CN105649775B

CN105649775B - With system and method, aircraft that compressed air is force source

Info

Publication number: CN105649775B
Application number: CN201610125197.0A
Authority: CN
Inventors: 王力丰
Original assignee: Individual
Current assignee: Individual
Priority date: 2016-03-04
Filing date: 2016-03-04
Publication date: 2017-06-23
Anticipated expiration: 2036-03-04
Also published as: CN105649775A

Abstract

The invention provides a kind of with system that compressed air is force source, including being to spray the compressed air ramjet (14) of working medium with high-voltage and ultra-high compressed air, the compressed air of a large amount of production storage supply high-voltage and ultra-high compressed airs in economic, environmental protection ground is produced for device (48) and controller；The compressed air ramjet (14) is arranged on the motion carrier of the Aeronautics and Astronautics such as aircraft, rocket, submarine, train, navigation and ground run, and the compressed air ramjet (14) is including laying in the gas tank (9) of compressed air and producing the ramjet (16) of power；The ramjet (16) is including main ramjet (41) for producing thrust, and multiple pair ramjets are used for air (or seawater) resistance that reduces during motion carrier is advanced and are beneficial to speed-raising, energy-conservation with the force of sliding friction of air (or seawater), and it is beneficial to aircraft short distance or VTOL etc. for improving aircraft wing lift.

Description

With system and method, aircraft that compressed air is force source

Technical field

The present invention relates to technical field of engines, especially provide a kind of with system that compressed air is force source and its side Method, aircraft.

Background technology

Engine (Engine), i.e. engine, be it is a kind of can the machine that can be converted into mechanical energy of other forms, be born In Britain, external-combustion engine and internal combustion engine development stage are successively experienced.The fuel of external-combustion engine such as steams in the external firing of engine Steam turbine；The fuel of internal combustion engine burns in engine interior, such as gasoline engine, diesel engine and jet engine.In fact, no matter in hair The outside or inside burning of motivation, the effect of burning is all generation " HTHP " gas in engine；Analysis " high temperature " and The direct effect of " high pressure ", professional knows that the effect of " high temperature " is essentially consisted according to the in-engine gas of thermodynamic principles Body pressure rise, the effect of " high pressure " then directly to do that mechanical work is related, the height of gas pressure determines that its is exported in engine The size of moment of torsion (such as steam engine, gasoline engine, diesel engine) or thrust (such as jet engine).

It is power output moment of torsion with " high pressure " gas of generation of burning just like steam engine, gasoline engine, diesel engine, has authorized Patent " economic utilization compressed air is the system of car power source " (patent No.：201520365135.8, inventor：Wang Lifeng) Disclose a kind of air compression power device (including it is vehicle-mounted storage tracheae and cylinder combine engine), using " high pressure " compressed air as Power source output torque, for producing driving power.

And just like jet engine with " high pressure " gas of generation of burning as power output thrust, it is contemplated that inquire into " high pressure " compressed air is used as power source thrust output, there is provided a kind of with system that compressed air is force source.

On prior art jet engine, there are various mode classifications, can be generally divided into aero-jet engine and fire The major class of arrow engine two.Wherein aero-jet engine is such to go back herein with turbojet (Turbojet) as representative Centrifugal-flow jet engine, axial flow turbojet, turbofan, punching press can be more specifically subdivided into Jet engine, pulse jet engine etc.；Rocket engine includes chemical energy rocket engine, electric energy rocket engine, core Energy rocket engine, solar rocket engine etc., current chemical energy rocket engine development are more ripe, with relatively wide, lead to Normal rocket engine is to refer to chemical energy rocket engine, can be divided into liquid-propellant rocket engine and solid propellant rocket.

Wherein, turbojet include 1., air intake duct, air through this enter next structure compressor；2., calm the anger Machine, is made up of stator (stator) blade with rotor (rotor) blade stagger, and a pair of stator vanes are referred to as one-level with rotor blade (generally having 8-12 grades), stator is fixed in engine frame, and rotor is connected with armature spindle with turbine；3., combustion chamber and whirlpool Wheel, air produces high temperature and high pressure gas expansion work, cocurrent by entering combustion chamber and fuel oil mixed combustion after compressor compression Cross turbine and promote turbine (most modern times opportunities of combat install after-burner additional to improve motor power after turbine)；4., jet pipe (nozzle, or Spray mouths), its convergence, convergence-expand the tube shape structures shape state of the air-flow of final discharge.Liquid Rocket engine be using the rocket engine of liquid propellant, generally comprise 1., promote mainly injector, be by liquid propellant The chemical energy of (fuel and oxidant) is transformed into the significant components of propulsive force, by propellant nozzle, combustion chamber and nozzle component etc. (fuel and oxidant enter combustion chamber to composition through propellant nozzle atomized spray, in combustion chamber mixed combustion, produce HTHP gas Body is discharged from nozzle component), 2., propellant feed system, by fuel and oxidant tank, fuel and oxidant pump, fuel and 3., engine control system oxidant transfer pipeline and valve etc. are constituted, by computer control with to measure engine system each The sensor of parameter, all kinds of valves and adjuster etc. are collectively formed, and 4., igniter (propellant enter combustion chamber when Punctum fire) etc..Solid propellant rocket be using the rocket engine of solid propellant, by 1., powder column, 2., combustion chamber, 3., Nozzle component and 4., the composition such as igniter, powder column mixes and is made in advance by solid propellant (fuel and oxidant) Directly filling is put into storage room to hollow circular cylinder (hollow space is combustion front, and its shape of cross section has circle, star etc.), works When storage room be exactly combustion chamber, propellant burns generation high temperature and high pressure gas herein, and nozzle component is by jet pipe and thrust vector control System composition processed, igniter is generally made up of for lighting powder column electric squib and gunpowder box.Rocket engine is employed State the semi-enclosed combustion chamber connecting spray nozzle (convergent-divergent channel) of special structure-mono-, such structure only to one outlet of combustion gas- Flowed in terms of jet pipe, other directions are restricted, therefore, combustion gas can be set up in combustion chamber certain pressure (1~ 20MPa), and the outer surface pressure of nozzle exit there was only 0.1MPa (sea-level atmosphere pressure) or (high-altitude is very less than 0.1MPa even zero To exoatmosphere), then combustion gas flows to jet pipe in the presence of inside and outside differential pressure, ejects at a high speed.In above-mentioned jet engine " HTHP " gas produced in combustion chamber, is subject to the active force flow direction spray that engine combustion chamber interior walls apply under " high pressure " Guan, according to Newton's third law, must be exactly to one reaction force of engine, this reaction force when gas departs from engine The thrust of engine, and " high pressure " pressure is higher, and usual engine performance is also better, and thrust is bigger.

The self-contained propellant of prior art jet engine (fuel or fuel oxidizer) and its related setting of burning Apply, it is heavier to the whole machine of engine, construction is complicated, be difficult to control, cost is higher, development ＆ production difficulty is big related.Such as aviation spray The self-contained fuel oil of gas engine, and need to carry as draw air is set as oxidant with fuel oil reactive combustion from air Multistage compressor, multistage turbine, multistage fan etc. not only increase weight but also greatly increase research and development manufacture difficulty, its difficulty reaches Such degree：Only Britain's Rolls-Royce share that first-class level turbofan technology is grasped in the whole world has Limit company abbreviation sieve sieve (Rolls-Royce Group plc, LSE：RR), the general Levin of state of U.S. is special and Whitney Jane Said Pu Hui And General Electric's aviation (GE Aviation) Deng Ji companies (Pratt＆Whitney)." father of space travel " Qi Aoerkefu Si Ji (K_{OHCтаHтиH} Ц_{иOΛковский}, 1857-1935) and propose that with " mass ratio " be the original of rocket at first The ratio of the remaining mass of quality and rocket weighs the performance of rocket, and he calculates and reaches the using nitric acid plus Hydrazine propellant The mass ratio of the rocket of one astronautical speed for 23.5, i.e. 100 tons of gross weight rocket need 96 tons of propellants, if plus terrestrial gravitation because Element, then mass ratio will be bigger, i.e., payload will be smaller with mass ratio of taking off.Aerospace field improve payload with In the research and development of mass ratio of taking off, two patents " high initial speed the projectile transmitting device " (patent No. for having authorized： 201420224494.7, inventor：Wang Lifeng) with " goods Rotary transport flywheel and its control method " (patent No.： 201110351539.8, inventor：Wang Lifeng) individually disclose a kind of high initial speed projectile transmitting device and a kind of goods rotation fortune Defeated flywheel and its control method, are able in flywheel rotates at a high speed with high initial speed launch payload, and reduce effectively load The difficulty that the weight of lotus is come to conveyer belt, they relate generally to the flywheel principle and its technology outside jet engine technical field The utilization of means.The mass ratio of rocket how is reduced, or how to improve rocket payload and quality of taking off for generally climbing over The ratio between, being always one has in the industry problem to be solved.From some prior art carrier rocket payload with take off quality it The data of ratio, can peep one spot：Israel's comet number (Shavit) payload accounts for quality 0.7% of taking off, India's polar-orbiting satellite fire Arrow (Polar Satellite Launch Vehicle) satellite accounts for the 1% of quality of taking off, Japanese H rocket series (H Launch Vehicles) payload accounts for quality 0.7% of taking off, and U.S.'s Saturn number (Saturn) payload accounts for the 1.6% of quality of taking off, Russian proton number (Proton) satellite accounts for the 0.3% of quality of taking off, and the payload that the Chinese Long March five is accounted for takes off quality about 2% etc., it is clear that the ratio of quality of being taken off shared by propellant and its related facility of burning is tangible at a relatively high (about 98-99%).

And it is a general knowledge out of question that compressed air can also produce thrust.Compressed air is main in existing rocketry It is applied to the cold air rail control Push Technology of one of rail control Push Technology.Rail control Push Technology generally include chemical propulsion, Cold air propulsion, electric propulsion, nuclear propulsion, momentum conversion are advanced and without working medium propulsion system etc., complete three kinds of functions：Gesture stability (keeping aircraft to point to the direction of setting), track keep (keep aircraft to be run on specified track) and Orbit Transformation (make aircraft from the track that current track moves to that another specifies).Wherein cold air propulsion system, i.e. rail control are advanced The cold air rail control Push Technology of one of technology, is typically made using compressed gas (such as air, nitrogen, helium, carbon dioxide) It is injection working medium, the typical usual thrust output scope 0.05N~22N of cold air propulsion system, is Spacecraft Attitude Control, track Keep and Orbit Transformation provides required thrust, torque；And cold air propulsion system uses MEMS (Microelectromechanical System) technology is easily achieved the miniaturization of system, integrated, composition micro propulsion device And with the basic industries such as microelectronics, micromachine, lightweight composite materials and Ultra-precision Turning are developed rapidly can integral installation On dividing plate is installed, be easily installed with replacement, and be applied successfully to as cold air micromass culture system small, micro-nano satellite cold The satellite of weight ＞ I000kg (is generally referred to as large satellite, weight is 500kg~1000kg by the practice and research of gas propulsion system Satellite be referred to as Satellite, weight is referred to as moonlet for the satellite of I00kg~500kg, and weight claims for the satellite of I0kg~I00kg It is microsatellite, and the satellite of Ikg~I0kg is referred to as Nano satellite, the satellite of 0.1kg~Ikg is referred to as skin satellite, and ＜ 0.1kg's defends Star is referred to as flying satellite).Prior art cold air propulsion system, on the one hand advances skill from the analysis of its functional character as a kind of rail control Art does not produce the demand of rocket main thrust using the compressed air of a large amount of high-voltage and ultra-highs, while on the other hand from existing skill Art cold air propulsion system structure signature analysis also without as a kind of rocket power jet using a large amount of high-voltage and ultra-highs compress Air is the technical characteristic and report in force source.

Have reason to envision, even if not against self-contained oxidized burning " high temperature " generation " high pressure " gas, starting Machine can also provide thrust by injection working medium of self-contained a large amount of high-voltage and ultra-high compressed airs.It is wherein airborne to lay in enough High-voltage and ultra-high compressed air is simultaneously supplied to engine as the device of working medium, herein referred to as " gas tank ", can use for reference patent " economical It is the system of car power source using compressed air " (the patent No.：201520365135.8, inventor：Involved by Wang Lifeng) The storage air pipe structure function of vehicle-mounted compressed air is subject to Curve guide impeller；And utilize the dress of high-voltage and ultra-high compressed air expansion work Put and (such as promote mainly injector：Expanding chamber, jet pipe), refer to conventional art liquid-propellant rocket engine and promote mainly injector (combustion chamber, spray Pipe) structure function be subject to Curve guide impeller.This engine with high-voltage and ultra-high compressed air as working medium, according to Newton's law (mainly the 3rd law, and second law) provides thrust, can be used for such as aircraft, rocket, naval vessels, vehicle motion carrier.

Contrast conventional art jet engine, its spout should not lean on closely, can not be against motion carrier in itself, because it sprays Mouthful scorching hot combustion gas for spraying ablation motion carrier surface or may at least increase the heat fatigue of its structure, and future trouble is serious；And from pressure The gas temperature that contracting aerojet engine spout sprays quite can closely be leaned on, put down without height like that, the high velocity air that it is ejected Row can directly brush the upper surface of wing, it might even be possible to oblique in certain distance, certain angle scope in motion carrier surface Against carrier head injection high velocity air, worry of the motion carrier without ablation damage.And conventional art jet engine Jet pipe generally only occurs at motion carrier rear portion, the inferior sustainer routine installation portion of the wing due to being correlated closely with fuel combustion Position；And compressed air ramjet jet pipe not can only occur in motion carrier rear portion, the inferior sustainer routine installation portion of the wing Position, in fact can be arranged at the substantially any position in need in motion carrier periphery, only need to be by high-voltage and ultra-high compressed air Air inlet pipe is connected thereunto.So, on the one hand according to " father of hydrodynamics " Denier Bernoulli Jacob (Daniel Bernoulli, 1700-1782) bernoulli principle of " air-flow or flow rate of water flow are increased, and pressure reduces " that proposes (Bernoulli's principle), and Coanda effect (Coanda Effect, also known as attached wall effect) etc., compressed air spray Gas engine jet pipe can be arranged on motion carrier front, body week, position and spray high velocity air at these positions before the wing etc., involve Corresponding local air force changes, gas density falls sharply, pressure declines, and corresponding hydrodynamics can be produced to motion carrier motion Influence, makes these compressed air ramjets that reduction running resistance such as air can be also endowed in addition to foregoing thrust and hinders The function such as power and frictional resistance, raising airfoil lift；Another aspect compressed air ramjet jet pipe may be provided at airframe Lower section spout produces downwards certain thrust vertically upward beneficial to airplane short takeoff, or set airframe afterbody lower section or Both sides spout with certain speed jet-stream wind, makes the aircraft buffer deceleration in traveling forward, beneficial to short distance landing.It is full side Position, it is multi-functional.

Clearly for " gas tank " of the airborne compressed air of the compressed air ramjet in proposal, indispensable one kind It is its production, storage, the device for supplying high-voltage and ultra-high compressed air, is compression herein referred to as " compressed air is produced and supplies device " " gas tank " inflation of aerojet engine.And it is known, the cost for producing high-voltage and ultra-high compressed air is very high, and main system is because raw About the 90% of the electric energy consumed in product converts my heat energy.The recycling of this partial heat energy can use for reference preceding patent " economic utilization Compressed air is the system of car power source " (the patent No.：201520365135.8, inventor：One kind involved by Wang Lifeng) The structure function that boiler type high pressure air produces storage device is improved, designed；Additionally, abbreviation " the compression in improving, designing Air is produced and supplies device ", due to the storage of compressed air in " gas tank " as the compressed air ramjet of the motion carriers such as aircraft Amount, pressure are all much larger than and the reserves higher than automobile mounted caisson compressed air, pressure are economically produced, it is necessary to be adapted to The high-voltage and ultra-high compressed air higher with a greater amount of, pressure is stored is filled with to " gas tank " of compressed air ramjet pressurization Gas；And also need to solve the problems, such as charging efficiency of pressurizeing, such as " compressed air is produced and supplies device " to compressed air ramjet " gas tank " pressurization inflation in, the design pressure of " gas tank " is also very high, when compressed air pressure in " compressed air produce supply device " When dropping to equal with " gas tank " of compressed air ramjet, also there are a large amount of high pressure compresseds in " compressed air is produced and supplies device " The unserviceable problem of air.This just must a kind of " compressed air product supplies device " and compressed air ramjet " gas tank " phase Mutually matchingly design, be designed to " gas tank " for including " compressed air produce supply device " and compressed air ramjet is System, it is a kind of with system that compressed air is force source.

The content of the invention

(1) technical problem to be solved

Can economically utilize high-voltage and ultra-high compressed air it is an object of the invention to provide one kind, with compressed air jet Motion carrier propulsive force, speed-raising of the engine as the Aeronautics and Astronautics such as aircraft, rocket, submarine, train, navigation and ground run With the system for increasing the force such as lift source.

(2) technical scheme

To achieve the above object, the invention provides a kind of with system that compressed air is force source, it is characterised in that bag It is to spray the compressed air ramjet of working medium to include with high-voltage and ultra-high compressed air, and compressed air is produced and supplies device and controller；

The compressed air ramjet is arranged on motion carrier；The compressed air ramjet includes gas tank and spray Gas engine；The gas tank is compressed-air-storing container, including multiple cylinders, the cylinder is used to laying in and supplying described Compressed air needed for ramjet；The ramjet includes main ramjet and multiple pair ramjets；The main jet gas It is to spray working medium that engine is used for the compressed air that be input into from the cylinder, and pushing away of travelling forward is granted to the motion carrier Power；Multiple secondary ramjets include the first secondary ramjet, the second pair that are separately positioned on around the motion carrier Ramjet, the 3rd secondary ramjet, fourth officer ramjet and the 5th secondary ramjet, for being input into from the cylinder Compressed air the motion carrier is formed on target direction for injection working medium and by coordinating with the main ramjet Push；

The compressed air is produced includes high-voltage and ultra-high air compressor and large-sized boiler formula pressure vessel for device；It is described The operating pressure of high-voltage and ultra-high air compressor is close, 100Mpa is equaled or exceeded, under the control of the controller Pressurizeed to the large-sized boiler formula pressure vessel and inflated；The large-sized boiler formula pressure vessel is used to producing and storing compression sky Multiple cylinder pressurizations are inflated by gas with the control of the controller；

The controller is used for by the main ramjet, the first secondary ramjet, the second secondary ramjet, the 3rd Secondary ramjet, the open and close controlling of fourth officer ramjet and the 5th secondary ramjet and target side is formed to the motion carrier To push.

Preferably, the main ramjet, the first secondary ramjet, the second secondary ramjet, the 3rd secondary ramjet, the Fourth officer ramjet and the 5th secondary ramjet include that the air inlet pipe, expanding chamber and the drawing that are made up of high pressure resistant, lighter material are cut down That jet pipe；

The air inlet pipe is connected between the cylinder and the expanding chamber；Air inlet pipe is provided with around the air inlet pipe All electric heaters, the air inlet pipe week electric heater is used to heat the compressed air in the air inlet pipe, so that the air inlet pipe Interior air pressure is raised；Compressed air in the cylinder is injected in the expanding chamber by the mouth of emanating of the air inlet pipe；

The expanding chamber locular wall of the expanding chamber injects adjuster equipped with gas, and the gas injects adjuster for regulating and controlling institute State air inlet pipe and inject setting pressure to the amount of the compressed air in the expanding chamber, so that the air pressure in the expanding chamber is maintained Setting pressure；Expanding chamber locular wall electric heater is provided with around the expanding chamber, the expanding chamber locular wall electric heater is used to make It is heated into the compressed air in the expanding chamber and is pressurizeed；

The sectional area of the De Laval noz(zle) first diminishes become big again from front to back；Cut down with the drawing end of the expanding chamber You are connected as a single entity at the tapered portion of jet pipe, and the expanding chamber compressed air accelerates tapered by the De Laval noz(zle) under stress Portion, De Laval noz(zle) throat and De Laval noz(zle) gradually wealthy portion, final high velocity air are sprayed by De Laval noz(zle) spout.

Preferably, the described first secondary ramjet is arranged on the front of the head of motion carrier；Described first secondary jet is drawn The profile with raindrop shape is held up, its front face area is less than the front face area of the corresponding motion carrier head；Described first is secondary Ramjet includes the first air inlet pipe, the first expanding chamber and the first De Laval noz(zle), described also including a firm tubular structure First secondary ramjet is fixed on the front of the motion carrier head by the firm tubular structure；The first air inlet pipe position Supported within the firm tubular structure and by the firm tubular structure；The end and first of first expanding chamber The tapered portion of De Laval noz(zle) is connected as a single entity；First De Laval noz(zle) is in integrally from front to back Rafael nozzle shape structure； First air inlet pipe is stretched out forwards together with the firm tubular structure from the head of motion carrier, and to described in forward position first Axially center sequentially passes through the first secondary ramjet spout, the first De Laval noz(zle) gradually wealthy portion, the first Laval to secondary ramjet Nozzle throat, the first De Laval noz(zle) tapered portion and first expanding chamber and with the expansion chamber-head of first expanding chamber Portion's inwall is fixedly connected；The expanding chamber head inwall equipped with the first air inlet pipe emanate mouth and gas injects adjuster；It is described First expanding chamber compressed air accelerates by the first De Laval noz(zle) tapered portion, the first De Laval noz(zle) larynx under stress Portion, finally by the gap positioned at first De Laval noz(zle) gradually between wealthy portion and the conical huge portion of firm tubular structure Rearward sprayed to around motion carrier head along a conical side surface, the bus of the conical side surface is equivalent to from described First De Laval noz(zle) throat is bored to the line of the motion carrier head periphery with forming one in front of the motion carrier head Bodily form low-pressure area, for reducing air drag or seawater resistance that the motion carrier runs forward；

Described first secondary ramjet is additionally operable to grant the tractive force that the motion carrier travels forward.

Preferably, the quantity of the described second secondary ramjet is multiple, and multiple described second secondary ramjets are circumferentially disposed In the week side of boss of the motion carrier, multiple described second secondary ramjet spouts spray at a high speed towards the rear of the motion carrier Air-flow travels forward to the motion carrier and grants thrust, and the high velocity air that the described second secondary ramjet spout is ejected Surface parallel and close to motion carrier, motion carrier is reduced to form one layer of low-pressure air layer around motion carrier Sliding-frictional resistance when running forward and between the external world.

Preferably, the motion carrier is provided with one or more described gas tanks, and the multiple in each described gas tank is described Cylinder is long tubular structure, with the cylindrical shape gas storage tube wall being made up of high pressure resistant, lighter material；

Multiple parallel bunchy arrangements of the cylinder, and cross section is that entirety is in plum blossom-shaped structure；Each described cylinder It is equipped with the intake valve and air bleeding valve individually opened and closed by controller control；

Standby electric heater is provided with around the cylinder, the standby electric heater is used in compressed air spray Start when gas engine works overloadingly for some reason, all the cylinder compressed air pressure is below setting lower limit；

One end of multiple cylinders many siphunculus of being bullied with are connected, and many siphunculus of being bullied converge for one is received Tracheae；The other end of multiple cylinders is communicated with many siphunculus of gas transmission, and multiple paths of many siphunculus of gas transmission converge It is combined into an appendix；The cylinder is connected by the appendix with the air inlet pipe；

The compressed air that the pipe of being bullied is filled with for receiving to be pressurizeed from the large-sized boiler formula pressure vessel.

Preferably, be the gas tank cylinder pressurization inflation the large-sized boiler formula pressure vessel include large-scale flowing Water tank and several Large Copacity tubular containers and collector for being placed in the water tank；

Several described Large Copacity tubular containers are divided into the comb of multigroup tiling shape, the multiple described comb in same group Two ends are connected to a collector；Comb shape described in wherein described Large Copacity tubular container, there is its entrance and exit；With The collector of the entrance connection of the Large Copacity tubular container in every group holds for the Large Copacity tubulose in arrival end collector, with every group The collector of the outlet of device is port of export collector；The entrance of the Large Copacity tubular container is provided with inlet valve, described The outlet of Large Copacity tubular container is provided with outlet valve；The arrival end collector is provided with a header inlet and its header inlet valve Door, the port of export collector is provided with a manifold outlet ports and its manifold outlet ports valve；

The design volume and pressure of the Large Copacity tubular container are respectively greater than and higher than the design volume of the cylinder And pressure；The part Large Copacity tubular container is coiled pipe, and the coiled pipe is multiple in the plane of comb tiling The tubular structure of roundabout extension；

It is laid in the comb in approximately the same plane, the arrival end collector of the coiled pipe and its both sides and outlet End collector constitutes a Large Copacity tubular container plane；Multiple Large Copacities are provided with a large-scale flowing water tank Tubular container plane, the arrival end collector in multigroup Large Copacity tubular container plane passes through arrival end header in communication Guan Lian It is logical, and a header inlet is shared, header inlet valve is provided with the header inlet；Each Large Copacity tubular container Port of export collector in plane is connected by port of export header in communication pipe, and shares the manifold outlet ports, and the collector goes out It is intraoral to be provided with manifold outlet ports valve；

The large-scale flowing water tank is provided with the water inlet for flowing into cooling water and the delivery port for flowing out hot water, institute Delivery port is stated to be connected with the direct buried insulating tube in central heating system；

The air compressor exhaust port of the high-voltage and ultra-high air compressor is detachably connected with the header inlet, for The Large Copacity tubular container pressurization inflation.

Present invention also offers a kind of aircraft, including as described above with the system that compressed air is force source, wherein institute State the first secondary ramjet and be arranged on plane nose front, the described second secondary ramjet is arranged on the week side of boss of airframe；And And the quantity of the 3rd pair ramjet is multiple, multiple described 3rd secondary ramjets are symmetricly set on aircraft both sides wing Leading edge front；The spout of the described 3rd secondary ramjet wing injection high velocity air rearward, and the described 3rd secondary spray The direction of the high velocity air that the spout of gas engine is ejected is consistent relative to the airflow direction of wing with when taking off sliding race； Described 3rd secondary ramjet is used to improve airfoil lift in aircraft short distance or VTOL, is additionally operable to grant corresponding to institute State the thrust travelled forward to the aircraft that the 3rd secondary ramjet spout gas injection reaction force is made a concerted effort.

Preferably, the fourth officer ramjet is arranged on the lower section of the airframe, for the back lower place to aircraft Or front lower place jet-stream wind, to grant the reaction force of forward upward or back upper place to the aircraft；Described 5th secondary jet is drawn The both sides for being arranged on immediately below the afterbody of the aircraft or being symmetricly set on afterbody are held up, for the inverse of the aircraft flight direction To injection high velocity air, buffer deceleration is played a part of with to the aircraft.

Present invention also offers a kind of operation method with system that compressed air is force source, comprise the following steps：

Step one：Pressurization inflation is carried out to large-sized boiler formula pressure vessel by high-voltage and ultra-high air compressor；

Header inlet valve, whole Large Copacity tubular container inlet valves and outlet valve are opened in this course, and Manifold outlet ports valve closing；

Motor is difficult the power supply of storage using night dip electric energy or wind-powered electricity generation, solar energy etc., empty by high-voltage and ultra-high Header inlet valve, whole Large Copacity tubular container entrance of the air compressor through air compressor exhaust port, header inlet and its unlatching And its inlet valve opened and whole Large Copacity tubular container outlet and its outlet valve opened are to being arranged at large-scale stream Arrival end collector, whole Large Copacity tubular containers and the pressurization inflation of port of export collector in dynamic water tank；

The air pressure and tolerance of the gas that controller control is filled with from air compressor exhaust port are adapted to from large-scale flowing water tank Cooling water and the water-carrying capacity of the hot water of delivery port outflow that water inlet is flowed into, make to hold in arrival end collector, whole Large Copacity tubuloses Occurred together in compressed air production process in device and the port of export collector generation heat in time be cooled water take away, cooling water is added Heat is used for central heating for the hot water of proper temperature leads to direct buried insulating tube from delivery port outflow in good time, until in arrival end Still basic a large amount of compressed airs that the temperature remains within the normal range reach design in collector, whole Large Copacity tubular containers and port of export collector High pressure, stores for future use；

Header inlet valve, whole Large Copacity tubular container inlet valves and outlet valve are closed when the time comes, manifold outlet ports valve Door continues to close；

Step 2：Inflated to gas tank by large-sized boiler formula pressure vessel；

Header inlet valve and whole Large Copacity tubular container inlet valves are closed in this course, whole Large Copacities Only single difference is opened in order in tubular container outlet valve and remaining is closed, manifold outlet ports valve opening；Manifold outlet ports and gas What cylinder was shared in case is docked by tracheae, and each cylinder intake valve only open and remaining closing in order by single difference in gas tank； Controller control compressed air in an orderly manner from some Large Copacity tubular container open outlet valve through open manifold outlet ports What cylinder was shared in valve, manifold outlet ports, gas tank is filled by tracheae and some cylinder intake valve opened to the cylinder Enter compressed air；

Air pressure is gradually reduced during a Large Copacity tubular container is inflated to cylinder one by one, so that wheel later Air pressure has dropped to gradually increase with the cylinder being bullied in the Large Copacity tubular container when being inflated to certain cylinder Air pressure it is equal, at this moment the Large Copacity tubular container is powerless is further continued for the cylinder gas transmission gas storage intraductal atmospheric pressure not yet Design requirement is raised to, controller controls the opening and closing of major capacity tubulose container outlet valves and each cylinder intake valve, makes air pressure The Large Copacity tubular container for having declined is inflated to not yet inflation or pressure low cylinder relatively, is made by the blowing pressure Although the gas storage for having risen but being not yet raised to design requirement is in control the Large Copacity tubulose with initial high pressure or relatively high pressure Container is inflated to it；

Wherein, come for cylinder internal memory air from during Large Copacity tubular container input cylinder in compressed air Say that pressure has certain intensification trend, but this part for being input to from Large Copacity tubular container in cylinder in rising Its pressure declines and has cooling trend for compressed air, and controller controls compressed air to be input into from Large Copacity tubular container The flow of cylinder, speed, make gas storage intraductal atmospheric pressure in this course be increased to design requirement steadily and intensification trend and drop Warm trend relative equilibrium, temperature is basicly stable；

Step 3：Gas tank is supplied gas to ramjet；

In the ramjet course of work, all cylinder intake valves are closed in gas tank, each cylinder air bleeding valve in gas tank Only single or several difference are opened in order and remaining is closed；Controller control compressed air in an orderly manner therefrom some or it is several Air bleeding valve that cylinder is opened, appendix send into connected air inlet pipe, and then via being arranged on penetrating for expanding chamber head Gas port, gas inject adjuster and inject expanding chamber；

Air inlet pipe caliber is smaller compared with cylinder caliber, and all electric heaters of air inlet pipe and expanding chamber locular wall electric heater work, Compressed air into expanding chamber is flowed into and expanding chamber end company successively under high pressure by appropriate heating, holding elevated pressures The De Laval noz(zle) tapered portion that is integrated, through De Laval noz(zle) throat and by De Laval noz(zle), gradually wealthy portion sprays, air-flow pole It is big to accelerate, huge thrust is produced, high velocity air also involves the change of corresponding local air force.

(3) beneficial effect

The invention provides a kind of with the system that compressed air is force source, wherein compressed air ramjet is as machine The high-voltage and ultra-high compressed air of gas tank conveying of compressed-air-storing container is carried for injection working medium produces power, is taken without itself With conventional art jet fuel and its related facility of burning, thus whole machine loss of weight, construction simplify, cost it is relatively low, profit In research and development, production, control and application.

Approached with operating pressure in the present invention, equal or exceed 100Mpa high-voltage and ultra-highs air compressor to the great Rong The cylinder that amount tubular container pressurization is inflated and then provides the gas tank by high-voltage and ultra-high compressed air is standby；The high pressure surpasses The motor of High-Pressure Compressor is utilized includes that night dip electric energy and the wind-powered electricity generation for being difficult to store work；A large amount of high-voltage and ultra-highs It is that compressed air occurs together in production process in the Large Copacity tubular container, converted equivalent to 90% electric energy for being consumed There is heat exchange in amount of heat, be heated to form hot water for central heating with the cooling water for flowing into the large-scale flow cistern.Cause And accomplish production compressed air pressure it is high, utilization of power is economic, while clean heat supply and energy-saving and emission-reduction.

In the gas tank of compressed air ramjet of the present invention, cylinder, snorkel, expanding chamber and De Laval noz(zle) High-voltage and ultra-high compressed air pressure can be approached, equal or exceed 100MPa, and its value can be more than prior art rocket chamber The pressure (1~20MPa) of interior combustion gas, can provide higher forces for main ramjet, and thrust-weight ratio is higher, " mass ratio " is relatively low, profit In raising payload and mass ratio of taking off.

Because compressed air ramjet spout of the present invention injection high velocity air temperature is started far below conventional art jet The scorching hot combustion gas that machine sprays will not cause ablation to damage on motion carrier body surface, peripheral facilities, road surface or deck, can be using its spray Penetrate high velocity air and involve local generation air force change, multiple pair ramjets may be provided at aircraft, rocket, train, submarine Deng motion carrier front and the week side of boss, for reducing the motion carrier traveling air drag or seawater resistance, force of sliding friction, have Beneficial to speed-raising, energy-conservation；May also be arranged on aircraft wing front, body lower section and tail is used to improve aircraft wing lift, raise Airframe and make aircraft buffer deceleration, be conducive to aircraft short distance/VTOL.

Brief description of the drawings

Fig. 1 is the schematic diagram of the structure of embodiment of the present invention compressed air ramjet；

Fig. 2 is in Fig. 1At IThe schematic perspective view of section stravismus；

Fig. 3 is the schematic side view of the secondary ramjet of the embodiment of the present invention first；

Fig. 4 is elevational cross-section enlarged diagram at II in Fig. 3；

Fig. 5 is that the compressed air ramjet of the embodiment of the present invention sets schematic side view aboard；

Fig. 6 is that embodiment of the present invention compressed air produces the structural representation for supplying device；

Fig. 7 is the schematic elevation view of embodiment of the present invention Large Copacity tubular container plane.

Reference：

1st, cylinder；2nd, gas storage tube wall；3rd, by tracheae；4th, it is bullied many siphunculus；5th, intake valve；6th, air bleeding valve；7th, gas transmission Many siphunculus；8th, appendix；9th, gas tank；10th, cylinder first；11st, cylinder second；12nd, cylinder third；13rd, cylinder fourth；13a, storage Tracheae penta；14th, compressed air ramjet；15th, standby electric heater；16th, ramjet；17th, air inlet pipe；17a, the first air inlet Pipe；18th, expanding chamber；18a, the first expanding chamber；19th, De Laval noz(zle)；19a, the first De Laval noz(zle)；20th, De Laval noz(zle) is gradually Contracting portion；20a, the first De Laval noz(zle) tapered portion；21st, De Laval noz(zle) throat；21a, the first De Laval noz(zle) throat；22nd, draw Cut down that jet pipe gradually wealthy portion；22a, the first De Laval noz(zle) gradually wealthy portion；23rd, De Laval noz(zle) spout；24th, high velocity air；25th, emanate Mouthful；26th, gas injects adjuster；27th, expanding chamber head；28th, expanding chamber locular wall；29th, air inlet pipe week electric heater；30th, expand Room locular wall electric heater；31st, the first secondary ramjet；32nd, motion carrier head；32a, line；33rd, firm tubular structure； The conical huge portion of 33a, firm tubular structure；34th, firm tubular structure and air inlet tube end；35th, emanate mouth and gas is penetrated Enter adjuster；37th, expanding chamber head inwall；39th, the first secondary ramjet spout；40th, cone-shaped low-pressure area；41st, main jet gas draws Hold up；42nd, the second secondary ramjet；43rd, raindrop shape profile；44th, the 3rd secondary ramjet；45th, upper surface of the airfoil；46th, fourth officer Ramjet；47th, the 5th secondary ramjet；48th, compressed air is produced and supplies device；49th, large-sized boiler formula pressure vessel；50th, high pressure Super high pressurized air compressor；51st, motor；52nd, air compressor exhaust port；53rd, collector；54th, large-scale flowing water tank；55th, intake Mouthful；56th, delivery port；57th, direct buried insulating tube；58th, cooling water；59th, hot water；60th, Large Copacity tubular container；61st, Large Copacity Tubular container tube wall；62nd, Large Copacity tubular container first；63rd, Large Copacity tubular container second；64th, Large Copacity tubular container third；65、 Arrival end collector；66th, header inlet；67th, header inlet valve；68th, port of export collector；69th, manifold outlet ports；70th, manifold outlet ports Valve；71st, arrival end header in communication pipe；72nd, port of export header in communication pipe；73rd, Large Copacity tubular container plane；74th, comb； 75th, coiled pipe；76th, Large Copacity tubular container entrance；77th, Large Copacity tubular container outlet；78th, Large Copacity tubular container inlet valve Door；79th, Large Copacity tubular container outlet valve.

Specific embodiment

Following examples are used to illustrate the present invention, but are not limited to the scope of the present invention.

In the description of the invention, it is necessary to explanation, unless otherwise clearly defined and limited, term " connection " should do Broadly understood, for example, it may be being fixedly connected, or being detachably connected, or be integrally connected；Can be joined directly together, Can also be indirectly connected to by intermediary；Can electrically connect, or communicate to connect.For the ordinary skill of this area For personnel, above-mentioned term concrete meaning in the present invention can be understood with concrete condition.

As shown in figs. 1-7, the present embodiment describes a kind of with system that compressed air is force source, it is characterised in that bag It is to spray the compressed air ramjet 14 of working medium to include with high-voltage and ultra-high compressed air (hereinafter referred to as compressed air), economically The device abbreviation compressed air of the production storage a large amount of compressed airs of supply is produced and supplies device 48, and controller；

The compressed air ramjet 14 is arranged on the Aeronautics and Astronautics such as aircraft, rocket, submarine, train, navigation and ground On the motion carrier of face traveling, the compressed air ramjet 14 includes gas tank 9 and ramjet 16；The gas tank 9 is pressure Contracting air storage volume, it includes several cylinders 1, and the compression needed for for laying in and supplying the ramjet 16 is empty Gas；The ramjet 16 includes main ramjet 41 and multiple pair ramjets；The main ramjet 41 may be provided at The inferior conventional art jet engine of aircraft tail, wing installation position aboard, or it is arranged on rocket, submarine, train etc. The rear end of motion carrier, for the compressed air that is input into from the gas tank 9 be injection working medium, to above-mentioned Aeronautics and Astronautics, navigation And the motion carrier of ground run grants the thrust for travelling forward；Multiple secondary ramjets for be arranged on aircraft, rocket, The secondary ramjet 31, second of the first of each position of motion carrier of the Aeronautics and Astronautics such as submarine, train, navigation and ground run The secondary ramjet 44 of secondary ramjet the 42, the 3rd, the secondary ramjet 47 of fourth officer ramjet the 46, the 5th, for from described The compressed air of the input of gas tank 9 is injection working medium, plays a part of the operation of the motion carriers such as second-mission aircraft；

The compressed air is produced includes high-voltage and ultra-high air compressor 50 and large-sized boiler formula pressure vessel for device 48 49；The operating pressure of the high-voltage and ultra-high air compressor 50 is close, 100Mpa is equaled or exceeded, with the control Pressurizeed to the large-sized boiler formula pressure vessel 49 under the control of device and inflated；In the large-sized boiler formula pressure vessel 49 production and The compressed air of storage can pressurize under the control of the controller and be filled with the cylinder 1 of the gas tank 9, for the major and minor spray Gas engine is utilized；

The controller is the automatic control system for including computer, sensor, all kinds of valves and its adjuster, and described Connected with system components that compressed air is force source, for control it is described with system coordination that compressed air is force source, Work in order；Wherein be mainly used in by the main ramjet, first the 31, second secondary ramjet 42 of secondary ramjet, 3rd secondary ramjet 44, the open and close controlling of fourth officer ramjet 46 and the 5th secondary ramjet 47 and to the motion carrier Form the push of target direction.

As shown in Figure 1, Figure 2 with shown in Fig. 5, the ramjet 16, no matter the main ramjet 41 or each secondary ramjet, Include air inlet pipe 17, compressed air expanding chamber hereinafter referred to as expanding chamber 18 and De Laval noz(zle) 19 (De Laval nozzle), It is made up of high pressure resistant, lighter material；

The air inlet pipe 17 is connected between the cylinder 1 and the expanding chamber 18, the length of the air inlet pipe 17 and Position where moving towards the cylinder 1 and the expanding chamber 18 with its two ends is relevant, with each major and minor ramjet institute It is equipped with pass in place；Air inlet pipe week electric heater 29 is provided with around the air inlet pipe 17, the compressed air in the cylinder 1 passes through The mouth 25 of emanating of the air inlet pipe 17 injects the expanding chamber 18；

The inner face of expanding chamber locular wall 28 of the expanding chamber head 27 injects adjuster 26 equipped with compressed air gas, described to penetrate Gas port 25 is to constitute the primary element that the gas injects adjuster 26, and the gas injects adjuster 26 and regulates and controls the air inlet pipe Institute is injected with certain flow by the compressed air of the air inlet pipe week appropriate heating of electric heater 29 thus pressure raising in 17 State expanding chamber 18；The expanding chamber 18 is cylindrical shape, or spherical or annular, and its volume size is ensureing from the air inlet pipe 17 compressed airs injected in it maintain design pressure to be defined, and expanding chamber locular wall electric heater 30 is provided with around the expanding chamber 18 Compressed air appropriate heating to entering the expanding chamber 18, is beneficial to maintenance compressed air pressure and swollen in the expanding chamber 18 Swollen acting；The end of the expanding chamber 18 is connected as a single entity with the De Laval noz(zle) tapered portion 20；

The sectional area of the De Laval noz(zle) 19 (also known as tapered gradually wealthy jet pipe) diminishes and then becomes big again first, by tapered portion Wealthy portion 22 of 20-throat 21-gradually constitutes, and is one " flow velocity enhancer "：Compressed air is under the effect of the pressure of expanding chamber 18 Tapered portion 20 is initially entered, is followed herein the original of " when fluid is moved in pipe, the small place's flow velocity in section is big, and section general goal flow velocity is small " Reason, air-flow constantly accelerates, and flow velocity can exceed velocity of sound when reaching throat 21, and transonic fluid is no longer followed in motion " The small place's flow velocity in section is big, and section general goal flow velocity is small " principle, but on the contrary, section is bigger, flow velocity is faster, in gradually wealthy portion The speed of 22 air-flows is further accelerated to supersonic speed, is sprayed with high flow velocity；

The spout of ramjet 16 injection high velocity air 24, produces huge thrust, for making the main jet described in the present embodiment Gas engine 41 grants propulsion to the motion carrier of the Aeronautics and Astronautics such as aircraft, rocket, submarine, train, navigation and ground run Power；The high velocity air 24 of the spout of the ramjet 16 injection simultaneously involves local generation air force change and the gas flow temperature is remote The scorching hot combustion gas sprayed less than conventional art jet engine will not be to motion carrier body surface (and peripheral facilities, road surface or first Plate) cause ablation to damage, the first secondary ramjet 31 can be made to be arranged on the Aeronautics and Astronautics such as aircraft, rocket, submarine, train, navigation And the front of motion carrier head 32 of ground run is for reducing (or the seawater resistance of air drag that the motion carrier is advanced Power), and the second secondary ramjet is arranged on submarine kayak body the week side of boss (not shown) for reducing kayak body and sea when submarine is travelled The force of sliding friction of water, also can distinguish the 3rd secondary ramjet 44, the secondary ramjet 47 of fourth officer ramjet 46 and the 5th Being arranged on aircraft wing front, body lower section and tail is used to improve aircraft wing lift, raise airframe and delay aircraft Eat up part of speed.

As shown in Fig. 3, Fig. 4 and Fig. 5, the described first secondary ramjet 31 is arranged on the front of the head 32 of motion carrier； Described first secondary ramjet 31 has the profile 43 of raindrop shape, and its front face area is less than the corresponding motion carrier head 32 Front face area；Described first secondary ramjet 31 includes the first air inlet pipe 17a, the first expanding chamber 18a and the first De Laval noz(zle) 19a, also including a firm tubular structure 33, is fixed on by the described in the firm tubular structure 33 first secondary ramjet 31 The front of motion carrier head 32；The first air inlet pipe 17a is located within the firm tubular structure 33, and for described firm Tubular structure 33 is supported；The end of the first expanding chamber 18a is connected as a single entity with the tapered portion 20a of the first De Laval noz(zle)； The first De Laval noz(zle) 19a is from front to back integrally in the tapered gradually wealthy structure of Rafael nozzle shape；First air inlet pipe 17a stretches out forwards together with the firm tubular structure 33 from the head 32 of motion carrier, and to the described in forward position first secondary jet Axially center sequentially passes through the first secondary ramjet spout 39, the first De Laval noz(zle) gradually wealthy portion 22a, the first Laval to engine 31 Nozzle throat 21a, the first De Laval noz(zle) tapered portion 20a and the first expanding chamber 18a, the then firm tubular structure And air inlet tube end 34 is fixedly connected with the expanding chamber head inwall 37；In the expanding chamber head of the first expanding chamber 18a Wall 37 equipped with the first air inlet pipe emanate mouth and gas injects adjuster 35；The first expanding chamber 18a compressed airs are in pressure Accelerate by the first De Laval noz(zle) tapered portion 20a, the first De Laval noz(zle) throat 21a under power, finally by positioned at institute State gap of first De Laval noz(zle) gradually between wealthy portion 22a and the conical huge portion 33a of firm tubular structure rearward along One conical side surface sprays to around motion carrier head, and the bus of the conical side surface is equivalent to from first Laval Nozzle throat 21a forms a cone to the line 32a of the periphery of motion carrier head 32 with the front of motion carrier head 32 Bodily form low-pressure area 40, for reducing air drag or seawater resistance that the motion carrier runs forward；

The first secondary ramjet 31 is mainly used in reducing the air drag that the motion carrier runs forward described in the present embodiment (or seawater resistance), the motion carrier runs forward thrust essentially from the main ramjet 41, and the described first secondary jet is drawn Hold up 31 spout gas injections reaction force make a concerted effort to have to the described first secondary ramjet 31 propulsive force forward i.e. The size of " traction force " that is travelled forward to the motion carrier, the controller control.

The quantity of the described second secondary ramjet 42 is multiple, the circumferentially disposed the week side of boss in the motion carrier, Duo Gesuo The second secondary spout of ramjet 42 is stated to transport the motion carrier forward towards the rear injection high velocity air of the motion carrier It is dynamic to grant thrust, and the high velocity air that the described second secondary spout of ramjet 42 is ejected is parallel and close to motion carrier Surface, between reducing when motion carrier the runs forward and external world to form one layer of low-pressure air layer around motion carrier Sliding-frictional resistance；

Described second secondary ramjet is arranged at submarine (not shown) body week, can there is multiple, and their spout is backward Square closely to lean on and spray high velocity air parallel to hull surface, the high velocity air covers submarine body surface, and flow velocity is greatly and to submarine body surface Normal pressure is small, and can dispel, rolling off is close to the seawater of submarine kayak body, and one layer of low-pressure air layer is formed around submarine kayak body, from And reduce the sliding-frictional resistance when submarine runs forward with surrounding seawater；And these described second secondary ramjets to Rear gas injection also grants certain thrust to submarine traveling.

As shown in Figure 1, shown in Figure 5, the described 3rd secondary ramjet 44 is arranged on aircraft wing leading edge front, symmetrical, often Side can set one or more the described 3rd secondary ramjets 44, and their spout wing rearward sprays high velocity air 24, its The angle of direction and the wing chord (leading edge of wing and the line of trailing edge) of spout injection high velocity air is equivalent to taking off sliding race When wing the angle of attack (Angle of attack) direction of air-flow and angle of wing chord when taking off sliding race, in other words institute State the direction of the 3rd secondary spout of ramjet 44 injection high velocity air and take off airflow direction when cunning is run relative to wing Unanimously；So, the high velocity air of the described 3rd secondary spout of ramjet 44 injection increases wing upper and lower surface pressure differential (wing The air velocity high pressure of upper surface 45 is low), the high velocity air of the described 3rd secondary spout of ramjet 44 injection also impacts and has The wing lower surface of certain angle of attack, and the air-flow of the described 3rd secondary spout of ramjet 44 injection is close to the wing upper table of protrusion Face 45 flows to the downward high-speed motion of air-flow for leaving wing, therefore according to bernoulli principle, Newton's third law, Coanda effect (Coanda Effect) the described 3rd secondary spout of ramjet 44 so sprays high velocity air has the work for improving airfoil lift With；

The lift formula of aircraft can generally be expressed as：

(wherein：Y is airfoil lift, C_yIt is lift coefficient, ρ is atmospheric density, and υ is speed of the air-flow relative to wing, S It is wing area)

Here, independent development of the present invention is a kind of to be applied to aircraft short distance or the simple mathematical of VTOL is theoretical, wherein Air-flow is referred to as " gas velocity " relative to the speed υ of wing, aircraft is referred to as " machine speed " and uses V relative to the speed of runway_aRepresent, And a new term " gas velocity machine speed ratio " is proposed accordingly, represented with B：

B=gas velocity/machine speed=υ/V_a

Under normal circumstances, during approximate calculation, υ ≈ V_a, in generally taking off that acceleration is sliding and running when υ reach its minimum safe from During ground speed (aircraft starts lift-off), B=υ/V_a≈1；

And for the aircraft with the described 3rd secondary ramjet 44, the described 3rd secondary spout of ramjet 44 is to its rear Wing injection high velocity air flow velocity herein be referred to as jet speed, be set to V_e, therefore for the described 3rd secondary ramjet 44 aircraft gas velocity υ is equivalent to machine speed V_aWith jet speed V_eSum, υ=V_a+V_e；

It is very high from the described 3rd secondary ramjet 44 (Fig. 5) Laval nozzle 19 (referring to Fig. 1) ejection air-flow velocity, as above State and can reach/exceed velocity of sound (>=340.29m/s, equivalent to >=1225km/h), the takeoff speed of remote super any aircraft (it is general and Speech, the takeoff speed of aircraft is in 200-350km/h), aircraft just run by off even not yet cunning, the only the 3rd secondary spout of ramjet 44 The jet speed V of high velocity air is sprayed to the wing at its rear_eThe gas velocity υ (i.e. speed of the air-flow relative to wing) of composition has reached To, more than the aircraft minimum safe flying speed (aircraft starts lift-off), " gas velocity machine speed ratio " B ratios (B=υ/V now_a) Greatly, machine speed V_aIt is very small, that is, take off it is sliding run aircraft in very short distance and gone up to the air, realize short distance/take off vertically；

When needing short distance/vertical landing, airfield approach enters near, glides, and evens up, and receives " throttle " to idling ... aircraft speed Degree (machine speed V_a) continue to reduce to the 3rd secondary ramjet 44 before airfoil lift is not enough to balance airplane weight and work with it to machine Winged injection high velocity air maintains airfoil lift (with jet speed V_eMaintain gas velocity υ), " gas velocity machine speed ratio " thus is improved, aircraft can be In the air, the secondary ramjet 44 of at this moment controller control the 3rd sprays for the predetermined slow decelerating flight in landing runway top or almost hovering Mouth jet is gradually slowed down, jet speed V_eGradually drop is that gas velocity υ gradually drops, and gradually dropping to airfoil lift to gas velocity υ is not enough to balance airplane weight Amount, aircraft descends slowly and lightly and contacts to earth, and the 3rd secondary ramjet 44 is stopped, and aircraft alightings run short distance to stopping with its leaving velocity, completes Short distance/vertical landing；

3rd secondary ramjet 44 described in the present embodiment has short distance/vertical to rise under the control of the controller in aircraft Drop needs or opens during other special circumstances, and controls its power output it is typically applied forward to aircraft within the specific limits The propulsive force of flight is very small；When necessary the controller can control the described 3rd secondary 44 pairs of aircrafts of ramjet apply to The propulsive force of preceding flight is moderately increased.

As shown in Figure 1, shown in Figure 5, the fourth officer ramjet 46 be arranged on airframe lower section its spout can be to aircraft The back lower place or front lower place jet-stream wind will not ablation road surface or deck the reaction force of forward upward or back upper place is granted to aircraft, And the 5th pair ramjet 47 is arranged on immediately below airplane tail group or the symmetrical reversible flight of its spout in tail both sides Direction jet has the effect of certain buffer deceleration to aircraft flight；

The spout of fourth officer ramjet 46 is to airframe described in when being necessary during aircraft short distance/take off vertically Back lower place jet-stream wind assists the described 3rd secondary ramjet 44 to work to the reaction force of the certain forward upward of aircraft One step shortens takes off ground run distance；

The 5th secondary spout of ramjet 47 described in when being necessary during aircraft short distance/vertical landing is against heading Jet makes aircraft, and the spout of fourth officer ramjet 46 is certain to aircraft to airframe front lower place jet-stream wind Reaction force rearwardly and upwardly, coordinate the described 3rd secondary ramjet 44 to work further to assist aircraft to be run in predetermined landing Road top is slow to fly or hovering, shortening aircraft landing ground run distance；

The secondary ramjet 47 of fourth officer ramjet the 46, the 5th described in the present embodiment is flying under the control of the controller Machine is opened when having short distance/VTOL needs or other special circumstances, and their power output is limited to coordinate, assists described 3rd secondary ramjet 44 completes aircraft short distance/VTOL.

As shown in Figure 1, Figure 2, shown in Fig. 3 and Fig. 5, on the Aeronautics and Astronautics such as aircraft, rocket, submarine, train, navigation and ground One or more the described gas tanks 9 matched with the major and minor ramjet can be set on the motion carrier of traveling；Described in each Multiple described cylinder 1 in gas tank 9 is long tubular structure, and its cylindrical shape gas storage tube wall 2 is by high pressure resistant, lighter material structure Into, its caliber less than the internal diameter of the identical capacity of conventional art and the compressed air reservoir of pressure therefore in the case of phase same material its Can pipe deposit pressure compressed air higher；

Multiple cylinders 1 can be arranged with front and rear parallel longitudinal bunchy, and such as its cross section is in plum blossom-shaped, referred to as plum tube Or it is more accurately called several hole plum tubes, such as Seven-hole plum tube；Wherein each described cylinder 1 respectively has its He of intake valve 5 Air bleeding valve 6 is certainly into a gas storage unit that can individually open and close；Multiple cylinders 1 are equivalent to multiple gas storage lists Unit, they can be referred to as cylinder first 10, cylinder second 11, cylinder the third 12, cylinder fourth 13, holder pipe penta according to sequence The design pressure of 13a ... their calibers, length and the gas tank 9, capacity are relevant；

Standby electric heater 15 is provided with around the cylinder 1, the standby electric heater 15 does not start generally, in institute State compressed air ramjet 14 work overloadingly for some reason, all the compressed air pressure of cylinder 1 be below a certain setting Fix limit certain in emergency circumstances, the in good time emergency start of the back-up heater 15 heats the cylinder 1, makes in its pipe Compressed air is heated up pressure rise simultaneously, and now air inlet pipe week electric heater 29, expanding chamber locular wall electricity add Hot device 30 is also met an urgent need and improves heating-up temperature, to maintain to be exported from the cylinder 1, inject the expanding chamber through the air inlet pipe 17 18 compressed air keeps certain temperature and pressure, and the dynamic of the compressed air ramjet 14 is maintained within a period of time Power；

The cylinder 1 can also spiral and draw close one with the space of the framework of the motion carrier where it, tendency, or bending Rise, or nature stretching, extension of taking advantage of a situation, and the cylinder 1 is disposed proximate to the ramjet that matches with it in the conceived case Position where 16, the cylinder 1 for such as matching with the 3rd ramjet 44 may be provided among aircraft wing Space；

Multiple cylinders 1 share one and receive tracheae 3, i.e., the front of their own intake valve 5 respectively with one Many siphunculus 4 of being bullied are communicated, and many siphunculus 4 of being bullied converge for one by tracheae 3, than seven air inlets of such as above-mentioned Seven-hole plum tube Valve 5 is just communicated with seven pipes in eight siphunculus, eight siphunculus vacant pipe be the Seven-hole plum tube share by tracheae 3；Similarly multiple cylinders 1 share an appendix 8, i.e., their own air bleeding valve 6 respectively leads to more with a gas transmission Pipe 7 is communicated, and it is an appendix 8 that many siphunculus 7 of gas transmission converge, than if seven air bleeding valves 6 of above-mentioned Seven-hole plum tube with Seven pipes in another eight siphunculus are communicated, eight siphunculus vacant pipe be the shared appendix 8 of the Seven-hole plum tube；

Wherein, a gas tank 9 can draw with a ramjet 16, the main ramjet 41 or secondary jet Hold up, match supply, at this moment the shared appendix 8 of each cylinder 1 in the gas tank 9 is straight with the air inlet pipe 17 of the ramjet 16 Lead in succession；One gas tank 9 also can be with multiple ramjets 16, the main ramjet 41 or secondary ramjet, phase Matching supply, at this moment the shared appendix 8 of each cylinder 1 in the gas tank 9 can bifurcated be that multiple pipelines match with above-mentioned again The air inlet pipe 17 of multiple described ramjet 16 be respectively communicated with；

What multiple cylinders 1 were shared in the gas tank 9 is used to receive to hold from the large-sized boiler formula pressure by tracheae 3 The compressed air that the pressurization of device 49 is filled with.

As shown in Figure 6,7, be the gas tank 9 cylinder 1 pressurization inflation the large-sized boiler formula pressure vessel 49 wrap Include large-scale flowing water tank 54 and several Large Copacity tubular containers 60 being placed in the water tank；The Large Copacity tubular container 60 is tubular, and its tube wall 61 is made by high pressure resistant, lighter material, and its caliber is less than identical capacity and the conventional art pressure of pressure The internal diameter of contracting air storage tank, it is tolerable in the case of phase same material and accommodates pressure compressed air relatively higher；

Multiple Large Copacity tubular containers 60 are laid into comb 74 in the large-scale flowing water tank 54, their two End is connected with collector 53, and every comb 74 is that each Large Copacity tubular container 60 has its entrance 76 and outlet 77 and its inlet valve Door 78 and outlet valve 79, the collector being connected with their entrance are referred to as arrival end collector 65, the collection being connected with their outlet Pipe is referred to as port of export collector 68, and the arrival end collector 65 and port of export collector 68 are respectively equipped with a header inlet 66 and collector Outlet 69, and it is respectively equipped with corresponding header inlet valve 67 and manifold outlet ports valve in the header inlet 66 and manifold outlet ports 69 Door 70；

The design volume and pressure equalization of the wherein single Large Copacity tubular container 60 not great Yu and it is described higher than single The design volume and pressure of cylinder 1；When a certain off-capacity of the comb 74 is to meet design requirement, due to necessary Ensure that tube wall is competent to bear high pressure and should not select to expand caliber to expand capacity, it is necessary to pass through that extension tube is long to reach setting for dilatation Meter is when requiring, can be with coiled pipe 75-a kind of repeatedly roundabout pipe in the plane that the comb 74 tiles-substitute the comb It is arranged between the arrival end collector 65 and port of export collector 68, the coiled pipe 75 is also with the entrance at its two ends, inlet valve Door and outlet, outlet valve are connected with the arrival end collector 65 and port of export collector 68 respectively；

It is laid in a comb 74 of plane, the coiled pipe 75 and its arrival end collector 65 described in both sides and outlet End collector 68 constitutes a Large Copacity tubular container plane 73；Multiple can be provided with a large-scale flowing water tank 54 The Large Copacity tubular container plane 73, wherein the phase intercommunication of arrival end collector 65 in each Large Copacity tubular container plane 73 Cross arrival end header in communication pipe 71 to connect, and share a header inlet 66 and its corresponding header inlet valve 67；Respectively Port of export collector 68 in the Large Copacity tubular container plane 73 is connected each other by port of export header in communication pipe 72, and is shared One manifold outlet ports 69 and its corresponding manifold outlet ports valve 70；

Wherein, the every comb 74 or coiled pipe 75 are relatively independent equivalent to a Large Copacity tubular container 60 i.e. Compressed air produce storage unit, be equivalent to multiple great Rong with many combs 74 and/or coiled pipe 75 In the case of amount tubular container 60, they can be referred to as Large Copacity tubular container first 62, Large Copacity tubular container second according to sequence 63rd, the multiple Large Copacity tubular containers 60 of Large Copacity tubular container the third 64 ... can be with the large-scale flowing water tank 54 Arranged by other forms, they can connect and be arranged in spiral arrival end collector and port of export collector such as in cylinder type water tank Between；

The large-scale flowing water tank 54 is provided with water inlet 55 so that cooling water 58 is flowed into, and delivery port 56 is so as to hot water 59 The logical direct buried insulating tube 57 of outflow is connected with central heating system；

The air compressor exhaust port 52 of the high-voltage and ultra-high air compressor 50 can be flexibly connected with the header inlet 66, The motor 51 of the high-voltage and ultra-high air compressor 50 includes that night dip and the wind-powered electricity generation for being difficult to store work using electric energy, Pressurizeed to each Large Copacity tubular container 60 by the header inlet 66 and inflated；A large amount of compressed airs are in these great Rong The amount of heat occurred together during being produced in amount tubular container 60 is sent out with the cooling water 58 for flowing into the large-scale flowing water tank 54 Heat is exchanged, and the cooling water 58 flows out the direct buried insulating tube 57 of remittance for central heating after being heated to form hot water 59； The a large amount of compressed airs produced in these described Large Copacity tubular containers 60 can be stored therein in, when needed the manifold outlet ports 69 can be filled with compression with being flexibly connected by tracheae 3 for the cylinder 1 in the gas tank 9 to the cylinder 1 in the gas tank 9 Air；

The large-sized boiler formula pressure vessel 49 can be arranged on ground, underground, on large ship, vehicle such as truck, On train and on bulk transport aircraft, the large-sized boiler formula pressure being provided with vehicle, bulk transport aircraft holds Device 49 can empty water in the large-scale flowing water tank 54, large-scale flowing water tank 54 described in removal before lifting or starting Instead a kind of protection shell of compact light weight is covered in outside the Large Copacity tubular container 60 casing, referred to as tubular container packaging Case (not shown), is readily transported, to be arranged on the compressed air on the motion carriers such as aircraft, rocket, train, submarine The cylinder 1 of the gas tank 9 of ramjet 14 is inflated；

Wherein, the tubular container container is set in being allowed on bulk transport aircraft as a kind of aerial filling machine, can Aerial aerating is implemented as the aircraft by mechanism of qi to other outfit compressed air ramjets 14；The airborne institute of aerial filling machine State the manifold outlet ports 69 in tubular container container leant out to square tube type after machine and end can be in umbrella tapered sleeve, it is described to receive On mechanism of qi head equipped with it is telescopic be bullied inserting tube (not shown) its received with described in cylinder 1 in the gas tank 9 on the machine Tracheae 3 mutually continues, by mechanism of qi and the machine of filling machine two " congregation " after, treat that the inserting tube of being bullied is connected automatic with the tapered sleeve of the umbrella Locking, gas circuit turn on automatically is completed " docking ", and aerial filling machine starts to aerial " aerating ", then two machines " dismission " by mechanism of qi.

As shown in Fig. 3, Fig. 5, the compressed air ramjet 14 may be provided at the boat such as aircraft, rocket, submarine, train On the motion carrier of sky, space flight, navigation and ground run；

Wherein aboard, the main ramjet 41 and the secondary ramjet 42 of the first secondary ramjet 31, second, 3rd secondary ramjet 44, the secondary ramjet 47 of fourth officer ramjet the 46, the 5th can be selected using or with certain traditional skill The collocation of art engine is used：1., the described first secondary ramjet 31, the described second secondary ramjet 42 are used to reduce aircraft flight Air drag and its force of sliding friction with air, are conducive to airplane accelerating, energy-conservation；2., the 3rd secondary ramjet 44, fourth officer Ramjet 46 can be used for aircraft short distance/take off vertically, and the 3rd secondary ramjet 44, fourth officer ramjet the 46, the 5th are secondary Ramjet 47 can be used for aircraft short distance/vertical landing；3rd secondary ramjet 44, fourth officer ramjet the 46, the 5th are secondary Ramjet 47 is before aircraft wing, under fuselage, the above-mentioned functions position such as tail be fixedly installed, or activity is set, i.e., these draw Hold up usually and be converged in during flight to be reduced in wing and/or fuselage and expose movable part, only having aircraft short distance/VTOL Above-mentioned functions position is reached when needing and is started；3. aerial aerating, can be carried out whenever necessary；4., overwork makes for some reason The compressed air pressure of the cylinder 1 can start back-up heater 15 when relatively low, maintain the compression empty within a period of time The power of gas ramjet 14；5., if necessary, such as when main 41 failure of ramjet, the 3rd secondary ramjet can be increased 44 power maintain one section of flight；6., the in emergency circumstances secondary jet of the 3rd secondary ramjet 44, fourth officer ramjet the 46, the 5th Engine 47 cooperates makes aircraft safety short distance/vertically land on a certain spacious region；And the main ramjet 41 7. With the described first secondary ramjet 31, the described second secondary secondary ramjet 44 of ramjet the 42, the 3rd all can to the aircraft to Thrust is granted in preceding motion；

The main ramjet 41 and the first secondary ramjet 31, the described second secondary ramjet can be arranged on fire On arrow, the compressed air design pressure of 41 expanding chamber of main ramjet 18 can notable >=20MPa, higher than in rocket chamber Combustion gas maximum pressure, and it is simple structure, light, advantageously reduce " mass ratio " of rocket；Described first secondary ramjet 31, institute State the second secondary ramjet and advantageously reduce rocket and fly out air drag and the force of sliding friction with air before atmosphere, make rocket Speed-raising, energy-conservation；And the main ramjet and the first secondary ramjet 31, the described second secondary ramjet all can be to institute State rocket and travel forward and grant thrust；

The main ramjet 41 and the secondary ramjet of the first secondary ramjet 31, second or they are traditional with certain The selection collocation of technology engine, is configurable on submarine；Described first secondary ramjet 31 is for dispelling, rolling off is hindered in submarine Seawater in front of head, forms a cone-shaped low-pressure area 40 (or even region of no pressure) in front of submarine head；Described second secondary spray Gas engine is for dispelling, rolling off is close to the seawater of submarine kayak body, and one layer of low-pressure air layer is formed around submarine kayak body, makes originally Submarine in the seawater high pressure of depths in low-pressure air, advantageously reduces the slip of seawater resistance and kayak body and seawater just like traveling Frictional force, makes submarine speed-raising, energy-conservation, and Jing Yin；The main ramjet and the first secondary ramjet 31, described second Secondary ramjet can all travel forward to the submarine and grant thrust；

The main ramjet 41, the secondary ramjet of the first secondary ramjet 31, second or they are traditional with certain The selection collocation of technology engine, can configure ON TRAINS；Described first secondary ramjet 31 is used in front of the train head A cone-shaped low-pressure area 40 (or even region of no pressure) is formed, air drag is advantageously reduced, makes train speed raising, energy-conservation；Multiple institutes State the second secondary ramjet spout and spray high velocity air towards the rear of the train (not shown), in the train body Around form one layer of low-pressure air layer and reduce the sliding-frictional resistance when train runs forward with air；Wherein, it is right In both sides there is aerofoil profile shape to protrude the train of structure, multiple described second secondary ramjets are arranged on the aerofoil profile shape and protrude structure Front, and rearward train body surface include the aerofoil profile shape protrude body structure surface injection high velocity air, although the wing Type shape protrude structure upper surface is streamlined raised but its distance prominents to both sides it is very small-small protrude knot to the aerofoil profile shape The lift that structure is produced is not enough to the train to lifting in the air, but because high velocity air is brushed in aerofoil profile shape protrusion structural table The lift that face produces alleviates normal pressure of the train to track, so as to reduce wheel and track during the train advances Force of rolling friction, is conducive to the train energy-saving, speed-raising；And the main ramjet, the first secondary ramjet 31, second are secondary Ramjet all travels forward to the train and grants thrust；And can set above-mentioned for airplane tail group in the last vehicle of train The 5th secondary ramjet, it can This train is bound for XXX that reverse jet is used for the train deceleration, parking to described.

The a kind of of the present embodiment is had the advantage that with the system that compressed air is force source：

1) it is without combustion to be rotated into from internal combustion engine from conventional art jet engine to compressed air ramjet 14 of the present invention Machine, it is to avoid the side effect and puzzlement related to burning

1. from self-contained fuel and its related facility of burning, simplify whole machine loss of weight, construction, cost it is relatively low, profit In research and development, production, control and application.

2. the technical barrier related to combustion high temperature is avoided：

Conventional art jet fuel, up to about 3500K (~5800 °F), often exceeds spray in combustion chambers burn temperature The fusing point (except graphite and tungsten) of pipe and combustor material, it is necessary to ensure that these materials will not burn, melt or seethe with excitement；Combustion chamber Under certain hoop stress, due to high-temperature work environment, making the tensile strength of its structural material significantly reduces, and also makes it can The design pressure that can be born is subject to a definite limitation；Also need to prevent material from overheating using cooling system, the conventional type of cooling is such as Ablation cooling (locular wall has ablator, can constantly absorb heat and come off), radiation cooling (make locular wall reach incandescent state with radiant heat Amount), sink type cooling (by a kind of propellant, typically liquid hydrogen falls down along locular wall), (propellant is before combustion first for re-generatively cooled Flow through the cooling collar in locular wall), Water-Curta in Cooling is (propellant jet device by special placement, so that the fuel gas temperature around locular wall Reduce), film cooling (locular wall is soaked by liquid propellant, liquid evaporation heat absorption be allowed to cool down), Sweat coolling (film cooling Special shape) etc., engine structure complexity, weightening ... these problems and combustion high temperature of conventional art jet engine are made unavoidably Correlation, and they are not hindered with compressed air ramjet 14 of the present invention.

3. due to not fill-before-fire high-temperature fuel gas, instead the relatively quite low high velocity air of injection temperation, will not carry to motion Body causes ablation to damage, therefore the present invention can involve the change of local air force using each secondary ramjet spout injection high velocity air Change, realize reducing air (or seawater) resistance and with air (or seawater) sliding-frictional resistance, improve the function such as airfoil lift.

2) produce for high-voltage and ultra-high compressed air economy, environmental protection

Conventional art jet engine (containing aero-jet engine, rocket engine), burning fuel produced HTHP gas Volume expansion is done work, and thus produces three subject matters：Resource consumption, environmental pollution, greenhouse gas emission, wherein aircraft and rocket Working depth is high, and the nitrogen oxides of generation is easier to damage the ozone layer.With compressed air ramjet 14 of the present invention powered motion Carrier, including aircraft, rocket, submarine, train etc., with high-voltage and ultra-high compressed air as power, when their Aeronautics and Astronautics, boat Zero-emission and nothing very resource consumption when sea, ground run；

Even if discharge and cost when investigating initial production high-voltage and ultra-high compressed air：Heretofore described high pressure Super high pressurized air compressor 50 (operating pressure close to, equal or exceed 100Mpa) can using night dip electric energy or wind-powered electricity generation, The electric energy that solar energy etc. is difficult storage is produced for the pressurization inflation of device 48 to the compressed air；And high-voltage and ultra-high air is in institute Stating a large amount of heat energy (equivalent to 90% electric energy for being consumed) occurred together in production process in large-sized boiler formula pressure vessel 49 can quilt Centralized recovery is used for central heating.

Therefore to the present invention with system that compressed air is force source from whole efficiency (The overall efficiency) Analysis, also pretty economical, inexpensive, energy-conservation, environmental assessment are good.

3) 14 expanding chamber of compressed air ramjet of the present invention, 18 pressure are high, thrust is big, safety, good seal

1., pressure is high, thrust is big

Professional knows that conventional art jet engine such as rocket chamber operating pressure are pressed between 1--20MPa Power is higher, and usual performance is also better, and thrust is relatively also larger.

And with the development of modern age pressure vessel, Pneumatic Transmission element and material science, the output of ultra high pressure compression air engine Pressure reaches>100MPa, super-pressure (code name U) container p >=100MPa in pressure vessel, far above 20MPa；

In addition Large Copacity tubular container 60 and cylinder 1 are long tubular structure in the present invention, and their caliber is respectively less than The internal diameter of identical capacity, the conventional art high pressure air air accumulator of pressure, it is tolerable in the case of phase same material and holds Receive pressure compressed air relatively higher, its according to one of can be found in the pressure formula that pipe in the mechanics of materials can bear

P=(2* σ/S* δ)/D

(wherein：P is pressure, and σ is tensile strength, and S is safety coefficient, and δ is wall thickness, and D is tube outer diameter)

And, in the present invention, high-voltage and ultra-high compressed air is injected in the way of expanding chamber 18 from cylinder 1 by air inlet pipe 17 Also by air inlet pipe week electric heater 29 and the appropriate heating of expanding chamber locular wall electric heater 30, be also conducive to its expansion work, obtain Thrust higher.

2., safety

Pressure vessel has formulated safety standard (Safety codes) as a kind of ripe industry, and safety standard is limited Fracture pressure (the rupture of the legal operating pressure (the legal workingpressure) less than caisson Pressure) 40%, safety coefficient be 2.5 the ratio between (that is, limit stress and allowable stress be 2.5), security reliability；

For another example the common feature in university textbook to the Pneumatic Transmission with compressed air as working medium is expressly recited：Air pressure Actuation is rapid, reaction is fast, and working environment adaptability is strong, is particularly disliked in the big temperature difference, inflammable and explosive, many dust, vibration etc. Safe and reliable work under bad operating mode, has the advantages that fire prevention, explosion-proof, energy-conservation, efficient, pollution-free；

With progress in materials science, pressure vessel is often made up of high pressure resistant, light weight carbon fiber, and carbon fiber is fragility, Even if can divide under the pressure of super large, but any shell fragment is not resulted in, housing " broken ", compressed air leakage at most only occurs The unsafe condition that fragment and gases at high pressure flash, would not occur in situation about going out, and security is also relatively preferable.

3., good seal

As for seal aspect, as Pneumatic Transmission technical progress valve seal technology is also relatively reliable, professional knows One contrast, the discouraged speed ratio of compressed air caisson battery in the case of non-electric automatically will as time went on The speed that its electricity slowly exhausts is also low.

4) motion carrier running resistance, speed-raising, energy-conservation are reduced；Aircraft wing lift is improved, beneficial to short distance/VTOL

These advantages and the present invention, can with the high-temperature fuel gas that high-voltage and ultra-high compressed air is force source and non-burning generation The air force produced around motion carrier according to bernoulli principle using the injection high velocity air 24 of the Laval nozzle 19 Change is relevant.

The Laval nozzle of Swede's Gustaf Erik de Laval (Gustav de Laval) invention, is acknowledged as " Flow velocity enhancer ", extensively using the jet pipe as rocket engine；Laval nozzle is as described in existing above in the present invention, The effect of " flow velocity enhancer " is also functioned to, makes to spray high velocity air 24 from the spout of the ramjet 16；

According to the Bernoulli's theorem that " father of hydrodynamics " Denier Bernoulli Jacob (Daniel Bernoulli) proposes (Bernoulli's principle), is stated with Bernoulli equation：

(p is the pressure suffered by fluid in formula, and v is flowing velocity, and ρ is fluid density, and g is acceleration of gravity, and h is the point Place is highly)

I.e. in a fluid system, such as air-flow, current, flow velocity is faster, and the pressure that fluid is produced is just smaller, substantially Fluid density reduces simultaneously.

This is related to, briefly benefit is done to the first secondary secondary ramjet of ramjet 31, second and the 3rd secondary ramjet 44 Fill：

Ith, on the first secondary ramjet 31

As described above when the first secondary ramjet spout 39 is oblique against motion carrier head in certain distance, certain angle scope 32 surroundings spray high velocity air 24, and a cone-shaped low-pressure area 40 is formed in the front of motion carrier head 32, and it is to motion carrier Head 32 is the first secondary ramjet 31 of the profile 43 with raindrop shape without very resistance, now motion carrier forefront.According to The formula of air drag：

(C is coefficient of air resistance in formula, and ρ is atmospheric density, and S object front face areas, V is the relative fortune of object and air Dynamic speed)

The first of profile 43 of the analysis with raindrop shape the secondary ramjet 31 meets air drag accordingly：1. air drag system Number (drag coefficient), also known as air resistance coefficient, its size is relevant with the shape of object, and the shape of raindrop shape belongs to wind Resistance coefficient reckling；2. the front face area of first of the profile 43 with raindrop shape the secondary ramjet 31 may diminish to only move / the tens of the front face area of carrier header 32 even more than one percent；3. air drag and moving object are operationally before it The air in face is subject to the elastic force of air related by compression, and after there is the first secondary ramjet 31 of the profile 43 of raindrop shape The outer surface of cone-shaped low-pressure area 40 is that conical side surface is the high velocity air 24 sprayed from the first secondary ramjet 31, flow velocity pole The movement velocity of height, typically much higher than motion carrier, not only will not be to the air in the first of raindrop shape the secondary front of ramjet 31 It has been compressed that, the air that front along band " pullling " has been flowed into rear therewith on the contrary, atmospheric density has declined, and is conducive to motion carrier Move ahead.

Known, motion carrier moves square being directly proportional for the air drag that is subject to and speed in atmosphere；Have been reported that speed Be directly proportional for the cube to speed by air drag when reaching 400~600 meter per second, the air drag in the case where speed is higher Can be directly proportional to the power high of speed.So how to be dropped for aerospace (before the atmosphere that flies out) aircraft of increasingly high speed Low-drag is a problem that can not ignore, and considers have especially on high-speed aircraft and rocket using the first secondary ramjet 31 Meaning.

IIth, on the second secondary ramjet

When object relative motion on the surface of another object, the power of the obstruction relative motion being subject to is cunning Kinetic force of friction, force of sliding friction heel pressure is directly proportional, that is, with an object to the vertical of another body surface It is directly proportional.Specifically, when submarine in the seawater relative to seawater movement when, submarine kayak body surface can be granted by seawater The force of sliding friction of its relative motion, this force of sliding friction is hindered to be directly proportional with the pressure of seawater, that is, with seawater to latent The normal pressure on ship kayak body surface is directly proportional.Can be with force of sliding friction formulae express：

F=μ F_N

(wherein：F is force of sliding friction, F_NIt is normal pressure, μ is dynamic friction factor)

Therefore when the second secondary ramjet spout is quite closely leaned on, rearward sprayed parallel to submarine (not shown) kayak body surface Penetrate high velocity air, high velocity air covering submarine body surface, flow velocity is big and small to submarine body surface normal pressure, and can dispel, rolling off it is tight The seawater of submarine kayak body is pasted, one layer of low-pressure air layer is formed around submarine kayak body, when being run forward so as to reduce the submarine With the sliding-frictional resistance of surrounding seawater；And these described second secondary ramjets rearward gas injection is travelled to submarine Grant certain thrust.

IIIth, on the 3rd secondary ramjet (44)

The seventies in last century, the U.S. and the former Soviet Union successively respectively release a kind of aircraft with wing engine, are respectively real The Boeing YC-14 (being cancelled for various reasons) and amp- 72 (А of the property tested_HTOHOвА_H- 72), the jet flow of their engines is straight The upper surface for brushing wing is connect, accelerates upper surface of the airfoil air-flow, increase lift, to realize STOL.This technology is (below It is referred to as А_H- 72 technologies) distinguishing feature is as follows compared with the of the present invention 3rd secondary ramjet 44：

①А_H- 72 engines (belong to internal combustion engine) with the combustion gas that fuel combustion is produced as power, the secondary jet of the present invention the 3rd Engine 44 (belongs to " without combustion engine ") with compressed air as power；

②А_HThe high-temperature fuel gas of -72 engine spray can cause the hot tired of a certain degree of ablation of aerofoil surface and structure Labor (, cost too high to wing material requirements is too expensive), secondary ramjet (44) jet-stream wind of the present invention the 3rd does not result in body Ablation is damaged；

③А_H- 72 engines are arranged on wing top, before the secondary ramjet 44 of the present invention the 3rd is arranged on the leading edge of a wing Side；

④А_HEffect of -72 engines to airfoil lift is primarily generated at upper surface of the airfoil, and the secondary jet of the present invention the 3rd is drawn Hold up 44 pairs of airfoil lift effects and be not only in that upper surface of the airfoil also acts on the wing lower surface with certain angle of attack, efficiency is more It is high；

⑤А_H- 72 wing engine that is, aircraft main engine needs continuous firing (when cruise does not need lift-rising Can not shut down and its combustion gas is persistently blown in upper surface of the airfoil), the secondary ramjet 44 of the present invention the 3rd only when lift-rising is needed in short-term Work (aircraft separately has main engine)；

⑥А_H- 72 voyages are limited (maximum commercial transport voyage 800km), and the secondary ramjet (44) of the present invention the 3rd is in usual feelings (aircraft separately has main engine) unrelated with voyage under condition；

⑦А_H" the gas velocity machine speed ratio " of -72 aircrafts generally continues in a metastable numerical value, with of the invention the " the gas velocity machine speed ratio " of the aircraft of three secondary ramjets 44 can raise that (the 3rd pair ramjet 44 works when taking off, land When), other times are as usual.

The present embodiment describes a kind of operation method with system that compressed air is force source, comprises the following steps：

Step one：Pressurization inflation is carried out to large-sized boiler formula pressure vessel 49 by high-voltage and ultra-high air compressor 50；

Header inlet valve 67, whole Large Copacity tubular container inlet valves 78 and outlet valve 79 are opened in this course Open, and manifold outlet ports valve 70 is closed；

Motor 51 is difficult the power supply of storage using night dip electric energy or wind-powered electricity generation, solar energy etc., by high-voltage and ultra-high Air compressor 50 enters through air compressor exhaust port 52, header inlet 66 and its valve 67 opened, whole Large Copacity tubular containers Mouth 76 and its valve 78 opened and whole Large Copacity tubular containers outlet 77 and its valve 79 opened are large-scale to being arranged at Arrival end collector 65, whole Large Copacity tubular containers 60 and the pressurization inflation of port of export collector 68 in flowing water tank 54；

The air pressure and tolerance of the gas that controller control is filled with from air compressor exhaust port 52 are adapted to from large-scale circulating water water Cooling water 58 and the water-carrying capacity of the hot water 59 of the outflow of delivery port 56 that 54 water inlet of case 55 is flowed into, make in arrival end collector 65, entirely Occurred together in compressed air production process in portion Large Copacity tubular container 60 and port of export collector 68 generation heat it is cold in time But water 58 is taken away, and the hot water 59 that cooling water 58 is heated to be proper temperature leads to direct buried insulation from the outflow of delivery port 56 in good time Pipe 57 is used for central heating, until in arrival end collector 65, whole Large Copacity tubular containers 60 and port of export collector 68 still So basic a large amount of compressed airs that the temperature remains within the normal range reach design high pressure, store for future use；

Header inlet valve 67, whole Large Copacity tubular container inlet valves 78 and outlet valve 79 are closed when the time comes, collector Outlet valve 70 continues to close；

Step 2：Inflated to gas tank 9 by large-sized boiler formula pressure vessel 49；

Header inlet valve 67 and whole Large Copacity tubular container inlet valves 78 are closed in this course, all big Only single difference is opened in order in capacity tubulose container outlet valve 79 and remaining is closed, and manifold outlet ports valve 70 is opened；Collector Outlet 69 is docked with what cylinder 1 in gas tank 9 was shared by tracheae 3, and 1 intake valve of cylinder 5 is single in gas tank 9 opens in order respectively Open and remaining closing；The outlet valve 79 that controller control compressed air is opened from some Large Copacity tubular container 60 in an orderly manner What cylinder 1 was shared in manifold outlet ports valve 70, manifold outlet ports 69, the gas tank 9 through opening is stored up by tracheae 3 and some unlatching Tracheae intake valve 5 is filled with compressed air to the cylinder 1 ... such as, and compressed air is input into gas storage from Large Copacity tubular container first 62 Pipe first 10, the intake valve 5 of cylinder first 10 is closed when in cylinder first 10 full of the compressed air for reaching design requirement pressure, so The intake valve 5 of cylinder second 11 is opened afterwards, and compressed air is input into cylinder second 11 from Large Copacity tubular container first 62 ...

Air pressure is gradually reduced during a Large Copacity tubular container 60 is inflated to cylinder 1 one by one, so that after When being inflated to certain cylinder 1 to take turns in the Large Copacity tubular container 60 air pressure have dropped to in the cylinder 1 being bullied The air pressure for gradually increasing is equal, and at this moment the Large Copacity tubular container 60 is powerless is further continued for the gas storage to the gas transmission of the cylinder 1 Air pressure is not yet raised to design requirement in pipe 1, and such as such case occurs in Large Copacity tubular container first 62 to cylinder the third 12 During gas transmission, both air pressure one drop one liter when reaching equal, and air pressure is not yet raised to design requirement and great Rong in cylinder the third 12 Air pressure has dropped to the powerless cylinder the third 12 for being further continued for being increased to certain value to air pressure of certain value in amount tubular container first 62 Continue gas transmission, the intake valve 5 of at this moment controller control cylinder the third 12 is closed, and the intake valve 5 of cylinder fourth 13, the 13a of cylinder penta enter The single orderly opening and closing in succession of the grade of air valve 5, make the air pressure also compression with certain overbottom pressure in Large Copacity tubular container first 62 Air is emptied to the relatively low cylinder fourth 13 of air pressure, the 13a ... of cylinder penta and then Large Copacity tubular container first 62 and goes out successively Mouthful valve 79 is closed, and the outlet valve 79 of Large Copacity tubular container second 63 is opened, while the intake valve 5 of cylinder the third 12 is again turned on, Make to have the Large Copacity tubular container second 63 of " original " high pressure makes to the inflation of the relatively low cylinder of pressure in contrast the third 12 The air pressure that certain value is had been raised to before in it continues rising and reaches design requirement, and then the intake valve 5 of cylinder the third 12 is closed, tightly Then the intake valve 5 of cylinder fourth 13 is opened ...

Wherein, it is empty for the internal memory of cylinder 1 in compressed air from during the input cylinder 1 of Large Copacity tubular container 60 Pressure has certain intensification trend in rising for gas, but for being input in cylinder 1 from Large Copacity tubular container 60 This Partial shrinkage air for its pressure decline and have cooling trend, controller controls compressed air from Large Copacity tubulose Container 60 is input into flow, the speed of cylinder 1, make air pressure in cylinder 1 in this course be increased to design requirement steadily and Intensification trend and cooling trend relative equilibrium, temperature are basicly stable；

Step 3：Gas tank 9 is supplied gas to ramjet 16；

In the course of work of ramjet 16, the intake valve 5 of all cylinders 1 is closed in gas tank 9, each cylinder 1 in gas tank 9 Air bleeding valve 6 is single or several difference are opened in order and remaining is closed；Controller control compressed air is a certain therefrom in an orderly manner Air bleeding valve 6 that individual or several cylinders 1 are opened, appendix 8 send into connected air inlet pipe 17, and then swollen via being arranged on The mouth 25, gas of emanating in swollen chamber-head portion 27 injects adjuster 26 and injects expanding chamber 18；

The caliber of air inlet pipe 17 is smaller compared with the caliber of cylinder 1, air inlet pipe week electric heater 29 and expanding chamber locular wall heater 30 Work, the compressed air into expanding chamber 18 is flowed into and the end of expanding chamber 18 under high pressure by appropriate heating, holding elevated pressures The De Laval noz(zle) tapered portion 20 that end is connected as a single entity-through De Laval noz(zle) throat 21-by De Laval noz(zle), gradually wealthy portion 22 sprays Go out, air-flow greatly accelerates, produce huge thrust, high velocity air 24 also involves the change of corresponding local air force.

The above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art For member, on the premise of the technology of the present invention principle is not departed from, some improvement and replacement can also be made, these improve and replace Also should be regarded as protection scope of the present invention.

Claims

1. a kind of with system that compressed air is force source, it is characterised in that including with high-voltage and ultra-high compressed air be injection The compressed air ramjet (14) of working medium, compressed air is produced for device (48) and controller；

The compressed air ramjet (14) is arranged on motion carrier；The compressed air ramjet (14) is including gas tank And ramjet (16) (9)；The gas tank (9) is compressed-air-storing container, including multiple cylinders (1), the cylinder (1) for laying in and supplying the ramjet (16) needed for compressed air；The ramjet (16) is drawn including main jet gas Hold up (41) and multiple pair ramjets；The main ramjet (41) is for the compressed air to be input into from the cylinder (1) It is injection working medium, the thrust for travelling forward is granted to the motion carrier；Multiple secondary ramjets include being separately positioned on The first secondary ramjet (31), the second secondary ramjet (42), the 3rd secondary ramjet (44) around the motion carrier, Fourth officer ramjet (46) and the 5th secondary ramjet (47), for being with the compressed air being input into from the cylinder (1) Injection working medium simultaneously forms the push on target direction to the motion carrier by coordinating with the main ramjet (41)；

The compressed air is produced includes high-voltage and ultra-high air compressor (50) and large-sized boiler formula pressure vessel for device (48) (49)；The operating pressure of the high-voltage and ultra-high air compressor (50) is close, 100Mpa is equaled or exceeded, in the control Pressurizeed to the large-sized boiler formula pressure vessel (49) under the control of device processed and inflated；The large-sized boiler formula pressure vessel (49) is used In production and storing compressed air, multiple cylinder (1) pressurizations are inflated with the control of the controller；

The controller is used for by the main ramjet (41), the first secondary ramjet (31), the second secondary ramjet (42), the open and close controlling of the 3rd secondary ramjet (44), fourth officer ramjet (46) and the 5th pair ramjet (47) and it is right The motion carrier forms the push of target direction.

2. it is according to claim 1 with system that compressed air is force source, it is characterised in that the main ramjet (41), the first secondary ramjet (31), the second secondary ramjet (42), the 3rd secondary ramjet (44), fourth officer ramjet (46) and the 5th secondary ramjet (47) include being made up of high pressure resistant, lighter material air inlet pipe (17), expanding chamber (18) and De Laval noz(zle) (19)；

The air inlet pipe (17) is connected between the cylinder (1) and the expanding chamber (18)；The week of the air inlet pipe (17) Enclose and be provided with air inlet pipe week electric heater (29), air inlet pipe week electric heater (29) is for heating in the air inlet pipe (17) Compressed air, so that the air pressure in the air inlet pipe (17) is raised；Compressed air in the cylinder (1) is by the air inlet The mouth of emanating (25) for managing (17) is injected in the expanding chamber (18)；

The expanding chamber locular wall (28) of the expanding chamber (18) injects adjuster (26) equipped with gas, and the gas injects adjuster (26) setting pressure to the amount of the compressed air in the expanding chamber (18) is injected for regulating and controlling the air inlet pipe (17), so that institute The air pressure stated in expanding chamber (18) maintains setting pressure；Expanding chamber locular wall electric heater is provided with around the expanding chamber (18) (30), the expanding chamber locular wall electric heater (30) adds for being heated the compressed air into the expanding chamber (18) Pressure；

The sectional area of the De Laval noz(zle) (19) first diminishes become big again from front to back；The end of the expanding chamber (18) with it is described The tapered portion (20) of De Laval noz(zle) is connected as a single entity, and expanding chamber (18) compressed air accelerates by the drawing under stress Cut down that jet pipe tapered portion (20), De Laval noz(zle) throat (21) and De Laval noz(zle) gradually wealthy portion (22), final high velocity air (24) Sprayed by De Laval noz(zle) spout (23).

3. it is according to claim 2 with system that compressed air is force source, it is characterised in that the described first secondary jet is drawn Hold up the front that (31) are arranged on the head (32) of motion carrier；The front face area of the described first secondary ramjet (31) is less than corresponding The motion carrier head (32) front face area；The first secondary ramjet (31) includes the first air inlet pipe (17a), the One expanding chamber (18a) and the first De Laval noz(zle) (19a), also including a firm tubular structure (33), the described first secondary jet Engine (31) is fixed on the front of the motion carrier head (32) by the firm tubular structure (33)；First air inlet pipe (17a) is located within the firm tubular structure (33) and is supported by the firm tubular structure (33)；First expansion The end of room (18a) is connected as a single entity with the tapered portion (20a) of the first De Laval noz(zle)；First De Laval noz(zle) (19a) by A-P is in integrally Rafael nozzle shape structure；First air inlet pipe (17a) is together with the firm tubular structure (33) from fortune The head (32) of dynamic load body stretches out forwards, and axially sequentially passes through first in center to the described in forward position first secondary ramjet (31) Secondary ramjet spout (39), the first De Laval noz(zle) gradually wealthy portion (22a), the first De Laval noz(zle) throat (21a), described first De Laval noz(zle) tapered portion (20a) and first expanding chamber (18a) and with the expanding chamber head of first expanding chamber (18a) Inwall (37) is fixedly connected；The expanding chamber head inwall (37) equipped with the first air inlet pipe emanate mouth and gas injects adjuster (35)；First expanding chamber (18a) compressed air accelerates by the first De Laval noz(zle) tapered portion under stress (20a), the first De Laval noz(zle) throat (21a), finally by positioned at first De Laval noz(zle) gradually wealthy portion (22a) with it is firm Gap between the conical huge portion (33a) of tubular structure rearward along week from a conical side surface to motion carrier head Injection is enclosed, the bus of the conical side surface is equivalent to from the first De Laval noz(zle) throat (21a) to the motion carrier head (32) line (32a) of periphery, forms a cone-shaped low-pressure area (40), for dropping with the motion carrier head (32) front Air drag or seawater resistance that the low motion carrier runs forward；

Described first secondary ramjet (31) is additionally operable to grant the tractive force that the motion carrier travels forward.

4. it is according to claim 3 with system that compressed air is force source, it is characterised in that the described second secondary jet is drawn It is multiple to hold up the quantity of (42), multiple described second secondary ramjet (42) circumferentially disposed the week side of boss in the motion carrier, many Individual described second secondary ramjet (42) spout sprays high velocity air to the motion carrier towards the rear of the motion carrier Travel forward and grant thrust, and the high velocity air that ejects of described second secondary ramjet (42) spout is parallel and close to fortune The surface of dynamic load body, reduced with forming one layer of low-pressure air layer around motion carrier when motion carrier runs forward with it is outer Sliding-frictional resistance between boundary.

5. it is according to claim 1 with system that compressed air is force source, it is characterised in that to be set on the motion carrier There are one or more described gas tanks (9), the multiple described cylinder (1) in each described gas tank (9) is long tubular structure, have There is cylindrical shape gas storage tube wall (2) being made up of high pressure resistant, lighter material；

Multiple parallel bunchy arrangements of the cylinder (1), and cross section is that entirety is in plum blossom-shaped structure；Each described cylinder (1) intake valve (5) and air bleeding valve (6) individually opened and closed by controller control are equipped with；

Standby electric heater (15) is provided with around the cylinder (1), the standby electric heater (15) is in the pressure Under contracting aerojet engine (14) works overloadingly for some reason, all cylinder (1) the compressed air pressure is below setting Start in limited time；

One end of multiple cylinders (1) many siphunculus (4) of being bullied with are connected, many siphunculus (4) of being bullied converge for One is received tracheae (3)；The other end of multiple cylinders (1) is communicated with many siphunculus of a gas transmission (7), and the gas transmission is led to more It is an appendix (8) that multiple paths of pipe (7) converge；The cylinder (1) is by the appendix (8) and the air inlet pipe (17) connect；

The compressed air being filled with for receiving to be pressurizeed from the large-sized boiler formula pressure vessel (49) by tracheae (3).

6. it is according to claim 1 with system that compressed air is force source, it is characterised in that to be the gas tank (9) Cylinder (1) pressurization inflation the large-sized boiler formula pressure vessel (49) including large-scale flowing water tank (54) and several put Large Copacity tubular container (60) and collector (53) in the water tank；

Several described Large Copacity tubular containers (60) are divided into the comb (74) of multigroup tiling shape, and the collector (53) is positioned at every group The both sides of the comb (74) of tiling shape, entrance is provided with Large Copacity tubular container (60) two ends of the comb (74) shape (76) and outlet (77), the collector (53) connected with Large Copacity tubular container entrance (76) in every group is arrival end collector (65) collector (53) for, being connected with Large Copacity tubular container outlet (77) in every group is port of export collector (68)；It is described The entrance (76) of Large Copacity tubular container (60) is provided with inlet valve (78), the outlet (77) of the Large Copacity tubular container (60) It is provided with outlet valve (79)；The arrival end collector (65) is provided with a header inlet (66) and its header inlet valve (67), The port of export collector (68) is provided with a manifold outlet ports (69) and its manifold outlet ports valve (70)；

The design volume and pressure of the Large Copacity tubular container (60) are respectively greater than and hold higher than the design of the cylinder (1) Product and pressure；The part Large Copacity tubular container (60) is coiled pipe (75), and the coiled pipe (75) is in the comb (74) tiling plane in repeatedly roundabout extension tubular structure；

The comb (74) being laid in approximately the same plane and its arrival end collector (65) on both sides and port of export collector (68) Large Copacity tubular container plane (73) is constituted；It is provided with described in multiple in a large-scale flowing water tank (54) Large Copacity tubular container plane (73), the arrival end collector (65) in multigroup Large Copacity tubular container plane (73) pass through into Mouth end header in communication pipe (71) connection, and a header inlet (66) is shared, the header inlet (66) is interior to be provided with collector Inlet valve (67)；Port of export collector (68) in each Large Copacity tubular container plane (73) is by port of export header in communication Pipe (72) connection, and a manifold outlet ports (69) is shared, the manifold outlet ports (69) are interior to be provided with manifold outlet ports valve (70)；

The large-scale flowing water tank (54) is provided with water inlet (55) for flowing into cooling water (58) and for flowing out hot water (59) delivery port (56), the delivery port (56) connects with the direct buried insulating tube (57) in central heating system；

The air compressor exhaust port (52) of the high-voltage and ultra-high air compressor (50) detachably connects with the header inlet (66) Connect, inflated for being pressurizeed to the Large Copacity tubular container (60).

7. a kind of aircraft, it is characterised in that including with compressed air being force source as described in any one of claim 1 to 6 System, wherein the described first secondary ramjet (31) is arranged on plane nose front, the described second secondary ramjet (42) is set In the week side of boss of airframe；And the quantity of the 3rd pair ramjet (44) is multiple, multiple described 3rd secondary jets are drawn Hold up the front that (44) are symmetricly set on the leading edge of aircraft both sides wing；The spout of the 3rd secondary ramjet (44) is rearward Wing sprays high velocity air (24), and the direction of high velocity air ejected of spout of the 3rd secondary ramjet (44) with Take off consistent relative to the airflow direction of wing during sliding race；Described 3rd secondary ramjet (44) is in aircraft short distance Or airfoil lift is improved during VTOL, it is additionally operable to grant anti-corresponding to the described 3rd secondary ramjet (44) spout gas injection The thrust travelled forward to the aircraft that active force is made a concerted effort.

8. aircraft according to claim 7, it is characterised in that the fourth officer ramjet (46) is arranged on the aircraft The lower section of fuselage, for the back lower place to aircraft or front lower place jet-stream wind, with the aircraft granted forward upward or it is rear on The reaction force of side；Described 5th secondary ramjet (47) is arranged on immediately below the afterbody of the aircraft or is symmetricly set on afterbody Both sides, for the contrainjection high velocity air to the aircraft flight direction, to play the work of buffer deceleration to the aircraft With.

9. a kind of operation method with system that compressed air is force source, it is characterised in that comprise the following steps：

Step one：Pressurization inflation is carried out to large-sized boiler formula pressure vessel (49) by high-voltage and ultra-high air compressor (50)；

Header inlet valve (67), whole Large Copacity tubular container inlet valve (78) and outlet valve (79) in this course Open, and manifold outlet ports valve (70) is closed；

Motor (51) utilizes night dip electric energy or wind-powered electricity generation, solar energy, by high-voltage and ultra-high air compressor (50) through sky Press exhaust outlet (52), header inlet (66) and its header inlet valve (67) opened, whole Large Copacity tubular container entrances And its inlet valve (78) opened and whole Large Copacity tubular container outlet (77) and its outlet valve opened (76) (79) to the arrival end collector (65) being arranged in large-scale flowing water tank (54), whole Large Copacity tubular container (60) and go out Mouth end collector (68) pressurization inflation；

The air pressure and tolerance of the gas that controller control is filled with from air compressor exhaust port (52) are adapted to from large-scale flowing water tank (54) water inlet (55) is flowed into cooling water (58) and the water-carrying capacity of the hot water (59) of delivery port (56) outflow, make in arrival end collection Pipe (65), whole Large Copacities tubular container (60) and the generation that occurred together in compressed air production process in port of export collector (68) Heat in time take away by cooled water (58), and cooling water (58) is heated to be the hot water (59) of proper temperature in good time from delivery port (56) Outflow leads to direct buried insulating tube (57) for central heating, until holding in arrival end collector (65), whole Large Copacity tubuloses Still basic a large amount of compressed airs that the temperature remains within the normal range reach design high pressure in device (60) and port of export collector (68), store standby With；

Header inlet valve (67), whole Large Copacity tubular containers inlet valve (78) and outlet valve (79) are closed when the time comes, collection Pipe outlet valve (70) continues to close；

Step 2：Inflated to gas tank (9) by large-sized boiler formula pressure vessel (49)；

Header inlet valve (67) and whole Large Copacity tubular containers inlet valve (78) are closed in this course, all big Only single difference is opened in order in capacity tubulose container outlet valve (79) and remaining is closed, and manifold outlet ports valve (70) is opened； Manifold outlet ports (69) are docked with what cylinder (1) in gas tank (9) was shared by tracheae (3), each cylinder (1) air inlet in gas tank (9) Valve (5) only open and remaining closing in order by single difference；Controller controls compressed air in an orderly manner from some Large Copacity tubulose Gas storage in manifold outlet ports valve (70), manifold outlet ports (69), gas tank (9) of the outlet valve (79) that container (60) is opened through opening What pipe (1) was shared is filled with compressed air by tracheae (3) and some cylinder intake valve (5) opened to the cylinder (1)；

Air pressure is gradually reduced during a Large Copacity tubular container (60) is inflated to cylinder one by one (1), so that after Large Copacity tubular container (60) the interior air pressure has dropped to and the cylinder being bullied when being inflated to certain cylinder (1) to take turns to (1) air pressure gradually increased in is equal, and at this moment the Large Copacity tubular container (60) is powerless is further continued for the cylinder (1) gas transmission And cylinder (1) the interior air pressure is not yet raised to design requirement, controller control major capacity tubulose container outlet valves (79) and The opening and closing of each cylinder (1) intake valve (5), makes the Large Copacity tubular container (60) that air pressure has declined to not yet inflation or presses Power low cylinder (1) inflation relatively, although making to have risen the gas storage for being not yet raised to design requirement by the blowing pressure Pipe (1) obtains the Large Copacity tubular container (60) with initial high pressure or relatively high pressure and is inflated to it；

Wherein, it is input into during cylinder (1) from Large Copacity tubular container (60) in compressed air, for cylinder (1) internal memory Pressure has certain intensification trend in rising for air, but for being input to cylinder from Large Copacity tubular container (60) (1) its pressure declines and has cooling trend for this Partial shrinkage air in, and controller controls compressed air from great Rong Flow, the speed of amount tubular container (60) input cylinder (1), make cylinder (1) interior air pressure in this course raise steadily Intensification trend and cooling trend relative equilibrium to design requirement, temperature are basicly stable；

Step 3：Gas tank (9) is supplied gas to ramjet (16)；

In ramjet (16) course of work, all cylinders (1) intake valve (5) are closed in gas tank (9), each in gas tank (9) Cylinder (1) air bleeding valve (6) only single or several difference are opened in order and remaining is closed；Controller control compressed air is in an orderly manner Some or several cylinders (1) are opened therefrom air bleeding valve (6), appendix (8) send into connected air inlet pipe (17), and then via being arranged on the mouth of emanating (25) of expanding chamber head (27), gas and injecting adjuster (26) expanding chamber is injected (18)；

Air inlet pipe (17) caliber is smaller compared with cylinder (1) caliber, air inlet pipe week electric heater (29) and expanding chamber locular wall electrical heating Device (30) is worked, and the compressed air into expanding chamber (18) is flowed into successively under high pressure by appropriate heating, holding elevated pressures The De Laval noz(zle) tapered portion (20) that is connected as a single entity with expanding chamber (18) end, through De Laval noz(zle) throat (21) and by drawing Gradually wealthy portion (22) sprays to cut down your jet pipe, and air-flow greatly accelerates, and produces huge thrust, and it is empty that high velocity air (24) also involves corresponding local Changes in aerodynamic forces.