission or aerocraft by variety of way, just spacecraft or aerocraft are launched afterwards.Can be applied to above-mentioned aerial emission spacecraft or aerocraft method to latent empty ship or the high-mobility, multipurpose, wheeled vehicle empty ship of diving as the parent aircraft.Six, dive empty ship or the high-mobility, multipurpose, wheeled vehicle empty ship of diving is applied to as high-altitude scientific experiment, breeding, remote measurement, satellite observing and controlling, navigation, the manufacturing cloud layer platform with cooling, rainmaking, personnel or matter transportation, air control, amusement and travel.
The invention has the beneficial effects as follows that this empty ship maneuvering performance of diving is better, the sounding height is higher, and aerial length of the halt can be very long, and it can provide energy-conservation failure-free high-mobility, multipurpose, wheeled vehicle aerial platform.
Description of drawings
The present invention is further described below in conjunction with drawings and Examples.
Fig. 1 is a volume rendering scheme drawing in side of the present invention.
Among the figure " air bag " of 1. latent empty ships, 2. dive " air bag " upholder of empty ship, 3. the dive main support rod of " air bag " upholder of empty ship, 4. dive secondary strut bar of each ring-type of " air bag " upholder of empty ship, 5. invest the filled gas of " air bag " wall or the tubulose network of liquid (a part), 6. aircraft (or its aerofoil), the 7. cyclotron of emission spacecraft or aerocraft or other objects.
The specific embodiment
Among the embodiment shown in the figure, the empty ship of diving has " air bag " (1), and the air in its " air bag " (1) is taken away to a certain extent and is configured to a certain degree the vacuum or the infrabar of extraneous air relatively as required.The main effect of " air bag " (1) of latent empty ship is to intercept extraneous air to enter inside, " air bag " (1), shape of " air bag " (1) of latent empty ship or volume are kept under the effect of upholder (2) or are regulated, in addition, diving that the locations of structures form of " air bag " (1) upholder (2) of empty ship can be designed to can be as required and controlled." air bag " (1) of above-mentioned latent empty ship or the air bag that causes lift or buoyancy (1) of other dirigibles or aircraft are made or are partly made by it by aerogel." air bag " (1) upholder (2) of latent empty ship can adopt following technical scheme to realize: scheme one, be made up of lightweight frame (2), this framework both can adopt with the separable design in " air bag " (1) also can adopt the design that combines together with " air bag " (1); Scheme two, by constituting of the cmpd that invests " air bag " (1) wall or itself and lightweight frame (2), this cmpd can be arbitrarily can be under the effect of the chemical reaction of air or light, electricity, heat or other materials etc. can the hardening or the material that relative position is difficult to change between it that becomes; Scheme three is constituted by (2) of the tubulose network (5) that invests " air bag " (1) wall or itself and lightweight frame, and this tubulose network (5) can fill gas or liquid; Scheme four is by constituting of such scheme; All kinds of technical scheme implementations of above-mentioned " air bag " (1) upholder (2) all be applicable to existing dirigible, balloon or other aircraft the air bag that causes lift or buoyancy (1) design and belong to the claimed content of the present invention.In " air bag " (1) of latent empty ship telescopic main support rod (3) is arranged; with main support rod (3) vertical plane surface on have many group secondary strut bars of ring-type (4) to link to each other with main support rod (3); thereby it can drive the secondary strut bar (4) of each ring-type do " air bag " (1) that the empty ship of diving is propped up in corresponding motion when main support rod (3) stretches; (" air bag " upholder (2) of the empty ship of diving is if adopt other versions then also to belong to the content that the present invention is contained); " air bag " (1) in this process thus also can constantly inflate fully and heave; when " air bag " (1) when volume is suitable; main support rod (3) stops to stretch; at this moment; can fill gas or liquid by the tubulose network (5) that invests " air bag " (1) wall; under the gas that the cmpd of its tubulose network (5) duct wall transmits in its pipeline or the effect of liquid; or hardening or the relative position that becomes between it are difficult to change under illumination or the galvanic action; in addition; gas or liquid itself full in tubulose network (5) pipeline also can play the support fixation effect to " air bag " (1); when heave and when macroscopic view hardens to appropriate level " air bag " (1); then the air in " air bag " (1) is taken away to a certain extent and made " air bag " (1) be configured to a certain degree the vacuum or the infrabar of extraneous air relatively as required; so; air lift force can float in the air the empty ship of diving, and above-mentioned feature is applicable to existing dirigible; the air bag that causes lift or buoyancy (1) of balloon or other aircraft and the design of upholder (2) thereof also belong to the claimed content of the present invention.Above-mentioned latent empty ship combines with other kinds aircraft (6), becomes the latent empty ship of the good high-mobility, multipurpose, wheeled vehicle of maneuvering performance.The present invention comprises following all application arbitrarily of dive empty ship or the latent empty ship of high-mobility, multipurpose, wheeled vehicle: one, it is applied to solar electrical energy generation, solar cell or coat solar electrical energy generation coating or load onto the utensil that other can utilize solar power on its any part or all of mounted on surface that can receive sunshine, parts of also extensible its surface or ad hoc reception solar power increase sunshine receiver area; Two, it is applied to wind-power electricity generation, especially " aerial wind-power electricity generation ", this method is meant a plurality of resistance-type wind turbines is connected with cable etc., and make the one end system empty ship (also can have only a resistance-type wind turbine and make the one end system empty ship of diving) of diving, make it can float or fly in the air, and the other end can bolt on the ground or on the water surface object or on another empty ship of diving or not bolt on other objects, a plurality of latent empty ships also can be arranged between a plurality of resistance-type wind turbines, a plurality of resistance-type wind turbines also can be designs itself that take itself and the empty ship of diving to combine together, each resistance-type wind turbine can not all be set up electrical generator separately and can be concentrated to the somewhere to the rotational kinetic energy that is driven by wind again by generator for electricity generation through transmission, thereby alleviate its weight, the mode of transmission kinetic energy can be that each wind turbine is set up wheel flutter, and, transmit kinetic energy step by step and finally combine in place generating by long-chain by wheel flutter drive long-chain; Three, it is combined with satellite or spacecraft be applied to the space method for electric generation using solar energy, satellite or spacecraft transfer to the space solar power of collecting on it; Four, it is applied to radio communication or broadcasting; Five, it is applied to the emission of aircraft or spacecraft, satellite; Six, it is applied to as high-altitude scientific experiment, breeding, remote measurement, satellite observing and controlling, navigation, manufacturing cloud layer platform or the instrument with cooling, rainmaking, personnel or matter transportation, air control, amusement and travel.The present invention proposes and claimed aerial emission spacecraft or aerocraft method; promptly; the spacecraft of needs emission or aerocraft are placed (or inner) on the skyborne parent aircraft; can realize need continuing to circle round and quickening to make it before the parent aircraft is left in emission, obtain bigger speed of the spacecraft of emission or aerocraft by cyclotron (7); just spacecraft or aerocraft are launched afterwards, can be applied to above-mentioned aerial emission spacecraft or aerocraft method to latent empty ship or the high-mobility, multipurpose, wheeled vehicle empty ship of diving as the parent aircraft.The empty ship of diving can combine with " novel flying disc type aircraft " (6), become the latent empty ship of the good high-mobility, multipurpose, wheeled vehicle of a kind of maneuvering performance, the gross area that " novel flying disc type aircraft " (6) described herein are meant its rotor with respect to rotor one end distance from the ratio of the length of rotor center of turn corresponding ratio much larger than existing helicopter, make it when far away the sight, present the aircraft of the form that is similar to flying saucer on the whole, its rotor both can have been regarded the screw propeller of huge area as, the big huge screw of extremely lacking length of the big amplitude variation of area that also can regard screw thread as, its each rotor degree of dip with respect to the horizontal plane can be adjusted rapidly at any time respectively as required, make it obtain the flight optimization characteristic, above-mentioned latent empty ship can be to make existing " air bag " (1) and the upholder (2) thereof that possesses the empty ship feature of diving of the latent empty ship of high-mobility, multipurpose, wheeled vehicle that the rotor that possesses " novel flying disc type aircraft " (6) ship feature be arranged again with the mode of " novel flying disc type aircraft " (6) combination.
Claims (9)
1. dive empty ship and application thereof, it is characterized in that: it has " air bag ", and the air in its " air bag " is taken away to a certain extent and is configured to a certain degree the vacuum or the infrabar of extraneous air relatively as required.
2. latent empty ship according to claim 1 and application thereof, it is characterized in that: the main effect of " air bag " of the empty ship of diving is to intercept extraneous air to enter " air bag " inside, the shape of " air bag " of latent empty ship or volume are kept under the effect of upholder or are regulated, in addition, diving that the locations of structures form of " air bag " upholder of empty ship can be designed to can be as required and controlled.
3. latent empty ship according to claim 1 and application thereof is characterized in that: " air bag " of above-mentioned latent empty ship or the air bag that causes lift or buoyancy of other dirigibles or aircraft are made or are partly made by it by aerogel.
4. latent empty ship according to claim 1 and application thereof, it is characterized in that: " air bag " upholder of the empty ship of diving can adopt following technical scheme to realize: scheme one, be made up of lightweight frame, this framework both can adopt with " air bag " separable design also can adopt the design that combines together with " air bag "; Scheme two, by constituting of the cmpd that invests " air bag " wall or itself and lightweight frame, this cmpd can be arbitrarily can be under the effect of the chemical reaction of air or light, electricity, heat or other materials etc. can the hardening or the material that relative position is difficult to change between it that becomes; Scheme three, by constituting of the tubulose network that invests " air bag " wall or itself and lightweight frame, this tubulose network can fill gas or liquid; Scheme four is by constituting of such scheme; All kinds of technical scheme implementations of above-mentioned " air bag " upholder all be applicable to existing dirigible, balloon or other aircraft the air bag that causes lift or buoyancy design and belong to the claimed content of the present invention.
5. latent empty ship according to claim 1 and application thereof; it is characterized in that: in " air bag " of the empty ship of diving telescopic main support rod is arranged; with the main support rod vertical plane surface on have the secondary strut bars of many group ring-types to link to each other with main support rod; thereby it can drive the secondary strut bar of each ring-type and make " air bag " that the empty ship of diving is propped up in corresponding motion when main support rod stretches; (" air bag " upholder of the empty ship of diving is if adopt other versions then also to belong to the content that the present invention is contained); in this process " air bag " thus also can constantly inflate fully and heave; when " air bag " when volume is suitable; main support rod stops to stretch; at this moment; can fill gas or liquid by the tubulose network that invests " air bag " wall; under the gas that the cmpd of its tubulose network duct wall transmits in its pipeline or the effect of liquid; or under illumination or the galvanic action or down hardening or become that relative position is difficult to change between it (herein if there is not this compounds also to belong to the content that the present invention is contained) of other effects; in addition; gas or liquid itself full in the tubulose network pipeline also can play the support fixation effect to " air bag "; when " air bag " heaved and when macroscopic view hardens to appropriate level; then the air in " air bag " is taken away to a certain extent and made " air bag " be configured to a certain degree the vacuum or the infrabar of extraneous air relatively as required; so; air lift force can float in the air the empty ship of diving, and above-mentioned feature is applicable to existing dirigible; the air bag that causes lift or buoyancy of balloon or other aircraft and the design of upholder thereof also belong to the claimed content of the present invention.
6. latent empty ship according to claim 1 and application thereof is characterized in that: above-mentioned latent empty ship combines with other kinds aircraft, becomes the latent empty ship of the good high-mobility, multipurpose, wheeled vehicle of maneuvering performance.
7. latent empty ship according to claim 1 and application thereof, it is characterized in that: the present invention comprises following all application arbitrarily of dive empty ship or the latent empty ship of high-mobility, multipurpose, wheeled vehicle: one, it is applied to solar electrical energy generation, solar cell or coat solar electrical energy generation coating or load onto the utensil that other can utilize solar power on its any part or all of mounted on surface that can receive sunshine, parts of also extensible its surface or ad hoc reception solar power increase sunshine receiver area; Two, it is applied to wind-power electricity generation, especially " aerial wind-power electricity generation ", this method is meant a plurality of resistance-type wind turbines is connected with cable etc., and make the one end system empty ship (also can have only a resistance-type wind turbine and make the one end system empty ship of diving) of diving, make it can float or fly in the air, and the other end can bolt on the ground or on the water surface object or on another empty ship of diving or not bolt on other objects, a plurality of latent empty ships also can be arranged between a plurality of resistance-type wind turbines, a plurality of resistance-type wind turbines also can be designs itself that take itself and the empty ship of diving to combine together, each resistance-type wind turbine can not all be set up electrical generator separately and can be concentrated to the somewhere to the rotational kinetic energy that is driven by wind again by generator for electricity generation through transmission, thereby alleviate its weight, the mode of transmission kinetic energy can be that each wind turbine is set up wheel flutter, and, transmit kinetic energy step by step and finally combine in place generating by long-chain by wheel flutter drive long-chain; Three, it is combined with satellite or spacecraft be applied to the space method for electric generation using solar energy, satellite or spacecraft transfer to the space solar power of collecting on it; Four, it is applied to radio communication or broadcasting; Five, it is applied to the emission of aircraft or spacecraft, satellite; Six, it is applied to as high-altitude scientific experiment, breeding, remote measurement, satellite observing and controlling, navigation, manufacturing cloud layer platform or the instrument with cooling, rainmaking, personnel or matter transportation, air control, amusement and travel.
8. latent empty ship according to claim 1 and application thereof; it is characterized in that: the present invention proposes and claimed aerial emission spacecraft or aerocraft method; promptly; the spacecraft of needs emission or aerocraft are placed (or inner) on the skyborne parent aircraft; realize to need continuing to circle round and quickening to make it before the parent aircraft is left in emission, obtain bigger speed of the spacecraft of emission or aerocraft by variety of way; just spacecraft or aerocraft are launched afterwards, can be applied to above-mentioned aerial emission spacecraft or aerocraft method to latent empty ship or the high-mobility, multipurpose, wheeled vehicle empty ship of diving as the parent aircraft.
9. latent empty ship according to claim 1 and application thereof, it is characterized in that: the empty ship of diving can combine with " novel flying disc type aircraft ", become the latent empty ship of the good high-mobility, multipurpose, wheeled vehicle of a kind of maneuvering performance, the gross area that " novel flying disc type aircraft " described herein is meant its rotor with respect to rotor one end distance from the ratio of the length of rotor center of turn corresponding ratio much larger than existing helicopter, make it when far away the sight, present the aircraft of the form that is similar to flying saucer on the whole, its rotor both can have been regarded the screw propeller of huge area as, the big huge screw of extremely lacking length of the big amplitude variation of area that also can regard screw thread as, its each rotor degree of dip with respect to the horizontal plane can be adjusted rapidly at any time respectively as required, make it obtain the flight optimization characteristic, above-mentioned latent empty ship can be to make existing " air bag " and the upholder thereof that possesses the empty ship feature of diving of the latent empty ship of high-mobility, multipurpose, wheeled vehicle that the rotor that possesses " novel flying disc type aircraft " ship feature be arranged again with the mode of " novel flying disc type aircraft " combination.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009102290027A CN102085910A (en) | 2009-12-07 | 2009-12-07 | Airship and application thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009102290027A CN102085910A (en) | 2009-12-07 | 2009-12-07 | Airship and application thereof |
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| Publication Number | Publication Date |
|---|---|
| CN102085910A true CN102085910A (en) | 2011-06-08 |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102923294A (en) * | 2011-08-12 | 2013-02-13 | 林海山 | Balloon lifter |
| CN102935887A (en) * | 2012-12-07 | 2013-02-20 | 徐大来 | Ground-to-air stratosphere aerospace vehicle and flying platform |
| CN104627349A (en) * | 2015-03-04 | 2015-05-20 | 刘君才 | Volume variable air boat |
| CN104993774A (en) * | 2015-07-23 | 2015-10-21 | 北京天航华创科技股份有限公司 | Light energy-wind energy integrated power generation system for stratospheric airship |
| CN104590533B (en) * | 2014-12-24 | 2016-06-08 | 中国特种飞行器研究所 | One can variant dirigible |
| CN106143866A (en) * | 2015-04-27 | 2016-11-23 | 黄福祯 | A kind of multi-functional geostationary satellite based on solar energy dirigible |
| CN106428555A (en) * | 2016-10-31 | 2017-02-22 | 成立 | Unpowered vacuum-energy flying saucer type spacecraft |
| WO2018219059A1 (en) * | 2017-06-02 | 2018-12-06 | 海口未来技术研究院 | Aerostat |
| CN111776195A (en) * | 2020-07-17 | 2020-10-16 | 河北柒壹壹玖工业自动化技术有限公司 | Solar unmanned aerial vehicle capable of replacing satellite communication |
-
2009
- 2009-12-07 CN CN2009102290027A patent/CN102085910A/en active Pending
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102923294A (en) * | 2011-08-12 | 2013-02-13 | 林海山 | Balloon lifter |
| CN102935887A (en) * | 2012-12-07 | 2013-02-20 | 徐大来 | Ground-to-air stratosphere aerospace vehicle and flying platform |
| CN104590533B (en) * | 2014-12-24 | 2016-06-08 | 中国特种飞行器研究所 | One can variant dirigible |
| CN104627349A (en) * | 2015-03-04 | 2015-05-20 | 刘君才 | Volume variable air boat |
| CN106143866A (en) * | 2015-04-27 | 2016-11-23 | 黄福祯 | A kind of multi-functional geostationary satellite based on solar energy dirigible |
| CN104993774A (en) * | 2015-07-23 | 2015-10-21 | 北京天航华创科技股份有限公司 | Light energy-wind energy integrated power generation system for stratospheric airship |
| CN106428555A (en) * | 2016-10-31 | 2017-02-22 | 成立 | Unpowered vacuum-energy flying saucer type spacecraft |
| WO2018219059A1 (en) * | 2017-06-02 | 2018-12-06 | 海口未来技术研究院 | Aerostat |
| CN111776195A (en) * | 2020-07-17 | 2020-10-16 | 河北柒壹壹玖工业自动化技术有限公司 | Solar unmanned aerial vehicle capable of replacing satellite communication |
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Application publication date: 20110608 |