CN1521084B - Composite airship - Google Patents
Composite airship Download PDFInfo
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- CN1521084B CN1521084B CN03103948.0A CN03139480A CN1521084B CN 1521084 B CN1521084 B CN 1521084B CN 03139480 A CN03139480 A CN 03139480A CN 1521084 B CN1521084 B CN 1521084B
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- dirigible
- lifting
- airship
- composite
- balloon outer
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Abstract
The composite airship is one composite flyer as one air transport facility. The present invention is developed on the basis of elevating airship patent of the present inventor and provides the elevating airship with wide application range and practical application. The present invention may be used widely in air transportation, amusement, construction and advertisement, and the composite airship may be in cylindrical, disc shape, streamline, spherical or other shape. The present invention is especially suitable for civil use.
Description
One, Composite airship claims again composite aircraft, it belongs to the another significant innovation product of aviation field transport facility, is that the inventor reforms the follow-up achievement developing after improvement on former < < lifting airship > > patented technology basis.For < < lifting airship > > patent provides more wide Applicable scope, product performance and the practical basis of lifting airship patent have been improved, it is extensively practically applicable to all trades and professions and individual's the activities such as air transport, amusement, construction, and that its profile is divided into is cylindrical, dish-shaped, streamline contour, spherical and special-shaped etc.
Two, present situation
1, conventional aircraft, when bringing many benefits to people, has following weakness:
(1) aircraft: involve great expense, the energy needing is many, and weight is large, complicated operation, during production to material require highly, complex manufacturing, needs airport and runway when taking off and landing.
(2) helicopter: need engine to produce huge lifting force during lifting, need the running of screw propeller Large-power High-Speed as guaranteeing.
(3) fire balloon: bulky, load carrying ability is little, and energy consumption is high, aerial length of the halt is short, and translatory velocity is minimum, is subject to windage large, and Applicable scope is quite narrow.
(4) traditional dirigible: lifting, the operation of advancing, turning to are controlled complicated, and smoothness is low, and translatory velocity is minimum, energy recharge difficulty.
(5) lifting airship: hang indigo plant and be subject to air resistance large, move flat speed still little, that people's goods etc. are subject in hanging basket is hot and cold, expose to wind and rain, solar radiation etc. affect large, and energy recharge is difficulty still.
2, reference books
The disclosed < < of 13 State Intellectual Property Office in November, (1) 2002 lifting airship > > application for a patent for invention specification sheets and patent model.
(2) < < aviation knowledge > > magazine and < < fluid mechanics > > book series in recent years.
The new life of (3) 1999 years 12 phase < < aviation knowledge > > magazine 35-42 page < < dirigibles---history, current situation and development > > mono-literary composition of the research of countries in the world dirigible.
Within (4) 2003 years, < < war industry science and technology > > magazine 17-26 page < < aeronautics expert talks freely about---evolution > > mono-literary composition of century-old aircraft manufacturing technology.
Three, goal of the invention
Various aircraft (dirigible, lifting airship, fire balloon, aircraft, helicopter etc.) advantage is separately extracted to combine and form aircraft of new generation---Composite airship.Make it have flexible fast lifting and the horizontal flight characteristic of high speed of helicopter, manufactured materials, the structure with dirigible, there is the load carrying ability of aircraft and the characteristic of running at high speed, allow portioned product have more the long timeliness function of all-weather flight, make it to become cheap " omnipotent aircraft ".
Four, solution
(1) take lifting airship technology as basis: 1, applied compression system changes the buoyancy size that volume that air bag arranges air changes dirigible, the object that reaches this aircraft of lifting (is about to the process that dirigible becomes lifting airship, refer to lifting airship application open file, its patent No.: 01111096.1).
2, by promoting passenger plane, put down at a high speed the front end (or rear end or rear and front end) that is contained in the fairing profile air bag of lifting airship to the screw propeller of motion, putting down to flying speed of raising lifting airship, makes it have part propulsion system structure and the function of aircraft.
3, in the air bag of lifting airship, open up one " vacant lot ", for manned loading and dress control system, what save traditional dirigible hangs the things such as indigo plant, lifting rope; Reduce air to the resistance of this dirigible and weather to hang basket in the infringement of people, machine thing, make it have the partial interior filling structure of aircraft and helicopter.
4 or applied solar energy battery membranes (as crystal silicon solar cell) to be covered in the outer air bag of lifting airship outer, collect aerial solar power as this kind of lifting airship, i.e. the energy of composite aircraft work.
(2) increase the method for load carrying ability: 1, borrow fire balloon principle.1. apply transparent membrane and make the air bag of this dirigible, allow light gas in solar energy heat air external capsule, in capsule, use material or the device that absorbs luminous energy, as black paper, cloth etc.2. apply electro-heat equipment (as the thermal chemical reaction of heating wire or combustible or heat release heat absorption etc.), the light gas in heating or cooling air bag.
2, improve and put down to flying speed, monnolithic case, the lifting force of change dirigible.
3, the auxiliary lifting force that produces of application power system.
Five, advantage
1,, aloft under static state or dynamic condition, steadily vertical lift, is equivalent to helicopter.Increased safety factor, airfield runway run-up is not taken off and slides deceleration; And speed of response is fast, easy and simple to handle.
2, streamline contour ectosome, can constant-bearing navigation.The level with passenger plane at a high speed and be subject to air resistance little, speed can reach per hour tens kilometers to hundreds of kilometer, be equivalent to automobile, be applicable to civilian.
3, light gas recycles for a long time, saves the energy and fee of material, and this composite aircraft is simple in structure, with low cost, easy to operate, convenient and practical.The lifting force of Composite airship is provided by light gas, and in the situation that load carrying ability is identical, its volume is large compared with helicopter, while accelerating flight, is subject to air resistance larger, therefore it is put down to flying speed not as good as aircraft and helicopter, speed is moderate, is particularly suitable for civilian, family expenses.
4, combine the advantage of dirigible and fire balloon, use the material of part fire balloon and dirigible, produce material and be easy to get, and easily manufacture, cheap practical.Under equal conditions, this aircraft has dwindled air bag volume, has increased load carrying ability.
5, applied solar energy, as the Composite airship of the work energy, has reduced consumption, has increased the skyborne flight length of the halt of this dirigible, for all-weather flight provides energy safeguard.
6, the same aircraft of Composite airship, helicopter are compared: due to the lift (claim again lifting force, lifting force equals buoyancy loss of weight power) of this dirigible, the buoyancy producing in air by light gas provides, low to the power requirement of power system, conduct oneself with dignity minimum, and energy consumption is also few.The lifting force of aircraft provides by power system, and passenger plane is by flying speed and the runway help-fly of improving the standard, by the rotation generation lifting force of fairing external form (being fluid continuity principle and Bernoulli theorem) and screw propeller; Helicopter is by changing the high speed rotating of engine screw propeller, produce the lifting force differing in size, realizing lifting.So their power system: weight is large, power requirement is high; While producing passenger plane and helicopter, material requirements is harsh.
Six, accompanying drawing explanation
Fig. 1, be Composite airship dimension sketch, wherein: (1) is screw propeller, during for constant-bearing navigation left/right rotation, controlling party to and flying speed.(2) be the outer air bag of composite bed.(3) be tail fin: for supporting dirigible and auxiliary directional navigation.(4) be capsula interna.(5) be load-carrying chamber door, of bag material or woven dacron, make, of slide fastener or hasp folding.(6) for dirigible is stopped the strong point.
Fig. 2, be Composite airship cross-section structure simplified schematic diagram, wherein: (7) are outer air bag composite and air chamber thereof, requiring between double-walled can relative motion, and the object of using composite to add air chamber is to reduce the aerial friction drag of dirigible and pressure drag; If the quantity of interval air chamber between increase bilayer, will reduce the horizontal resistance of air.(8) be fixing lightweight air chamber, the interior light gas (identical with the light gas of external capsule gas and composite air chamber) of this air chamber is not participated in compression cycle; The object of using this air chamber is the rigidity that increases dirigible front end, the resistance of air to dirigible during antagonism flight.(9) for the inner chamber skeleton (again claim fin) of manned loading with dress compression system, dress control part, of the material that wing gliding parachute skeleton is identical, make; Prevent that capsula interna from subsideing to load-carrying chamber.(10) be the strut bar of support helix oar, if when screw propeller is directly fixed on air bag front end, can save this bar.(11) be load-carrying chamber ship type sole, require to fix with skeleton, increase after base areas, just dwindle people and the thing base pressure to air bag; It makes (as plank, plastic flagstone etc.) with light weight board, is fixed on air bag inwall or air bag the latter half is directly made with light weight board with restricting, and the first half is made with air bag material.(12) be the pressure schematic lines of air to motion synthesis dirigible.
The selection of bag material: lightweight, any surface finish, stiffness high (reason is to reduce windage resistance, Reducing distortion and improve inflation performance, the polyester dacron of the anti tear of coated on both sides ultra-violet radiation resisting is made).Air bag monnolithic case is streamline contour (reason is the resistance of air while reducing airship flight, increases air to the lifting force of dirigible and constant-bearing navigation ability, and foundation is fluid continuity principle and Bernoulli theorem), requires sealing air tight.
The whole selection principle of Composite airship: weight is lighter, intensity is more high better.
Seven, profile kind: the profile kind of Composite airship is varied.
1, be mainly used as having of high-speed carriering tool: streamline contour, dish etc.
2, be mainly used in amusement and low speed and use having of the instrument of carrying: bar shaped, horse shape, ship shape etc.
3, be mainly used as have (as elevator, construction, the amusement etc.) of vertical pinpoint lifting tool: cylindrical, spherical, square etc.
4, having for advertisement, art and publicity: the abnormity of various shapes.
Eight, specific embodiments
1, streamline contour Composite airship, lifting is all placed in the manned loading chamber (hanging indigo plant) of dirigible and control system, compression system etc. in the air bag of dirigible.[do not repel streamline contour hang indigo plant (loading chamber) and screw propeller be placed in air bag bottom (minute direct-connected integral body or cotton rope interval articulate)], operation is controlled part and is placed in the front bottom of lifting airship air bag, and remaining is placed on rear lower.The object often changing for people and loads etc. is placed on center of gravity place.
2, dish-shaped Composite airship, is placed in bottom, the dish-shaped dirigible center of circle by ship shape loading chamber etc., and position, loading chamber is divided into directly whole or cotton rope interval and articulates, and loading chamber is divided into the relation of outer air bag: fixedly shape is with relative rotary-type.Utilize recoil moving system, allow recoil air-flow go out or to produce from the edge of flying saucer air bag, allow edge rotarily drive whole flight.
3,, 1. to needing this Composite airship of horizontal motion, by promoting screw propeller that dirigible moves flat, be placed on dirigible (above or below or two places, front and back) and promote this dirigible and put down to advancing at utmost speed.
2. for Composite airship and the modified product thereof of only requiring vertical lift, horizontal propulsion device and control setup be will save, lifting and control system and loading chamber function retained.
3. to this aircraft that only needs the short time to fly, adopt the power of combustion engine or battery band electrical motor action control system and horizontal propulsion system aloft.
4. to long-time this Composite airship of flight aloft of needs, adopt solar cell, as the power of control system and horizontal propulsion device, replace the power such as combustion engine battery.
While 4, increasing as far as possible load carrying ability or scarce light gas for needs, electro-heat equipment or thermal chemical reaction device can be installed in air bag or absorb solar radiation device and increase or dwindle air bag volume, control the lifting of this dirigible, electro-heat equipment now, thermal chemical reaction device and solar power are vacuum device used can be share mutually with the compression system of aforementioned lifting airship, or uses separately or in addition mutual applied in any combination.
Claims (3)
1. a dirigible of making lifting drive with gas compressor; It comprises the hanging basket being placed in balloon outer, be placed in the horizontal propelling screws of balloon outer front end and/or afterbody, for reduce between the double-walled of air resistance can relative motion balloon outer composite and double-walled between interval air chamber, for increasing the fixedly air chamber of dirigible front end rigidity, antagonism flight resistance, for a plurality of inner bladder of sealing to each other of Leakage prevention, for putting the cavity of gas compression system, object, operation control system.
2. dirigible according to claim 1, is characterized in that:
Application gas compression system is discharged into balloon outer by the light gas of inner bladder, the light gas of balloon outer is compressed in inner bladder, the volume size that arranges air to change whole balloon outer is used as the main lifting lifting force of this dirigible, with screw propeller, thermal chemical reaction device, electro-heat equipment as assistance for lifting lifting force, with solar energy equipment, collect the energy, make the long-time delay of this dirigible aerial.
3. dirigible according to claim 1, is characterized in that:
There is multiple product profile; Need the streamline contour of high-speed cruising, dish-shaped product, cylindrical, spherical, the square products that need elevator, cable car, the crane of vertical pinpoint lifting to use, do bar shaped, ship shape, the horse shape product of amusement or low speed transportation means, does advertisement, artistic special-shaped product.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN03103948.0A CN1521084B (en) | 2003-02-15 | 2003-02-15 | Composite airship |
Applications Claiming Priority (1)
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CN03103948.0A CN1521084B (en) | 2003-02-15 | 2003-02-15 | Composite airship |
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CN1521084B true CN1521084B (en) | 2014-03-19 |
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CN03103948.0A Expired - Fee Related CN1521084B (en) | 2003-02-15 | 2003-02-15 | Composite airship |
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2428656A (en) * | 1941-06-18 | 1947-10-07 | Arthur J Elliott | Dirigible airship |
US4773617A (en) * | 1987-03-05 | 1988-09-27 | Mccampbell Burton L | Lighter-than-air craft |
US6354535B1 (en) * | 1998-12-11 | 2002-03-12 | Southwest Research Institute | Autonomous stratospheric airship |
CN1359827A (en) * | 2000-12-22 | 2002-07-24 | 张涛 | Hard-shell balloon or airship using hydrogen safety and able to control its lifting |
CN1376617A (en) * | 2001-03-22 | 2002-10-30 | 高松 | Manned craft |
CN1392083A (en) * | 1997-01-04 | 2003-01-22 | 赫尔曼.孔克勒 | Aeroplane with fuselage designed as air static floatage body on the whole |
-
2003
- 2003-02-15 CN CN03103948.0A patent/CN1521084B/en not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2428656A (en) * | 1941-06-18 | 1947-10-07 | Arthur J Elliott | Dirigible airship |
US4773617A (en) * | 1987-03-05 | 1988-09-27 | Mccampbell Burton L | Lighter-than-air craft |
CN1392083A (en) * | 1997-01-04 | 2003-01-22 | 赫尔曼.孔克勒 | Aeroplane with fuselage designed as air static floatage body on the whole |
US6354535B1 (en) * | 1998-12-11 | 2002-03-12 | Southwest Research Institute | Autonomous stratospheric airship |
CN1359827A (en) * | 2000-12-22 | 2002-07-24 | 张涛 | Hard-shell balloon or airship using hydrogen safety and able to control its lifting |
CN1376617A (en) * | 2001-03-22 | 2002-10-30 | 高松 | Manned craft |
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Granted publication date: 20140319 Termination date: 20150215 |