CN106741938A

CN106741938A - The linear hypersonic speed of stray bullet flies hole passenger plane

Info

Publication number: CN106741938A
Application number: CN201710088001.XA
Authority: CN
Inventors: 鲁正祥
Original assignee: Individual
Current assignee: Individual
Priority date: 2016-05-11
Filing date: 2017-02-19
Publication date: 2017-05-31
Also published as: CN105775129A

Abstract

Fly hole passenger plane (solely flying airliner) the present invention relates to a kind of hypersonic speed, it is characterized in that be provided with a frame in the straight close-fitting winged hole of an elongated tubular product level solely flies passenger plane (solely flying airliner) by burning hot taper head, the snakelike fuselage of overlength, afterbody direct-injection rocket, the whole body imitative machine of thousand cabin of body, thousand people one of the strip that tiltedly flame arrow is constituted, the passenger plane is stamped into hole by means of " velocity of sound ejection ", and the direct-injection and oblique flame arrow are just lighted a fire when velocity of sound enters hole；Steadily accelerate by means of " ten inner ejections "；Wall is not touched by means of " hole bullet punching press " bullet；Flown over by means of " breakthrough sound barrier " seamless；Hole wall is not burnt by means of " velocity of sound flame "；" light hole preheating " is borrowed to drive air away；By means of " vexed tank rocket " ten times of velocities of sound；By means of " close-fitting air bag " forced position；Clinostatism is forced by means of " half meter thin hole "；Racing is offset by means of " balance nozzle "；The present invention is " ten minutes airliners " (the short hole supersonic speed in hole long, hundred inner a thousand lis ten minutes).

Description

The linear hypersonic speed of stray bullet flies hole passenger plane

Technical field

Fly hole passenger plane (solely flying airliner) the present invention relates to a kind of hypersonic speed, it is characterized in that in an elongated tubular product level pen Tiltedly flame arrow is constituted by burning hot taper head, the snakelike fuselage of overlength, afterbody direct-injection rocket, the whole body to be provided with a frame in straight close-fitting winged hole The imitative machine of thousand cabin of body, thousand people one of strip solely fly passenger plane (solely flying airliner), the passenger plane is stamped into hole by means of " velocity of sound ejection ", and this is straight The just igniting when velocity of sound enters hole of spray and tiltedly flame arrow；Steadily accelerate by means of " ten inner ejections "；Wall is not touched by means of " hole bullet punching press " bullet；Borrow " breakthrough sound barrier " flies over seamless；Hole wall is not burnt by means of " velocity of sound flame "；" light hole preheating " is borrowed to drive air away；By means of ten times of " vexed tank rocket " Velocity of sound；By means of " close-fitting air bag " forced position；Clinostatism is forced by means of " half meter thin hole "；Racing is offset by means of " balance nozzle "；The present invention is " ten minutes airliners " (the short hole supersonic speed in hole long, hundred inner a thousand lis ten minutes).

Background technology

Existing gas hole is big because of air drag, it is impossible to travel hypersonic speed driving or hypersonic plane (therefore, might as well be by visitor Machine head is just designed to thousand degree of high temperature " burning hot head " since the zero-speed start of a race or the velocity of sound start of a race, so as to rarefied air, neutralizing resistance Power).Existing trunk driving or trunk aircraft have been wheel or have had the wing, and it is linear to have impact on stray bullet, increased passenger plane deadweight, are only beneficial to Low-speed operations are unfavorable for hypersonic flight (hypersonic vehicle all should be designed to " without wheel without the wing " and " stray bullet is linear ").It is existing Have supersonic speed trunk passenger plane before hole is entered using " velocity of sound ejection " (such as " flywheel ejection " or " electromagnetic launch " or other Ejection) (" flywheel ejection " refer to by be arranged in straight up to several kilometers even more than ten kilometers style of opening passages on up and down Four thousands of of side even tens thousand of relays drive flywheel or " roadside flywheel " to provide machine outer power, will be without wheel without the wing thousand Velocity of sound is arrived in the quick speed-raising before hole is entered of the rice burning hot head zero-speed passenger plane of the snakelike figure of fuselage, and is launched into hole with velocity of sound).It is existing " vacuum trunk Concord " is not to open trunk using normal pressure, it is impossible to solves trunk facility, trunk material, trunk gate and resists The anti-negative pressure problem of vacuum (in other words, realizes that vacuum is difficult, maintains vacuum to be more difficult to；In other words, it is difficult in vacuum trunk with it Supersonic speed is realized, supersonic speed is realized not as being forced in normal pressure opening trunk；In other words, it is real in vacuum trunk not as abandoning Show hypersonic speed but directly realize hypersonic speed in atmospheric gas hole；In other words, should be using a kind of completely newly winged hole scheme, should Winged hole is that vacuum trunk does not influence hypersonic speed；In other words, " hypersonic speed flies hole " both can be that " rarefied air flies Hole " can also be " denser air flies hole ").Dense gas in narrow trunk is external " winged in the supersonic speed for running into unexpected visiting Play passenger plane " when can only be squeezed in the narrow gap of body surrounding formation " hole bullet punching press " (especially " head because having little time diffusion Punching press ") (as long as " passenger plane is launched into hole with velocity of sound ", is just bound to be formed " hole bullet punching press " and " head punching press "), as One floor height is calmed the anger pad, by force separates body with cartridge chamber, " bullet does not touch wall " is realized, so as to eliminate hard thing between body and cartridge chamber rub Wipe (only gas current friction), both protected cartridge chamber or protected body not by hard thing scratch (and greatly reducing frictional resistance).It is existing It is not " stray bullet is linear " (not being that low drag profile is designed) to have supersonic speed manned vehicle in trunk, it is impossible to simulates and " plays shape to fly OK " or " cartridge chamber flight ", thus can not as bullet small space " forcing flight ", be more unable to reach more than ten times it is superb Velocity of sound；All simply a unit, both cannot be by " overlength group machine " rather than one group of unit for existing rocket aircraft or rocket driving Improve single order of classes or grades at school freight volume；More cannot by the powerful inertia quality of " overweight group of machine " eliminate human body speed change pressure (because The too light inertia of unit quality is too small, and the inertia of can all cause slightly had an effect changes, although fuselage car body is can stood, but people body Can't stand；In other words, during unit flight, human body speed change pressure is too big, and during group machine flight, human body speed change pressure is just small；Change sentence Talk about, existing ten times of unmanned opportunities of combat of velocity of sound cannot turn into ten times of velocity of sound someone's opportunities of combat, cannot more turn into ten times of velocity of sound passenger planes；It is existing Why ten times of Sonic Wings Limiteds cannot turn into ten times of velocity of sound passenger planes, because ten times of Sonic Wings Limiteds nobody can only fly in open space OK, it is impossible to manned in closed trunk, therefore, having ten times of unmanned opportunities of combat of velocity of sound to be not equal to has had ten times of velocity of sound passenger planes)；It is existing It is not " only one of which order of classes or grades at school within a hole " (such as " solely fly airliner ") to have trunk driving or trunk aircraft, but " hole it It is interior including multiple order of classes or grades at school " (such as " with flying airliner "), therefore previous order of classes or grades at school occur that dangerous situation is next cannot hedging；Existing trunk Why driving or trunk aircraft are unable to reach supersonic speed, because front and rear " and then winged aircraft " or the front and rear " car for and then running " it is too many so that have little time between vehicle or between aircraft moment scheduling (therefore, " one minute airliner " is due to having little time scheduling So nonsensical, " ten minutes airliners " need not be dispatched or have grace time to dispatch so meaningful；In other words, " one point Clock airliner " reaction even if passenger plane is able to do in time, passenger also has little time reaction, it is easy to missed boarding；In other words, " ten minutes classes Not only passenger plane has enough time to react machine ", and passenger also has enough time to react).On existing thousands of kilometers of course lines or on high ferro circuit it So be all multimachine with flying or many cars are with running (rather than " machine solely flies " " car solely runs "), because can not find one kind very The aircraft or train that can be just finished the full distance in clock (cannot such as find a kind of " ten times of velocities of sound solely fly airliner "；Such as previous visitor Machine flies the whole process that is over, and next passenger plane just allows then to fly, and only has a frame passenger plane flying on whole circuit all the time, so that passenger plane is adjusted Degree get up it is extremely simple even without scheduling i.e. " acyclic homologically trioial degree ").It is " flat that existing " hang down jump fire arrow " why fltting speed can not show a candle to Jump fire arrow " because " hang down to jump fire arrow " most thrust be used for gravity consume rather than for vertical displacement (only by " flat Rocket thrust almost all could be used for horizontal displacement by jump fire arrow ", without comprehending vertical gravity；Dissolving vertical gravity can Winged thing is separated by force with hole wall with by " hole bullet punching press ", and the gravity for often saving single-berth cabin can not possibly be too big, especially ten times Velocity of sound single-berth cabin)；Existing passenger plane be not single-berth cabin longitudinally layout but system between cabin landscape layout, only by " cabin fatter body between system " " the thin fuselage of single-berth cabin " (such as " snakelike fuselage ") is changed to, " hole bullet punching press " could can be also borrowed in the case where wing is not set by visitor The thin fuselage of machine is gently lifted, and is realized " bullet does not touch wall ".Rocket is mostly " be at a stop igniting " rather than " point on the run in existing trunk Easily there is blast and (only " light a fire on the run " or even " sound in fire " (being less " velocity of sound igniting "), the igniting that is at a stop in narrow trunk Speed igniting " just can guarantee that and be perfectly safe).Why existing hypersonic speed opportunity of combat and hypersonic speed passenger plane easily disintegrate, be because Do not set circular fuselage only to set circular head, easily produce " non-annularity, it is non-embrace, it is non-parcel, asymmetric " disorderly air-flow, nothing Method simulation " circular bullet " and " circular flies hole " such " ring-type embrace, symmetrically parcel " steady air flow (only by Steady air flow could be formed in " the linear passenger plane of stray bullet " and " straight close-fitting winged hole ", universal shake is prevented, prevents from disintegrating).It is existing Hypersonic speed passenger plane or hypersonic speed opportunity of combat be all " thin head " and " fatter body " (" thin head " cannot be protected " fatter body ") (the most thick portion part of " taper head " is preferably designed to " equally thin " with the most thick portion part of " overlength fuselage ", a sharpening is similar to Thin pencil afterwards).Existing hypersonic speed opportunity of combat is often that head and windward side are easily disintegrated when sound barrier is broken through, and this points out me , it is necessary to head and windward side are designed to " firm resistance to burning is replaceable ".Existing trunk passenger plane is not up to several kilometers Overlength fuselage, design engineer takes for only ultrashort fuselage and can just obtain head protection (as long as passenger plane is with straight in fact Body makees that hypersonic speed is flat straight to fly in straight trunk, then, then fuselage long can also obtain the protection of head) (in other words Say, passenger plane once reaches hypersonic speed, it will be no longer fuselage but head to spell) (even " several meters of short heads " burns out, " thousand Rice fuselage long " also stands intact) (therefore, when passenger plane has flown full journey, even if to change " several meters of short heads " every time, also it is not required to " km fuselage long " is changed every time, flight cost is greatly reduced).Why little the trunk passenger plane of existing actual promotion and implementation is Using rocket propulsion, all because machine is easily influenceed by preceding tail gas, waste gas, parabolic, gurry after when multimachine is with flying, only using one Machine solely flies that this problem (at least providing cleaning in ten minutes) perfect could be solved, therefore, only " solely flying airliner " could use fire Arrow is advanced.Existing trunk passenger plane is not that sound barrier has just been broken through outside hole, it is impossible to the smooth flight in hole, it is impossible to experience " tranquil As before " or " flying over seamless " (this points out us, it is necessary to for zero-speed passenger plane provides " velocity of sound ejection " open channel outside hole, Just to be injected in trunk after first steadily accelerating to velocity of sound outside hole).

The content of the invention

The solution of the present invention is to be provided with a frame by burning hot taper machine in the straight close-fitting winged hole of an elongated tubular product level Head, the snakelike fuselage of overlength, afterbody direct-injection rocket, the whole body imitative machine of thousand cabin of body, thousand people one of the strip that tiltedly flame arrow is constituted solely fly visitor Machine (solely flies airliner), and the passenger plane is stamped into hole by means of " velocity of sound ejection ", and the direct-injection and oblique flame arrow are just lighted a fire when velocity of sound enters hole, should Passenger plane is " ten minutes airliners " (the short hole supersonic speed in hole long, hundred inner a thousand lis ten minutes)；Steadily accelerate by means of " ten inner ejections "；By means of " stream Snap the line type " is without wheel without the wing；Wall is not touched by means of " hole bullet punching press " bullet；By means of " body bullet speed " simulation fly bomb；Reduce by means of " taper head " and hinder Power；By means of " burning hot head " rarefied air；" light hole preheating " is borrowed to drive air away；Draw body with flying by means of " head punching press "；By means of " breakthrough sound Barrier " flies over seamless；Hole wall is not burnt by means of " velocity of sound flame "；Do not turn by means of " normotopia ejection " line silk；By means of " being launched outside hole " without hole resistance；Borrow " velocity of sound igniting " decompression explosion-proof；By means of " vexed tank rocket " ten times of velocities of sound；Most saved by means of " inertia is flown nonstop to " power consumption；Heat is robbed by means of " heat-insulated close cabin " Flight；" disposable shell " is borrowed to rob light flight；Fuselage is protected by means of " the resistance to burning of head "；Oxygen flight is robbed by means of " closed oxygen cabin "；By means of " end Water hole " terminal is forced and stopped；Land by means of " bottom wall pulley " is flexible；Match somebody with somebody close-fitting air bag by means of " cabin in roller "；Body is forced by means of " close-fitting air bag " Position；Clinostatism is forced by means of " half meter thin hole "；Racing is offset by means of " balance nozzle "；Heat wave is avoided by means of " head division "；By means of " airport point Flexibly go for a stroll in cabin "；By means of " oxygen-enriched winged hole " rocket detonation；Reclaimed by means of " arrow has flown " whole rocket；Got over by means of " the useless arrow of multistage " and leapt gently；Borrow " half way fuel " is flame-out continuous winged；Speed change pressure is kept away by means of " overlength passenger plane "；Falling bodies pressure is kept away by means of " zero meter of drop "；By means of " hypersonic speed " If ten minutes airliners；By means of the flight of " falling without parachuting " loss of weight；Replace rocket by means of " magnetcisuspension power "；It is dirty by means of " closed trunk " zero noise zero Dye；Solely fly by means of " people of thousand cabin thousand " machine；By means of " solely flying airliner " acyclic homologically trioial degree (ten minutes a time)；It is unmanned by means of " straight hole solely flies "； It is long-distance by means of " hole is moved in hundred cities " short change；Halve by means of " single line is returned " investment.

In scheme, unless otherwise specified, " the straight close-fitting winged hole of elongated tubular product level " can referred to as " winged hole " or " trunk "； " close-fitting vest winged hole " trunk bore very little and gap very little (ensuring " hole bullet punching press " the suitable premise between trunk and passenger plane Under, the gap left after a such as circular fuselage of " half rice diameter " is accommodated in circular trunk is can be small then small), it is " close-fitting Winged hole " effect has three, and one is smaller gap, can more form hole bullet punching press；Two is that trunk bore is smaller is more conducive to consumption minimum Cost maintains oxygen-enriched trunk；Three is that trunk bore is smaller can more save construction cost；Four is that trunk bore is smaller can more reduce machine Head windward side maximum, in a disguised form reduces resistance；Five is that the smaller trunk anti-pressure ability that can more improve of trunk bore (such as resists " hole Play punching press " or " head punching press ").In scheme, the external diameter of the internal diameter slightly larger than passenger plane cross section of " trunk " is (just as the internal diameter of gun barrel The external diameter of shell will not be far longer than)；" trunk " internal diameter (do not oppose more than one meter) preferably below one meter, just only accommodates one The circular cab body of individual horizontal single-berth cabin, and just it is slightly larger than existing minimum rocket size.In scheme, " the imitative body passenger plane of strip " (if scaled after) be somewhat like in shape one fine away after elongated pencil (but be definitely not straight stiff figure, and Can be the soft figure of bending, i.e., " snakelike figure ") (preferably by the most thick portion part of " taper head " with " overlength fuselage " most Thick portion part is designed to " equally thin ", is similar to the thin pencil after a sharpening), therefore, " imitative body passenger plane " is alternatively referred to as " imitative rocket body Passenger plane " or " imitative snake body passenger plane " or " fly bomb passenger plane " or " flying arrow passenger plane " (unless otherwise specified, all can referred to as " passenger plane "), Passenger plane " playing shape flight " is alternatively referred to as passenger plane " arrow-like flight " or similar " snake body Durchgangshohle ".In scheme, " the snakelike fuselage of overlength " is Although referring to that often section single-berth cabin is very hard very short (such as only two meters long), when hundreds of sections or thousands of section single-berth cabins are cascaded It is no longer stiff afterwards, can flexibly be bent as " snakelike figure " and (although flying to be bent in hole straight, always run into The micro- slope or micro-bend that cannot be overcome, or need to go for a stroll in airdrome control transition or when turning around temporarily).In scheme, " overlength is snakelike The cross section of fuselage " (or " thin circle fuselage ") and the cross section of " taper head " are preferably circular (just as bullet or big gun The cross section of bullet) (the circular taper head of circular fuselage and sub warhead apperance is most beneficial for the formation " ring-type in straight trunk Embrace, symmetrically wrap up " steady air flow, prevent " non-annularity, it is non-embrace, it is non-parcel, asymmetric " disorderly air-flow, prevent passenger plane Disintegrate) (thickness of " taper head " is preferably equally thick with " thin circle fuselage ", and " taper head " thickness is not at least in other words Can be thinner than fuselage；Otherwise " thin head cannot protect fatter body ").In scheme, " the snakelike fuselage of overlength " is partable " activity (activity is more big more advantageously forms the soft figure of bending, and be just adapted to can be potentially encountered is not very straight for connecting cabin " Be slightly curved trunk, just can by head punching press draw body it is curved fly, just can be that near airports make small model at trunk two ends Enclose roundabout low speed to jog)；In other words, soft figure or snake body figure are suitable only for being jogged near airports low speed, are not suitable for Trunk is flown nonstop in supersonic speed；It must be stressed that, whenever, only straight even " silk is straight " trunk of level is just suitable for Supersonic Speed, and micro-bend trunk or bending trunk are intended merely to theoretically give counterevidence " the straight trunk of silk " or be suitable only for the low speed start of a race or low speed Landing phases (so-called " silk is straight " refers to that the straight degree in " the winged hole of close-fitting vest " should be similar to gun barrel or the precision of bore).In scheme, Often section " fuselage compartment " (or single-unit cabin) is preferably both single tank type (between not opposing that being changed to two people cabins or multimanned catsule even unites Cabin).In scheme, " level is straight " or " straight flat winged " is all relatively not absolute, i.e., especially supersonic speed flies trunk full section Row section should try one's best holding " level is straight ", but (such as, " micro-bend or micro- slope " to be applied to China west high not to oppose to have micro-bend or micro- slope Eastern low, the northern low basic topography-geomorphology in south high).In scheme, " people of thousand cabin thousand " is generally to refer to, refers to the fuselage compartment in the middle part of a frame passenger plane It is not cabin between a big system, but (such as one " single-berth cabin adds luggage successively to save " the circular fuselage compartment " of very little by a section Cabin ") in tandem occasional combination form, the quantity of these " single-berth cabin adds luggage compartment " is not necessarily 100 sections or 1,000 sections, But including any occasional combination number, i.e., do not oppose more than 1000 sections " single-berth cabin adds luggage compartment " or " single-berth cabin adds less than 100 sections (under special circumstances, such as ultrashort journey, super few passenger flow, do not oppose that a frame passenger plane only sets one or two section single-berth cabin to luggage compartment ", only Take one or two people).In scheme, " afterbody direct-injection rocket " is located at passenger plane most afterbody, spout straight backward, produce it is straight forward Thrust (therefore alternatively referred to as " arrow is crossed in horizontal sliding ").In scheme, " the oblique flame arrow in the whole body " is stealthy to be embedded in each single-unit shell interlayer out of my cabin In, only expose and be uniformly distributed in a whole circle spout of single-unit cabin surrounding (such as four spouts form a circle, eight spouts surround one Circle, 16 spouts spout that forms a circle or more form a circle；The direction of these spouts is backward and outward-dipping, so as to by fire Flame gas is sprayed on the wall of surrounding hole to retreading, and " laterally decompose thrust " that can have both produced towards hole wall allows passenger plane, and " bullet is not touched Wall ", it is also possible to which passenger plane is flat straight to fly to produce straight " longitudinal direction decomposition thrust " forward to allow) (due to " horizontal stroke that " oblique flame arrow " is produced To decomposition thrust " cancelled each other out along hole wall surrounding, last only remaining straight " longitudinal to decompose thrust " forward, therefore " oblique flame arrow " Fall within " horizontal sliding rocket ")；It is smooth that above-mentioned " oblique flame arrow " stealthy embedded purpose is to maintain fuselage cover surface, is more beneficial for Passenger plane is carried out " flywheel ejection " outside hole, and is more beneficial for passenger plane and is realized in hole " without wheel without the wing " and " stray bullet is linear ".Scheme In, just because of in the supersonic flight stage, body is liftoff, can just deserve to be called " passenger plane " (otherwise, not as be referred to as " passenger boat " or " car ").In scheme, close-fitting air bag is matched somebody with somebody by means of " cabin in roller "；By means of " close-fitting air bag " forced position, (one refers to single-berth cabin and luggage Cabin is preferably " tubbiness clinostatism " or " roller clinostatism " to best suit " stray bullet is linear " thin fuselage；Two refer to " close-fitting air bag " or " apery body air bag " or " Lee's air bag of following an example " once inflation just can immediately around human body or luggage so that protect human body or Luggage, and force human body to keep " stretched dorsal position "；Three refers to that " close-fitting air bag " can be mitigated or eliminated human body " universal pressure " And shake；Four refer to configure " close-fitting air bag " precondition be passenger plane be not in overheat, can otherwise burn air bag or appearance Abnormal pressure；Five refers to " forced position " although can be limited limb activity, and need to only stand can fly hole in ten minutes or so Road is whole；Six refers to that " close-fitting air bag " and " forced position " allows passenger to be rotated with fuselage, such as from dorsal position with slower speed Rotating to be lateral position or prone position or even continuously turn-taked with slower speed will not allow passenger to feel that position has the drop will not also to feel To dizziness) (in other words, the largest benefit of " close-fitting air bag " and " forced position " is to allow fuselage slow-speed；Should otherwise enable " flat Weighing apparatus nozzle " offsets fuselage racing).In scheme, it (refers to passenger plane fuselage diameter and " the winged hole of close-fitting vest " to force clinostatism by means of " half meter thin hole " Internal diameter is not too big, it is possible to only half meter or so, it is impossible to forced sitting position, can only force clinostatism, and need to only be adhered to very Clock).In scheme, racing is offset (refer to due to passenger plane appearance " without wheel without the wing " easily rotation, therefore can be by means of " balance nozzle " The passenger plane whole body is embedded " balance nozzle ", and " balance spray opposite to the direction of rotation can be automatically turned on when passenger plane rotation is too obvious Mouth " is to offset racing；" balance nozzle " can be not turned on when passenger plane rotation is less obvious, because " close-fitting air bag " and " strong Compel position " allow passenger not to be afraid of slight rotation) (in other words, rotated not substantially if passenger plane is whole, or passenger is revolved to passenger plane Turn to be reacted without uncomfortable, can not enable always " balance nozzle ").Without wheel without the wing (refer to outside passenger plane by means of " stray bullet is linear " in scheme Shape is " imitative stray bullet linear " or " imitative rocket body is linear " to realize " lower resistance ", passenger plane belly or not setting wheel does not set wing all over the body) Although (in low-speed operations, perhaps wing can provide equilibrant force and lift to passenger plane, and under the conditions of hypersonic speed, wing is on the contrary Large drag forces can be turned into, have no benefit, not as not setting wing) (another benefit of " stray bullet linear+taper head " is advantageous for Reduce and even eliminate " sonic boom ", realize " absolute quietness flight ").In scheme, it (refers to that passenger plane exists steadily to accelerate by means of " ten inner ejections " Into before straight " the winged hole of close-fitting vest ", i.e., when passenger plane hole outside block clearance time, preferably by being up to more than ten kilometers of " flywheel ejection " Or the straight ejection channel such as " electromagnetic launch " or " steam ejection " or " cannon ejection ", " ejection channel " is more long outside the hole, passenger plane Accelerate more steady；" ejection channel " is shorter outside the hole, and passenger plane accelerates more rapid；Therefore, do not oppose that " ejection channel " is only several Kilometer, hundreds of meters or it is shorter).In scheme, it (refers to that dense gas in narrow trunk is running into that wall is not touched by means of " hole bullet punching press " bullet Suddenly the shape in the narrow gap of body surrounding can only be squeezed because having little time diffusion during supersonic speed external " the fly bomb passenger plane " of visiting Into " hole bullet punching press ", calmed the anger pad as a floor height, by force separate body with cartridge chamber, " bullet does not touch wall " is realized, so as to eliminate bullet Hard thing friction between body and cartridge chamber, only gas current friction, had both protected cartridge chamber or had protected body not abraded by hard thing, and significantly Reducing friction resistance；" hole bullet punching press " crosses tunnel and starts blast, steamer and cross valley and lift to the impact that hole wall is produced with motor-car Play billow some similar simply forcing and act on narrow trunk；Producing the precondition in " hole bullet punching press " includes four aspects, one It is to want high-speed flight especially supersonic flight, two is the narrow cartridge chamber or trunk that have intimate close-fitting vest, and three is to have " dense sky Gas " or high velocity air (velocity of sound air-flow)；Four is to have spout towards back sweep and inclined " tiltedly towards hole wall on the passenger plane whole body Flame arrow " is (so as to by " laterally decompose thrust " realizations of " oblique flame arrow " " the not tactile wall of bullet ", and by " oblique flame arrow " " decomposing thrust in longitudinal direction " realizes that straight putting down flies).(refer to that passenger plane can not only maximum limit by means of " body bullet speed " simulation fly bomb in scheme The profile of degree simulated flight neutron bomb or guided missile be " stray bullet is linear " to obtain lower resistance, and can pursue to greatest extent in-flight The speed of bullet or guided missile is " hypersonic speed ", although be extremely difficult to the bullet flying speed of " 20 times of velocities of sound ", but at least can be with Reach one times or many times even ten times of speed of supersonjc missile；And do not oppose that passenger plane speed is less than velocity of sound from start to finish, such as 300 kilometers of short distance trunk passenger planes, even if speed is lower, similarly need to only spend and fly full journey in ten minutes or so).In scheme, " sound Speed ejection " includes " flywheel ejection " or " electromagnetic launch " or " steam ejection " or " cannon ejection " or other ejections, common feature It is that passenger plane can be accelerated to subsonic speed, velocity of sound or supersonic speed from zero-speed；Suggestion is preferential to use " flywheel ejection ".In scheme, " sound Speed ejection " can also be subsonic ejection or supersonic ejection.In scheme, it (refers to passenger plane elder generation to be stamped into hole by means of " velocity of sound ejection " Accelerate hundreds of meters or several public affairs by " flywheel ejection " or " electromagnetic launch " or " steam ejection " or " cannon ejection " etc. outside hole In or more than ten kilometers after reach supersonic speed, just arrive at hole, pour in hole；Since being launched into hole with velocity of sound, will necessarily shape Into " hole bullet punching press " especially " head punching press ", it is ensured that bullet does not touch wall) (by taking " people of thousand cabin thousand " as an example, above-mentioned " flywheel ejection " is Refer to by be arranged in straight up on several kilometers of even more than ten kilometers opening passages four thousands of of side very up and down Flywheel or " roadside flywheel " is driven to provide machine outer power to tens thousand of relays, will be burning hot without the wing snakelike figure of km fuselage without taking turns Head zero-speed passenger plane quickly to velocity of sound, and with velocity of sound launch hole and be stamped into hole [i.e. passenger plane passes through most before being stamped into hole by speed-raising Trigger rocket firing switch during several flywheels in advance afterwards, rocket has been lighted a fire after being stamped into hole], so as to realize that velocity of sound enters hole, i.e., Supersonic speed) (size or material of above-mentioned " flywheel " are usually, using the diameter steel wheel also bigger than automobile wheel footpath, not oppose to use Rubber inflatable wheel, wooden wheel, plastics plastic roller or other materials wheel；Do not oppose using greater or lesser wheel footpath, and wheel footpath is bigger, Ejection inertia is bigger, and ejection efficiency is higher) (if " flywheel ejection " is recorded into slow motion, " flywheel ejection channel " has in principle As " general cargo roller Transfer pipe ", only " flywheel ejection " is arranged with flywheel to point in four walls, and " roller transmission " only exists Bottom wall is arranged with roller) a kind of (so-called " velocity of sound ejection " is fully horizontally straight push forward completely) (either " flywheel bullet Penetrate " or other ejections, " seamless ejection " and " seamless igniting " all should be accomplished, such as should pass through last several flywheels in passenger plane When, rocket firing switch is triggered immediately, it is ensured that passenger plane has been lighted a fire into hole moment rocket launching, if too late, will result in Concord suddenly loses thrust entering hole moment).In scheme, " direct-injection and oblique flame arrow when velocity of sound enters hole Igniting " refers to that passenger plane at least should in advance trigger rocket automatic ignition inductive switch before " velocity of sound enters hole ", and rocket is in the wink for entering hole Between just completed igniting (before in other words, hole would rather being got the jump on just light a fire, can not slowly be misfired after hole is entered).Side In case, by means of " burning hot head " rarefied air, (including two aspects, one refers to " active high temp fire heat engine head ", will passenger plane head Since off " the burning hot head " started with regard to active designs into extreme temperatures of zero-speed, such as thousands of degree high temperature, so as to rarefied air, change Solution resistance；Two refers to " passive high temp fire heat engine head ", i.e., passenger plane is not warm in low speed block clearance time head, when supersonic speed is reached by sky Gas friction head can be more and more warmmer, can also dissolve air drag).In scheme, do not oppose to be changed to " burning hot taper head " " not hot Taper head " (does not oppose to be changed to " burning hot head " " not heat engine head ").In scheme, borrow " light hole preheating " to drive air away (to refer to Borrowing " naked light fire hole " or " dying fire fire hole " long in advance can largely drive outside hole the air in " the winged hole of close-fitting vest " out of, ensure On the premise of thering is enough gas to maintain " head punching press " and " hole bullet punching press " in " close-fitting vest winged hole ", simulate to greatest extent " thin Gas emulates Altitude "；Now, whether passenger plane head is designed to " burning hot head " or " taper head " and perhaps recedes into the background) (ratio Such as electrothermal tube or similar naked light dying fire preheating device are laid in " the winged hole of close-fitting vest " all fronts or most middle part or most two ends；Such as use again Whole solar energy photovoltaic panel is preheated to " the winged hole of close-fitting vest ", even if simply warm fire even dying fire can also drive large quantity of air away) (change Sentence is talked about, if " the winged hole of close-fitting vest " use " fiery hole preheating+magnetic suspension advances+rob hot flight " pattern, can cancel " straight as far as possible Flame arrow " and " oblique flame arrow ", or no longer need to rely on or less need for " hole bullet punching press " and " head punching press " is relied on as far as possible, more Need not rely on traditional " negative-pressure vacuum flies hole ") (" robbing hot flight " refers to allow passenger plane to fly full journey before getting the jump on interior cabin heating, and Need to only fly ten minutes or so) (if " the winged hole of close-fitting vest " is too big using " fiery hole pattern " cost from the beginning to the end, can only in weight Point hole section uses " fiery hole pattern ", such as only at the hole of " velocity of sound ejection be stamped into hole " or use in a bit of winged hole nearby " fiery hole pattern ", can significantly mitigate too high punching press).In scheme, it (refers to " flying outside hole not turn by means of " normotopia ejection " line silk Wheel ejection channel " or other ejection channels can control passenger plane position balance up and down equivalent to one " straight normotopia runway ", Passenger plane will not be especially allowed axial-rotation occur, so that keep human body to be constantly in stretched dorsal position as far as possible, but because human body has Close-fitting air bag protection, it is allowed to which human body has slight or slow rotation；Even if additionally, human body surprisingly in stretched prone position or goes out Now slight rotation also need to only be restrained oneself ten minutes).In scheme, (refer to, why using " outside hole without hole resistance by means of " being launched outside hole " Ejection " rather than using " launch " in the hole in because small in the resistance ratios hole that is subject to of passenger plane open space outside the hole, it is easier to reality Existing short distance accelerates to take off, therefore " being launched outside hole " is more much higher than the efficiency of " being launched in hole ").In scheme, by means of " velocity of sound igniting " decompression It is explosion-proof (to refer to that passenger plane block clearance time rocket and misfires outside hole, but just triggered when reaching supersonic speed and launch into hole Rocket firing is switched, and allows rocket entering hole moment " lighting a fire on the run "；" on the run light a fire " is than " allowing passenger plane to stay in and as you were being stranded point Fire " can more disperse hole to press, and prevent from being exploded because of partial high pressure, thus " on the run light a fire " than " allowing passenger plane to stay in as you were It is stranded and lights a fire " safer).In scheme, by means of " vexed tank rocket " ten times of velocities of sound (refer to that traditional rocket is all used in open space, and The small space in trunk is not used for, former capital is not " vexed tank rocket "；The rocket in trunk is only located at just equivalent to " vexed tank Rocket ", only " vexed tank rocket " could force space to force to have an effect by narrow and small, and thrust multiplication forces passenger plane to raise speed quickly To hypersonic speed；Therefore, even same rocket, the performance in hole outside hole is completely different, and thrust is far longer than hole in hole Outward).In scheme, it (refers to that could only allow passenger plane inertia operation side in the straight trunk of level most to be saved by means of " inertia is flown nonstop to " power consumption It is completely superposed to rocket thrust direction, does not just need thrust-augmented rocket；One because horizontal sliding rocket need not overcome gravity, two Because the straight rocket that pushes away does not need bend power consumption).In scheme, it (refers to that head is produced prior to fuselage to draw body with flying by means of " head punching press " Raw punching press, as long as head realizes " bullet does not touch wall ", fuselage also can slightly bend up and and then leave hole wall, as long as head turns in hole Curved, fuselage also can slightly bend up and and then turn, and certainly, " head turning " is imagination, because head is not required in straight trunk Turn, but if gravity will be overcome on the way in view of passenger plane, turn upwards with faint inclination angle always equivalent to head It is curved；In other words, if man-machine can bear, it is allowed to which passenger plane flies in curved hole；In other words, " it is curved winged that the primary drying pressure that takes this opportunity draws body " It is a meaning with " the primary drying pressure that takes this opportunity is drawn body and flown nonstop to "；In other words, although passenger plane, but also definitely can be slightly always straight winged It is curved winged, similar to " snake body Durchgangshohle "；In other words, " head turning " be possible to bent trunk suitable for imperceptible sedimentation Or suitable for the uneven ground one high and one low gentle slope trunk of potential condition, such as China belongs to Xi Gaodong low-lyings).In scheme, by means of " breakthrough It (refers to that on the premise of passenger plane speed has broken through sound barrier, passenger plane advantage kinetic energy is relatively too strong, weak in hole that sound barrier " flies over seamless Gesture air-flow is relatively too weak, and now, no matter how dense the gas in " close-fitting vest winged hole " has, and is no longer effective resistance, or at all Have little time to form resistance, surging passenger plane is seamless to be flown over) (in other words, on the premise of sound barrier is broken through, passenger plane is no longer because heading on Vapour lock produces enough " head extra-high voltage ", and no longer because air-flow suck-back produces enough " tail spy negative pressure ", whole trunk is in height When Concord flies over it is tranquil as before, it is in a trance all do not occurred) (passenger plane fuselage is more long, the relatively surging kinetic energy of passenger plane It is more obvious, more can in a disguised form dissolve all gas-flow resistances, and have little time to trigger hole inner high voltage just harmless under the conditions of hypersonic speed Pass through) (in a word, once passenger plane breaks through sound barrier, not only imperceptible air-flow sound, and imperceptible stream pressure) (with " tight Body flies hole " certain point position as a example by, any one sonic boom point or high pressure spot are all only equivalent to " miscarriage miso-fire ", and hole wall will not be produced Actual destruction, because when " extra-high voltage produced at head " does not have enough time to jump on hole wall generation destruction also just by " machine The special negative pressure produced at tail " lightning is caught up with and lightning is neutralized；That is, destructive hole pressure also to get up just dodging without liter completely Recover as before between electricity, and passenger plane is from safe the distant of myriametre that fly out in current point position；Even if current point position hole wall is by accidental destruction Also there is the grace time up to " ten minutes " to be repaired, meet next frame " solely flying airliner ") (in theory, after sound barrier is broken through, Ten times of velocities of sound " small bullet " can become " very surging bullet " in face of air drag；But, ten times of velocity of sound " big head visitors Machine " can become " passenger plane surging very much " in face of air drag, because kinetic energy ratio " small of " big head passenger plane " The kinetic energy of bullet " does not know to be eager to excel how many times greatly, therefore " passenger plane surging very much " can more be realized " flying over nothing than " very surging bullet " Trace ") (in other words, passenger plane breaks through sound barrier in advance only outside hole by " velocity of sound ejection ", is just more beneficial for easily changing in hole Solution air drag；Therefore " velocity of sound ejection " is into the key of " hole evagination distorsion barrier, hole internalization solution resistance ") (hypersonic speed passenger plane exists Under " straight flat winged " state, the interference in air flow suffered by fuselage is comparatively substantially zeroed, because interference in air flow is again mostly by head Bear；In other words, after passenger plane has flown full journey, optimal situation is that " thousand section fuselage the slightests are lossless (or need to only to be changed once Property fuselage cover) ", the situation of worst is " head that only need to more renew ", and the cost of head loss or shell loss is too low, low Fuel cost must be only equivalent to, here it is the pleasant place of " straight flat winged in straight trunk "：" protected by need to only sacrificing several meters of heads Km fuselage ") (only km fuselage can just greatly improve single order of classes or grades at school " solely fly airliner " transport power, such as small by " unit one " Transport power brings up to " people of thousand cabin thousand " big transport power).In scheme, by means of " velocity of sound flame " do not burn hole wall (refer to due to passenger plane fly it is too fast, Either the head flame of thousands of degree or the tail rocket of thousands of degree are all without to any baking of hole wall generation or ablation effect； Therefore, do not oppose papery or modeling will to be changed to close to ten times of velocities of sound or more than ten times of hypersonic speed section steel of velocity of sound " the winged hole of close-fitting vest " Material " the winged hole of close-fitting vest "；Such as, even if paper hole is surprisingly burnt, passenger plane is flown over beyond km already, and is enough to change in ten minutes New paper hole, meets next frame " solely flying airliner ") (although second half section speed of the passenger plane in " the winged hole of close-fitting vest " has lowered, no It is again " velocity of sound flame " or " velocity of sound rocket ", but now rocket has stopped working, and " burning hot head " has shifted to an earlier date and is separated with fuselage, And leave by " auxiliary to push away rocket " or " head power " lightning in " the winged hole of close-fitting vest ", leave behind lukewarm fuselage without a head by " trunk bottom wall groove pulley " lowers the temperature in " end Fei Dong " or " end water hole " while jog, until stopping).Scheme In, force and stop that (it is preferably to meet head on to pierce in " end water hole " when passenger plane is soon reached home to refer to, both by means of " end water hole " terminal Can lower the temperature can slow down again, until force stopping；Should " end water hole " should be able to breathe freely, so as to mediate heat engine to the cold water when a large amount of steamings for producing Vapour；Should " end water hole " after passenger plane comes to a complete stop and cools down should be able to draining rapidly, so as to entrance guest go out cabin program).In scheme, borrow " bottom wall pulley " flexible landing (refers to be provided with curved groove point in " end water hole " bottom wall or whole " the winged hole of close-fitting vest " bottom wall Cloth or the load-bearing pulley being distributed in half moon groove, obtain groove pulley support when passenger plane can not only be allowed to land, and can be by Groove pulley eliminates the harmful friction between hole wall and passenger plane).In scheme, it (refers to red as fire to avoid heat wave by means of " head division " Head can produce strong heat radiation, and the last second just allows head to close up with fuselage preferably before ejection starts；Preferably in visitor Machine just allows head to be separated as early as possible with fuselage when starting to land or slow down, and can thus allow passenger entering when cabin goes out cabin away from hot spoke Penetrate；Such as, when passenger plane prepares fall-retarding, head can be allowed to depart from fuselage, is not slowed down not only on the contrary by head ancillary rocket Accelerate, take advantage of before flood in hole pours in down a chimney and run more remote better, one is " steam fumigating day " so that made when head is contacted with water, Two is so that head meets water is forced cooling, because head can not lower the temperature always, directly to turn around while hot as next airliner Burning hot head, if three is that short head is combined with fuselage long, is difficult to turn or turns around, short head departs from leader after one's death Could flexibly turn, flexibly turn around, could shift to an earlier date from hole or independent from hole prior to fuselage).In scheme, by means of " airport subdivision " flexibly Going for a stroll, (it is airport at trunk two ends to refer to, " thousand cabin chiliarch fuselage " only is dispersed into a short fuselage single-berth cabin successively, Can flexibly be turned by the car that picks near airports, flexibly turned around, flexible transition).In scheme, by means of " oxygen-enriched winged hole " rocket detonation (refer to " close-fitting vest winged hole " be preferably belonging to that can special oxygen supply " oxygen-enriched winged hole ", benefit can be to allow rocket burning to fill Point, power is violent, less can accident extinguishing, can also further mitigate invalid load from carrying too heavy oxygen gas tank on passenger plane) (such as Fruit is to employ " fiery hole preheating drive air away ", then air and oxygen in " the winged hole of close-fitting vest " can largely be driven away, now without Method realizes " oxygen-enriched winged hole ", and now passenger plane must be carried " rocket fuel oxygen tank ").In scheme, the power of passenger plane is dynamic except rocket Outside power, can also be jet power, electromagnetic path power, magnetcisuspension track power, nuclear power, solar energy and other power (if Using " magnetic suspension power ", " the winged hole of close-fitting vest " can be designed to " fire hole long " and drive air in hole away, because in magnetic suspension mould No longer needed under formula in " hole bullet punching press " and " head punching press ", the purpose for driving air away is to reduce air drag).In scheme, by means of " half Journey fuel " stops working to continue and flies (to refer to that rocket whole fuel are preferably " half way fuel ", i.e., when can only fly to more than half voyage for passenger plane Will after-flame stop working, range-to-go slows down rather than grounding immediately naturally；Therefore, the purpose of " half way fuel " is to allow passenger plane Fly over unconditional pre-decelerating during more than half voyage, it is ensured that safety, and substantially reduce passenger plane body weight；In other words, " half way fuel " " would rather fly also fly over terminal less than terminal " " would rather be stayed in trunk should not also hit mountain more " " Ning Yaoan can be realized Entirely should not speed "；In other words, think again very fast a little without strength after passenger plane flies over more than half voyage；Existing passenger plane it So can not halfway stop working or double hairs must be set, because existing passenger plane is in meters altitude, stops working and mean that air crash, compare Under, trunk passenger plane is nap of the earth flight, even if courageously flame-out do not suffer from myriametre drop yet；Double hair passenger planes or complete in meters altitude Journey fuel will greatly increase the invalid load of passenger plane, and limitation is effectively manned；Single-shot passenger plane or half way fuel will mitigate significantly in trunk The invalid load of passenger plane, increase is effectively manned) (additionally, the more potential safety hazards of fuel are bigger).In scheme, do not oppose " half way fires Material " is changed to " global fuel ", does not oppose to be changed to " half way all burnt is flame-out continuous winged " " the sufficient shutdown of global fuel is continuous to fly ".Side In case, do not oppose to be located at head or fuselage by institute is dynamic, rather than tail must be located at.In scheme, by means of " arrow has flown " Whole rocket recovery (refer to that passenger plane need to only fly ten minutes, therefore need to only assemble one piece of rocket, and halfway need not abandon rocket, Therefore can accomplish that whole rocket is reclaimed).In scheme, got over by means of " multistage useless arrow " and leap that light (one piece big rocket for referring to passenger plane afterbody can be by Multistage mouse composition, every grade of mouse can be discarded in trunk to mitigate passenger plane weight on the spot after running out of gas, and The useless arrow energy intelligent positioning abandoned, can just open trunk and renovate the useless arrow of recovery with positioning mileage, or in the trunk of every kilometers length An automatic obstacle cleaning machine is provided with, can be cleaned up one kilometer of trunk long in ten minutes；Removed obstacles than opening in regular trunk Removed obstacles between emptying much easier；" the useless arrow of multistage " can allow passenger plane more to leap light or more leap fast；" the accumulative weight of multistep rocket Amount " is conducive to mitigating human body acceleration pressure by overweight rocket body in the off stage；" cumulative weight " is more big more can mitigate in early stage Human body accelerates pressure, and more ultralight passenger plane can be obtained in the later stage after going out of use) (strong suggestion is not used only with " one-stage rocket " " multistep rocket ", benefit is to be not required to midway to throw arrow, in fact " whole rocket is reclaimed completely automatically ").In scheme, kept away by means of " overlength passenger plane " Speed change pressure (refer to passenger plane more long, quality is bigger, slight external force be difficult change passenger plane inertia, thus be difficult generation allow human body without The speed change pressure that method is born).In scheme, it (refers to that passenger plane flies in the straight trunk patch of level to keep away falling bodies pressure by means of " zero meter of drop " OK, it is impossible to have drop over the ground, unlikely there is myriametre drop, be not required to worry air crash；Will not produce and make human body unaffordable Falling bodies pressure).In scheme, by means of " hypersonic speed " set ten minutes airliners (refer in thousands of inner trunks passenger plane with general " ten overtones Speed " is probably only needed to ten minutes or so when having flown full journey；Do not oppose, higher or lower than " ten times of velocities of sound ", not oppose to be more or less than Ten minutes one time, but advise that either a thousand li trunk or hundred inner trunks all preferably maintain to should be for ten minutes one time strongly " ten minutes airliners ", because " one minute airliner " is although it is possible to realize but too short due to being spaced between airliner, even if passenger plane comes Obtain and react, passenger also has little time reaction, can usually miss boarding).In scheme, unless otherwise specified, " ten minutes " are general Refer to, refer generally to ten minutes or so, but do not oppose far more than or less than ten minutes.In scheme, by means of the flight of " falling without parachuting " loss of weight (refer to space return capsule or Great Britain and France consonance Concord compared with, can at least remove from weigh hundred kilograms parachute harness and Controlling organization, so as to mitigate the invalid load of passenger plane significantly, increases passenger plane payload；Why passenger plane need not set landing Umbrella, because can realize prompt drop using the reverse wind-tunnel of trunk end, reverse water hole, reverse steam, slow drop, force-land, force Stop).In scheme, by means of " magnetcisuspension power " replace rocket (refer to select passenger plane power when, preferential recommendation " rocket passenger plane ", but Do not oppose to be changed to " electromagnetic power passenger plane "；" electromagnetic power passenger plane " refers to be made up of stator trunk or stator track and mover passenger plane Electromagnetic power passenger plane, the passenger plane makees " electromagnetic launch " outside trunk or makees magnetic suspension supersonic flight in trunk；Passenger plane is moved Power generally can be divided into " ejection power outside hole " and " rocket-powered in hole " two parts, not oppose to be changed to " rocket-powered in hole " Jet engine, electromagnetic path power, magnetcisuspension power, solar energy, nuclear power etc.；Do not oppose to be changed to " flywheel ejection outside hole " " electromagnetic launch outside hole " or other types are launched, such as do not oppose to be changed to " driven by power ejection " " Electromagnetic Drive ejection ").Side In case, solely fly by means of " people of thousand cabin thousand " machine (although referring to only to allow " machine solely flies " in whole " the winged hole of close-fitting vest " in every ten minutes, This " solely flying airliner " often not only takes the people hundreds of people of several people tens, but takes thousands of people, therefore freight volume is big) (do not oppose this " solely flying airliner " is provided only with the people of a cabin one, the people of ten cabin ten, the people of hundred cabin hundred, or more or less).In scheme, by means of " solely flying airliner " Acyclic homologically trioial degree (since referring to only to allow " machine solely flies " in the straight trunk of thousands of kilometers, avoids the need for considering multi-machine Scheduling, less Need to consider air control；Only need to ensure next passenger plane enter hole instruction must be under ability after a passenger plane in confirmation has been appeared Reach；In other words, it is not that must assign within every ten minutes passenger plane to enter hole instruction).It is unmanned by means of " straight hole solely flies " in scheme (when referring to passenger plane a machine solely flies in straight close-fitting winged hole, both do not need control direction, it is not required that aircraft before and after observation, more Front road conditions need not be observed, therefore need not be manned) (only unmanned, could further to reduce invalid load) ( Have unmanned, can just get around " burning hot head cannot accommodate driver's cockpit " without solution problem) (but never oppose will be unmanned It is changed to manned).In scheme, by means of " closed trunk " zero noise no pollution (refer to noise again it is big pollution again weigh can be closed Or semi-hermetic is in individual layer or interlayer trunk, supply need to be only set at the hole of two ends or along trunk keypoint part or trunk and supplied Oxygen system or Abgasabsaugung system) (due to there is no " with flying airliner " after " solely flying airliner ", there is time enough space to aspirate Rocket tail gas in " the winged hole of close-fitting vest ", such as automatic trigger ventilatory switch, changes clean fresh oxygen-enriched air when passenger plane flies over, Next airliner can be completely met after ten minutes again).In scheme, it (refers in thousands of public affairs that by means of " hole is moved in hundred cities ", short change is long-distance Hundred small cities must be built up along the straight trunk in borough chief way includes new city or old city, and every small city individually builds one section can be with " the two km augers " of integral translation, typically just equivalent to two km length of the people's passenger plane of thousand cabin of a frame thousand, should " two km machines Hole " can be to be incorporated to main line, so that all small cities along the line after one or two meter of main line or left and right translation are incorporated to after one or two meter of upper and lower translation Can lead to " fly hole passenger plane ", precondition is only to allow a small city to merge every ten minutes or so, it is ensured that in ten minutes An only frame passenger plane is flying on thousands of kilometers of trunks all fronts).In scheme, " hole is moved in hundred cities " can also be " hundred Cheng Cha holes " (branch Hole and trunk hole pass through the doubling of turnout hole) (with traditional track switch unlike, it is impossible to the two frame passenger planes of appearance or winged track switch at Car, that is, be not in collide or conflict, because being " solely flying airliner ", therefore " hundred Cheng Cha holes " is safe everywhere).In scheme, by means of " single line Return " to halve (refer to that can both build one toward one to return multiple line trunk, it is also possible to only build a single line trunk for investment；If only building one Bar single line trunk, can be flown for preceding ten minutes by a frame airliner is positive, can reversely be flown by another frame airliner within ten minutes afterwards；" single line Return " precondition be " as long as having flown full journey ten minutes or so "；" single line is returned " can halve trunk investment).Scheme In, by means of " heat-insulated close cabin " rob heat flight (refer to passenger plane shell be bound in hypersonic flight heating even be under fire, but due to Passenger plane has flown full journey and has only needed to ten minutes, can only allow nacelle cover to generate heat or be under fire by " heat-insulated close cabin " completely, does not allow machine Cabin inner casing heating, and need to only adhere to ten minutes, so as to realize " robbing hot flight ").In scheme, borrow " disposable shell " to rob fire to fly (" robbing fiery flight " refers to allow passenger plane to get the jump in baked wheaten cake to have flown full journey before cabin to row, and need to only be flown ten minutes or so, at this very Allowed in clock " burning outer cabin ") (" robbing hot flight " or " robbing fiery flight " cannot be only used for high temp fire hole, it can also be used to lukewarm Normal temperature and pressure " close-fitting vest winged hole ") (since allowing " burning outer cabin ", illustrate that fuselage and the appearance of hole wall unintentionally rub not intentionally It is again extremely big bad thing；In addition the rigidity friction under the conditions of hypersonic speed between fuselage and hole wall becomes air cushion friction, therefore rub Coefficient is wiped to reduce rapidly) (in other words, in order to obtain " hypersonic speed ", fuselage cover can be designed to the wear-resisting " weight of resistance to burning Renaturation uses shell " or " single use shell ", this " disposable shell " is somewhat similarly to the " special outer of Manned reentry capsule Shell+surface coating ") (in other words, in order to obtain " hypersonic speed ", sometimes have to sacrifice fuselage cover) (" rob heat to fly OK " or " robbing fiery flight " is alternatively referred to as " rob shell flight " sometimes).In scheme, by means of " the resistance to burning of head " protection fuselage (refer to, as long as The resistance to burning of head, would not burn fuselage, now, it is no longer necessary to use " disposable fuselage cover ", at most only need using " disposable Handpiece case ") (such as, " solely fly airliner " and flown full journey, if need to only change handpiece case, be not required to change fuselage cover, then Flight cost is substantially reduced) (in other words, passenger plane once reaches hypersonic speed, spells no longer to be fuselage but head, in other words Only needing to spelling head need not spell fuselage) (only by " straight trunk " " thin circular knitting machine body " " taper head ", head could be damaged Mistake is preferably minimized).In scheme, by means of " closed oxygen cabin " rob oxygen flight (refer to " passenger plane single-berth cabin " preferably with it is existing " space flight return The structure of cabin " or " deep sea diving water tank " is similar to, preferably hermetically sealed, high temperature resistance, anti-high pressure, from oxygen supply, air-tight cabin, watertight compartment knot Structure, such as can place a small amount of sodium peroxide oxygen generating agent in cabin and provide oxygen, and need to only maintain " to rob oxygen to fly for ten minutes or so OK "；Get the jump on and flown full journey in cabin before oxygen depletion) (one of the shortcoming of existing " space flight return capsule " is needed by huge Manpower and materials could position drop point in boundless and indistinct landing field, spacefarer is delayed significantly and goes out cabin, and " passenger plane return capsule " need not Positioning, must be located in trunk, must be located at destination county；Therefore, the advantage of " passenger plane return capsule " is accurate positioning, goes out cabin Hurry up) (the two of the shortcoming of " space flight return capsule " are to need to carry heavy parachute, therefore, nacelle is too big；Conversely, " passenger plane is returned Without parachute kit, the bodily form is light and handy, reduces invalid load, improves payload in cabin ") (" passenger plane return capsule " mentioned here with " passenger plane single-berth cabin " or " cabin in passenger plane " is a meaning).In scheme, " trunk " or " main cabin " whether light-permeable transparent nothing is fastened Will, because even passenger is put into " hole Zhong Hei rooms " also need to only stand ten minutes or so；Even if communication signal is interrupted in cabin, also most Many " lost contacts " (compared with spaceship, are always maintained at easy to be obtained to carrying out monitoring remote video in passenger plane cabin for ten minutes It is many).

Specific embodiment

Embodiment one：It is with " Beijing to linear ten times of velocities of sound of Hong Kong stray bullet flies hole passenger plane (unmanned solely winged airliner) " now The invention will be further described for example (referred to as " long-distance Beijing-Hongkong passenger plane ")；Assuming that passenger is 100 people, " ten times of velocities of sound " strip is taken The people's passenger plane of hundred cabin of shape hundred, passenger plane reaches Hong Kong after ten minutes for half way fuel from Beijing, and 2200 kilometers of trunk total length (is Normal temperature and pressure " the winged hole of close-fitting vest ", does not use fiery hole temporarily)；(" flywheel ejection " close-fitting vest passage using three kilometers long)." long-distance capital The specific flight course of guests from Hong Kong's machine " is as follows, and " the people's passenger plane of hundred cabin hundred " finishes relief cold body in " Beijing Fei Dong airports " passenger's boarding It is connected as a single entity with heat engine head, accelerated to be issued to supersonic speed in thousands of flywheel relays by over one hundred second, it is " close-fitting that will reach Rocket automatic ignition inductive switch is triggered in advance during the entrance of winged hole ", is launched into hole (being stamped into hole) moment, passenger plane afterbody in passenger plane Tiltedly flame arrow has been lighted a fire (on the run light a fire) (velocity of sound igniting) for direct-injection rocket and the passenger plane whole body, and passenger plane is by means of " hole bullet punching press " and " machine Primary drying pressure " bullet does not touch wall, and passenger plane is in the case where the strength of " the oblique flame arrow of afterbody direct-injection rocket and the whole body " (i.e. " vexed tank rocket ") is promoted Quickly reach hypersonic speed (ten times of velocities of sound), when passenger plane flies over " more than half voyage ", rocket fuel exhaust in advance in advance stop working but Passenger plane continues to flight, when passenger plane substantially reduces speed now, allows head to be separated with fuselage, although head does not slow down or slows down Be consistently faster than fuselage (head with auxiliary push away rocket), therefore head can speed away currently " close-fitting to fly hole ", only passenger plane fuselage and The people of hundred cabin hundred also continues to fly and slowly slow down in current " the winged hole of close-fitting vest ", when passenger plane is reached in last 20 kilometers " the winged hole of close-fitting vest " When, triggering " end water hole flood pours in down a chimney switch ", passenger plane is slided forward by " close-fitting fly hole " bottom wall pulley on one side, while by Slow down against the current and lower the temperature by cold water, until (and unnecessary ponding in hole is entered into trunk lower section closed conduit and reusable edible) is stopped, After passenger plane comes to a complete stop, whole segment length's fuselage be divided into 100 section single-berth cabin (respectively with the car that picks), with the car that picks leave it is thousands of in The least significant end in straight hole, " Hong Kong Fei Dong airports " exit is reached by airport bend, and hatch door is automatically turned on, and passenger freely goes out cabin.

Embodiment two：It is with " Wuchang to the linear one times of velocity of sound of Jing Zhou stray bullet flies hole passenger plane (unmanned solely winged airliner) " now The invention will be further described for example (referred to as " short distance force chaste tree passenger plane ")；Assuming that passenger is 10 people, " one times of velocity of sound " strip is taken The people's passenger plane of ten cabin of shape ten, passenger plane reaches Jing Zhou after ten minutes for half way fuel from Wuchang, and 200 kilometers of trunk total length (is normal Normal temperature and pressure " the winged hole of close-fitting vest ", does not use fiery hole temporarily)；(" electromagnetic launch " track using two kilometers long)." short distance force chaste tree visitor The specific flight course of machine " is as follows, and " the people's passenger plane of ten cabin ten " finishes relief cold body with heat in " Wuchang Fei Dong airports " passenger's boarding Head is connected as a single entity, and supersonic speed is issued to by the lasting acceleration in electromagnetic launch track in a hundred or so second, " close-fitting that will reach Rocket automatic ignition inductive switch is triggered in advance during the entrance of winged hole ", is launched into hole (being stamped into hole) moment, passenger plane afterbody in passenger plane Tiltedly flame arrow has been lighted a fire (on the run light a fire) (velocity of sound igniting) for direct-injection rocket and the passenger plane whole body, and passenger plane is by means of " hole bullet punching press " and " machine Primary drying pressure " bullet does not touch wall, and passenger plane is in the case where the strength of " the oblique flame arrow of afterbody direct-injection rocket and the whole body " (i.e. " vexed tank rocket ") is promoted Supersonic speed (one times of velocity of sound) is quickly reached, when passenger plane flies over " more than half voyage ", rocket fuel exhausts stop working in advance but visitor in advance Machine continues to flight, when passenger plane substantially reduces speed now, allows head to be separated with fuselage, although head does not slow down or slows down the beginning Fuselage (head pushes away rocket with auxiliary), currently " the winged hole of close-fitting vest ", only passenger plane fuselage and ten therefore head can speed away are faster than eventually The people of cabin ten also continues to fly and slowly slow down in current " the winged hole of close-fitting vest ", when passenger plane reaches last 3 kilometers " the winged hole of close-fitting vest ", Triggering " end water hole flood pours in down a chimney switch ", passenger plane is slided forward by " close-fitting fly hole " bottom wall pulley on one side, while by inverse Water slows down and lowers the temperature by cold water, until stop (and unnecessary ponding in hole is entered into trunk lower section closed conduit and reusable edible), when After passenger plane comes to a complete stop, whole segment length's fuselage is divided into ten section single-berth cabins (respectively with the car that picks), and hundreds of li of straight holes are left with the car that picks Least significant end, reach " Jing Zhou Fei Dong airports " exit by airport bend, hatch door is automatically turned on, and passenger freely goes out cabin.

In the above two embodiments, " the close-fitting winged hole of normal temperature and pressure " can be changed to " the close-fitting fire hole of high-temperature pressure " (two The open fire hole in end hole, burning things which may cause a fire disaster is located at trunk interlude or trunk full section), or " can be with reusable passenger plane shell " be changed Into can be with " the disposable shell " of Quick universal.In the above two embodiments, in " the winged hole of the close-fitting vest " second half section, passenger plane has slowed down To subsonic speed even well below velocity of sound, especially " end water hole " passenger plane speed is very low, therefore, " the winged hole of the close-fitting vest " second half section (including " end water hole ") is preferably open ventilative hole or pressure release hole, so as to lay down in time partial high pressure in trunk (this be because For subsonic speed passenger plane cannot break through sound barrier in " the winged hole of the close-fitting vest " second half section, therefore subsonic speed passenger plane is in " the winged hole of close-fitting vest ", and the second half section is on the contrary Than hypersonic speed passenger plane actual pressure that " close-fitting vest winged hole " front half section is met with is relatively higher, actual resistance is relatively bigger, just Small air drag also becomes advantage relatively during like " an arrow at the end of its flight -- a spent force ") (in other words, the most dangerous rank of passenger traffic Section is not the hypersonic speed stage, but catapult-assisted take-off stage or eventually end landing phases；Fortunately either catapult-assisted take-off or eventually end Landing, passenger plane is all controlled in " four walls close-fitting vest passage ", is not in that open aerial shake even fuselage is overturned, thus visitor Opportunity to it is dangerous be all " controllable danger " among expecting) (do not oppose " close-fitting vest winged hole " all designs from the beginning to the end Into opening ventilative hole or pressure release hole, such as whole holes wall is provided with " air-vent " or " relief valve " along trunk).

The either people of hundred cabin hundred or the people of thousand cabin thousand, are preferably subdivision boarding and preferably with following " six during passenger's boarding Step boarding method "：1 passenger gets " the loose air sac coat " of unaerated；2 passengers put on " the loose air sac coat " of unaerated；3 passengers are double Pin closes up arms down stretched and stands immediately below " roller fuselage cover "；4 upper ends bind lower ending opening " roller fuselage cover " with Mechanical arm is slowly decreased until and covers upright passenger completely；5 " loose air sac coats " inflation become " close-fitting air sac coat " (passenger by " autonomous orthostatic position " becomes " forcing stretched position ")；The closing of 6 " roller fuselage cover " cover mouths (i.e. by manually or mechanically closing hatch door, And vertical shape " roller fuselage cover " is become into the shape " closing single-berth cabin " that couches by mechanical arm, and by the people of hundred cabin hundred or the people of thousand cabin thousand Be connected as a single entity composition " the snakelike fuselage of overlength ").It is (similar that " luggage compartment " also substantially follows above-mentioned " six step boarding methods "； Only " luggage compartment " is significantly shorter than " single-berth cabin ", such as " luggage compartment " is about half meter and " single-berth cabin " is about two meters；Do not oppose Vary with each individual i.e. the person that has luggage or individual sub- the higher person with " trombone single-berth cabin " no baggage person or shorter person with " cornet one Cabin "；Either fat person or lean person its cab body thickness all should be equally) (over dimensioning luggage refuses boarding).

Claims

1. a kind of linear hypersonic speed of stray bullet flies hole passenger plane (solely flying airliner), it is characterized in that, it is straight in an elongated tubular product level A frame is provided with the winged hole of close-fitting vest to be made up of burning hot taper head, the snakelike fuselage of overlength, afterbody direct-injection rocket, the oblique flame arrow in the whole body The imitative machine of thousand cabin of body, thousand people one of strip solely flies passenger plane (solely flying airliner), and the passenger plane is stamped into hole by means of " velocity of sound ejection ", the direct-injection And tiltedly flame arrow is just lighted a fire when velocity of sound enters hole.

2. hole passenger plane (solely flying airliner) is flown according to a kind of stray bullet linear hypersonic speed described in claim 1, it is characterised in that by means of " ten In launch " steady accelerate；By means of " stray bullet line style " without wheel without the wing；Wall is not touched by means of " hole bullet punching press " bullet；Fly by means of " body bullet speed " simulation Bullet；Reduce resistance by means of " taper head "；By means of " burning hot head " rarefied air；" light hole preheating " is borrowed to drive air away；By means of " head is rushed Pressure " draws body with flying；Flown over by means of " breakthrough sound barrier " seamless；Hole wall is not burnt by means of " velocity of sound flame "；Do not turn by means of " normotopia ejection " line silk；Borrow " being launched outside hole " is without hole resistance；By means of " velocity of sound igniting " decompression explosion-proof；By means of " vexed tank rocket " ten times of velocities of sound；By means of " inertia is flown nonstop to " power consumption Most save；Hot flight is robbed by means of " heat-insulated close cabin "；" disposable shell " is borrowed to rob light flight；Fuselage is protected by means of " the resistance to burning of head "；By means of " closed Oxygen flight is robbed in oxygen cabin "；Force and stop by means of " end water hole " terminal；Land by means of " bottom wall pulley " is flexible；Match somebody with somebody close-fitting gas by means of " cabin in roller " Capsule；By means of " close-fitting air bag " forced position；Clinostatism is forced by means of " half meter thin hole "；Racing is offset by means of " balance nozzle "；By means of " head point Close " avoid heat wave；Flexibly gone for a stroll by means of " airport subdivision "；By means of " oxygen-enriched winged hole " rocket detonation；Reclaimed by means of " arrow has flown " whole rocket；Borrow " the useless arrow of multistage " is got over and is leapt gently；It is flame-out continuous winged by means of " half way fuel "；Speed change pressure is kept away by means of " overlength passenger plane "；Kept away by means of " zero meter of drop " Falling bodies pressure；Ten minutes airliners are set by means of " hypersonic speed "；By means of the flight of " falling without parachuting " loss of weight；Replace rocket by means of " magnetcisuspension power "； By means of " closed trunk " zero noise no pollution；Solely fly by means of " people of thousand cabin thousand " machine；By means of " solely flying airliner " acyclic homologically trioial degree (ten minutes a time)； It is unmanned by means of " straight hole solely flies "；It is long-distance by means of " hole is moved in hundred cities " short change；Halve by means of " single line is returned " investment.

3. hole passenger plane (solely flying airliner) is flown according to a kind of stray bullet linear hypersonic speed described in claim 1, it is characterised in that " close-fitting Fly hole " " fiery hole preheating+magnetic suspension advances+rob hot flight " pattern can be used.

4. hole passenger plane (solely flying airliner) is flown according to a kind of stray bullet linear hypersonic speed described in claim 1, it is characterised in that " burning hot Taper head " can be changed to " thermal spike does not cut head ".

5. hole passenger plane (solely flying airliner) is flown according to a kind of stray bullet linear hypersonic speed described in claim 1, it is characterised in that " close-fitting Fly hole " both can be high temp fire hole, or lukewarm normal temperature and pressure hole.

6. hole passenger plane (solely flying airliner) is flown according to a kind of stray bullet linear hypersonic speed described in claim 1, it is characterised in that " close-fitting Fly hole " can be open ventilative hole or pressure release hole.

7. hole passenger plane (solely flying airliner) is flown according to a kind of stray bullet linear hypersonic speed described in claim 1, it is characterised in that " velocity of sound Ejection " can be flywheel ejection or electromagnetic launch or steam ejection or cannon ejection.

8. hole passenger plane (solely flying airliner) is flown according to a kind of stray bullet linear hypersonic speed described in claim 1, it is characterised in that the visitor Machine is " ten minutes airliners " (the short hole supersonic speed in hole long, hundred inner a thousand lis ten minutes).

9. hole passenger plane (solely flying airliner) is flown according to a kind of stray bullet linear hypersonic speed described in claim 1, it is characterised in that " velocity of sound Ejection " can be velocity of sound ejection, subsonic ejection or supersonic ejection.

10. hole passenger plane (solely flying airliner) is flown according to a kind of stray bullet linear hypersonic speed described in claim 1, it is characterised in that thousand cabins Thousand people use " six step boarding methods " subdivision boarding.