CN105156230A - Working method of Laval nozzle effect stacking ram rocket - Google Patents

Working method of Laval nozzle effect stacking ram rocket Download PDF

Info

Publication number
CN105156230A
CN105156230A CN201510409699.1A CN201510409699A CN105156230A CN 105156230 A CN105156230 A CN 105156230A CN 201510409699 A CN201510409699 A CN 201510409699A CN 105156230 A CN105156230 A CN 105156230A
Authority
CN
China
Prior art keywords
many
fuel adding
anemostat
laval nozzle
breathing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201510409699.1A
Other languages
Chinese (zh)
Inventor
杜善骥
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201510409699.1A priority Critical patent/CN105156230A/en
Publication of CN105156230A publication Critical patent/CN105156230A/en
Pending legal-status Critical Current

Links

Landscapes

  • Monitoring And Testing Of Nuclear Reactors (AREA)
  • Testing Of Engines (AREA)

Abstract

The invention relates to a working method of a Laval nozzle effect stacking ram rocket and belongs to the technical field of aviation. Air suction is conducted two times or multiple times, and the rocket can launch at the zero speed. A small head rocket (1) (a traditional rocket needing liquid oxygen) drives two sets of flow jetting and air sucking devices to complete active air suction and fuel filling. When the rocket enters the outer space, all valves (8) are closed. The rocket flies in a traditional liquid oxygen and liquid oxygen combustion mode. After the work in the outer space is finished, the rocket flies back to atmosphere. The small head rocket ignites again, and the Laval nozzle effect stacking ram rocket which can be used repeatedly is started to return to the ground. According to the working theory, a Laval nozzle is utilized by an American engineer, positive pressure is created at one end, negative pressure is created at the other end, and a table tennis ball reaches supersonic velocity so that a table tennis bat can be broken to pieces (details can be found in the Laval nozzle part in substantive examination reference data). The technique is applied to a propelling system of the rocket, hypersonic-velocity jet flame is generated, and therefore the flying speed of the rocket is higher.

Description

Laval nozzle effect superposition ram rocket method of work
Technical field
Laval nozzle effect superposition ram rocket method of work relates to and belongs to aviation and space technology field.For following sky and space plane motor and re-entry space vehicle motor.
Background technique
Although space shuttle is a a progressive step compared with nonrecoverable carrier rocket, still have such as faults frequent, many deficiencies such as somewhat expensive.And sky and space plane is different from space shuttle, its ground installation is simple, and safeguard easy to use, operating cost is low, and on common large airport, just energy horizontal take-off and landing, has the flight frequency of general course line airliner.The external form of this aircraft is similar to large-scale supersonic jet passenger plane, has the advantage of aircraft more., when aerial flight, make full use of the oxygen in air.What it can be up to a hundred time in addition reuses, and really achieves the advantage of high-effect and low expense.It is estimated, launch near earth satellite expense with its and only have 1/5 of space shuttle, and launch synchronous satellite expense and only need 1/10.
Summary of the invention
Laval nozzle effect superposition ram rocket method of work is in brief: air-breathing duct 2 in flame jet drive first set jet suction means < after head mouse 1 (being the traditional rocket needing liquid oxygen to carry out work) starts (or, with outer suction duct 3), induction chamber 4, Laval nozzle 5, diffusing tube 6 is called first set jet suction means >, at fuel adding point 10, fuel adding point 11 is annotated rocket fuel, light a fire in igniting place 9, fuel and air burn in the typhon mouth of diffusing tube 6, jet suction means (suction port 17 is overlapped in the injection motivational drive second produced, outer air-breathing duct 16, diffusing tube 6, diffusing tube 15 is called the second cover jet suction means) at fuel adding point 13, fuel adding point 14 filling liquid, solid fuel and catalyzer, in a place 18 igniting, burn in rocket chamber 7.
When rocket flight speed can meet punching press suction condition, head mouse quits work, due to the high speed of rocket flight, make the air of head-on coming be stamped into interior suction duct 2 (or, with outer air-breathing duct 3) in outer air-breathing duct 16, be stamped in diffusing tube 6, meanwhile to annotate rocket fuel at fuel adding point 10 and fuel adding point 11, the fuel mixed with air enters in diffusing tube 15 through diffusing tube 6, meanwhile to annotate rocket liquid at fuel adding point 13 and fuel adding point 14, solid rocket fuel and catalyzer, air is stamped in diffusing tube 15 through outer air-breathing duct 16 and suction port 17, air and fuel mix at this, meanwhile another part air is stamped to two punching press sucking pipes 19 and (opens two valves 8 on this two tubes, at punching press sucking pipe front end filling rocket fuel and igniting place can be set) if needed, import the typhon mouth place of diffusing tube 15, light a fire with igniting place 18, spray in rocket chamber 7 and burn.
In arrow firing chamber 7, flame of combustion air-flow sprays into Laval nozzle means for influencing (Laval nozzle 20 through Laval nozzle 20, vacuum chamber 21, diffusing tube 22, your means for influencing of Bearing score nozzle indication be exactly these 3 parts), the working principle of Laval nozzle effect rocket utilizes Laval nozzle according to American engineer, malleation is set up in one end, the other end sets up negative pressure, make table tennis reach ultrasound velocity and smash table tennis bat (the Laval nozzle part see examination as to substances reference), this technology is used in rocket propulsion system, produce hypersonic flame flow, make the speed of rocket flight faster and have two punching press air suction functions and two filling rocket fuels awing, this rocket can take off in zero-speed, active inspiration and fueling are something or somebody to fall back on portion mouses (is utilize liquid hydrogen, traditional rocket of liquid oxygen work) drive jet suction means to complete, when the speed of rocket can meet punching press suction condition, head mouse 1 quits work, enter punching press air-breathing working method, closeall valve 8 when entering space, use traditional liquid hydrogen and the flight of liquid oxygen combustion manner, at the complete reentry of space work, head mouse is lighted a fire again, start Laval nozzle effect superposition ram rocket and return to ground, Laval nozzle effect superposition ram rocket is can repeatedly with the rocket made.
The appended drawings show
Fig. 1 is many interior gas duct Lavalle effect superposition ram rocket figure, as shown in Figure 1, 4 interior air-breathing ducts 2, the inside penetrating head mouse 1 from the front of head mouse 1 passes to induction chamber 4, first time, air-breathing was by head mouse driving the 1st cover jet suction means, filling rocket fuel, burn in diffusing tube 6 typhon mouth after igniting, the flame flow produced drives the 2nd cover jet suction means, filling rocket fuel, burn in rocket chamber 7 after igniting, when meeting punching press suction condition, whether head mouse quits work (head mouse can be selected to quit work according to flight survey formula), and air enters through the 1st cover and the 2nd cover jet suction means (Laval nozzle does not work), filling rocket fuel, air imports in diffusing tube 15 typhon mouth through punching press sucking pipe 19 by another part air, enter after igniting in rocket chamber 7 and burn, select the open/close states of valve 8 as required, the flame flow produced sprays into Laval nozzle means for influencing through Laval nozzle 20, make the faster of rocket flight.
Fig. 2 is many interior air-breathing ducts and single outer gas duct Lavalle effect superposition ram rocket figure, as shown in Figure 2, 4 interior air-breathing ducts 2, penetrate inside to pass (induction chamber 4 fuses with outer air-breathing duct 3) from the front of head mouse 1 to outer air-breathing duct 3, 1st time air-breathing drives the 1st cover jet suction means by head mouse, filling rocket fuel, burn in diffusing tube 6 typhon mouth after igniting, the flame flow produced drives the 2nd cover jet suction means, filling rocket fuel, burn in rocket chamber 7, when meeting punching press suction condition, whether head mouse quits work (head mouse can be selected to quit work according to flight survey formula), and air enters through first set and the 2nd cover jet suction means (Laval nozzle does not work), filling rocket fuel, another part air imports in diffusing tube 15 through punching press sucking pipe 19, enter after igniting in rocket chamber 7 and burn, select the open/close states of valve 8 as required, the flame flow produced sprays into Laval nozzle means for influencing through Laval nozzle 20, make the faster of rocket flight.
Fig. 3 is single outer air-breathing duct superposition ram rocket figure, as shown in Figure 3, first time, air-breathing was by head mouse driving the 1st cover jet suction means, filling rocket fuel, burn in diffusing tube 6 typhon mouth after igniting, the flame flow produced drives the 2nd cover jet suction means, filling rocket fuel, burn in rocket chamber 7 after igniting, when meeting punching press suction condition, whether head mouse quits work (head mouse can be selected to quit work according to flight survey formula), and air enters through the 1st cover and the 2nd cover jet suction means (Laval nozzle does not work), filling rocket fuel, air imports in diffusing tube 15 typhon mouth through punching press sucking pipe 19 by another part air, enter after igniting in rocket chamber 7 and burn, select the open/close states of valve 8 as required, the flame flow produced sprays into Laval nozzle means for influencing through Laval nozzle 20, make the faster of rocket flight.
Fig. 4 is that single interior gas duct (with nozzle group) superposes ram rocket figure, as shown in Figure 4, 1 interior air-breathing duct 2, penetrate inside from head mouse 1 front dead center centre to pass to head mouse 1 afterbody centre, head mouse 1 afterbody Laval nozzle 5 (nozzle group), be located in the head mouse afterbody annular wall around interior air-breathing duct 2, the flame of Laval nozzle 5 (nozzle group) sprays and meets at a bit with funnel-like, calculate the distance between intersection point and diffusing tube, hopper centre can produce vacuum (being similar to fluid eddies principle) and be referred to as first time air-breathing, 2nd time air-breathing drives the 1st cover jet suction means by head mouse, filling rocket fuel, burn in diffusing tube 6 typhon mouth after igniting, the flame flow produced drives the 2nd cover jet suction means to be referred to as the 3rd air-breathing, filling rocket fuel, burn in rocket chamber 7 after igniting, rocket is flown, when meeting punching press suction condition, whether head mouse quits work (head mouse can be selected to quit work according to flight survey formula), and air enters through the 1st cover and the 2nd cover jet suction means (Laval nozzle does not work), filling rocket fuel, air imports in diffusing tube 15 typhon mouth through punching press sucking pipe 19 by another part air, enter after igniting in rocket chamber 7 and burn, select the open/close states of valve 8 as required, the flame flow produced sprays into Laval nozzle means for influencing through Laval nozzle 20, make the faster of rocket flight.
Fig. 5 is gas duct superposition ram rocket figure in many branch fork dendroids, as shown in Figure 5, 1 interior air-breathing duct 2 penetrates inside from head mouse 1 front dead center centre and passes to head mouse 1 afterbody centre, in addition four interior air-breathing ducts 2, outside the head mouse 1 front dead center heart, penetrate head mouse 1 inner, and meet on Centromedian interior air-breathing duct 2 in head mouse 1 inside, on the Centromedian interior air-breathing duct 2 connected with dendritic structure, head mouse 1 afterbody Laval nozzle 5 (nozzle group), be located at the head mouse 1 afterbody annular wall in centre around air-breathing duct 2, the flame of Laval nozzle 5 (nozzle group) sprays and meets at a bit with funnel-like, and set the distance (this be vacuum important indicator) of intersection point at diffusing tube, the flame of Laval nozzle sprays with funnel-like, can produce vacuum (approximate flow eddies) in funnel is first time air-breathing, 2nd time air-breathing drives the 1st cover jet suction means by head mouse 1, filling rocket fuel, burn in diffusing tube 6 typhon mouth after igniting, the flame flow produced drives the 2nd cover jet suction means to be referred to as the 3rd air-breathing, filling rocket fuel, burn in rocket chamber 7 after igniting, rocket is flown, when meeting punching press suction condition, whether head mouse quits work (head mouse can be selected to quit work according to flight survey formula), and air enters through the 1st cover and the 2nd cover jet suction means (Laval nozzle does not work), filling rocket fuel, air imports in diffusing tube 15 typhon mouth through punching press sucking pipe 19 by another part air, enter after igniting in rocket chamber 7 and burn, select the open/close states of valve 8 as required, the flame flow produced sprays into Laval nozzle means for influencing through Laval nozzle 20, make the faster of rocket flight.
Fig. 6 is that the equipment of Lavalle effect superposition ram rocket and name of parts are carefully shown.
Embodiment
Superposition ram rocket method of work.The composition of its equipment unit: head mouse 1, interior air-breathing duct 2 (or, and outer suction duct 3), induction chamber 4, Laval nozzle 5, diffusing tube 6, rocket chamber 7, valve 8, igniting place 9, fuel adding point 10, fuel adding point 11, interior air-breathing duct horn mouth 12, fuel adding point 13, fuel adding point this 14, diffusing tube 15, outer air-breathing duct 6, air-breathing shout 17, igniting place 18, punching press sucking pipe 19, Laval nozzle 20, vacuum chamber 21, diffusing tube 22, rocket nozzle 23, rocket envelope 24.
Lavalle effect superposition ram rocket operating principle, as shown in Figure 1, after head mouse 1 (being the traditional rocket needing liquid oxygen to carry out work) startup work, the 1st cover jet suction means is driven (can vacuum to be produced, please read examination as to substances reference sparger part) time row the 1st air-breathing, filling rocket fuel, burn in rocket chamber 7 after igniting, when rocket flight speed can meet punching press condition, whether head mouse quits work (can quit work according to flight survey formula determination head mouse), atmospheric air is stamped to the 1st cover jet suction means and the 2nd cover jet suction means, burn in rocket chamber 7 after filling rocket fuel and igniting, meanwhile another part air is stamped to two punching press sucking pipes 19, import the typhon place of diffusing tube 15, after igniting place 18 is lighted a fire, enter in rocket chamber 7 and burn, select the open/close states of valve 8 as required, the flame flow produced sprays into Laval nozzle means for influencing (please read examination as to substances reference Laval nozzle part) through Laval nozzle 20, make the faster of rocket flight.
Active inspiration and fueling are that something or somebody to fall back on portion mouse 1 (needing traditional rocket of liquid oxygen) drives two cover jet suction meanss to complete, closeall valve 8 when entering space, traditional liquid hydrogen and liquid oxygen combustion manner is used to fly, at the complete reentry of space work, head mouse is lighted a fire again, start Laval nozzle effect superposition ram rocket and return to ground, this rocket is can the rocket of Reusability.

Claims (10)

1. Laval nozzle effect superposition ram rocket method of work: by head mouse 1, interior air-breathing duct 2 (or, and outer suction duct 3), induction chamber 4, Laval nozzle 5, diffusing tube 6, rocket chamber 7, valve 8, igniting place 9, fuel adding point 10, fuel adding point 11, interior air-breathing duct horn mouth 12, fuel adding point 13, fuel adding point this 14, diffusing tube 15, outer air-breathing duct 16, air-breathing shout 17, igniting place 18, punching press sucking pipe 19, Laval nozzle 20, vacuum chamber 21, diffusing tube 22, rocket nozzle 23, rocket envelope 24 form.
2. superpose punching press can be regarded as: 2 grades of punching press air-breathings, Multi-stage ram air-breathing/Laval nozzle group flame sprays with funnel-like and meets at a bit, and negative pressure/punching press sucking pipe 19 suction port place that hopper centre produces arranges fuel adding point/diffusing tube 6 typhon mouth one end and to annotate as fuel chambers/at fuel adding point 13, fuel adding point 14 valve 8 of rocket fuel and catalyzer/design in diffusing tube 15.
3. diffusing tube 6 spray flame, for diffusing tube 15 light a fire/design 1 punching press sucking pipe, design many punching press sucking pipes/closeall valve 8, make firing chamber 7 meet the condition 8 of space flight.
4. single interior air-breathing duct (band Laval nozzle group)---------1 piece of head mouse--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13,An a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----1 outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,An a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------many punching press air intake ducts 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,An a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (band Laval nozzle group)---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------1 piece of head mouse--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------many anemostat 22-------1 rocket nozzle // many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13,Air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----1 outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13,Air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,Air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake ducts 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,A fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------many anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------1 piece of head mouse--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13,An a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----1 outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,An a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake ducts 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,An a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------many anemostat 22-------1 rocket nozzle.
5. single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------1 piece of head mouse--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13,An a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----1 outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16,Suction hole 17--------many fuel addings 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------many punching press air intake ducts 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10,Fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------many anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------1 piece of head mouse--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13,An a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------1 fuel adding point 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16,A suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----1 outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10,Fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------many punching press air intake ducts 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, an a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,An a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/single interior air-breathing duct (Laval nozzle group) and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and many outer air-breathing duct---------1 piece of head mouse--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------many anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16,A suction hole 17--------1 fuel adding 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----1 outer air-breathing ducts 16,A suction hole 17--------1 fuel adding 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16,Suction hole 17--------many fuel addings 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake ducts 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and many outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16,Suction hole 17--------many fuel addings 13, air-breathing duct and single outer air-breathing duct---------1 piece of head mouse--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------many anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16,A suction hole 17--------1 fuel adding 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----1 outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16,Suction hole 17--------many fuel addings 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake ducts 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16,Suction hole 17--------many fuel addings 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------many anemostat 22-------1 rocket nozzle.
6. air-breathing duct---------1 piece of head mouse--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in two branch fork dendroids, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13,Air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------many anemostat 6-----1 outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,Air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake ducts 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,Air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/two branch fork dendroid, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------many anemostat 22-------1 rocket nozzle.
7. air-breathing duct---------1 piece of head mouse--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in many branch fork dendroids, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------1 induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------1 Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------1 fuel adding point 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13,Air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------1 anemostat 6-----1 outer air-breathing duct 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------many anemostat 6-----1 outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, a suction hole 17--------1 fuel adding 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,Air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------1 igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct and single outer air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------1 punching press air intake duct 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake ducts 19---------1 combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------1 Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13,Air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in a fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------1 vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, air-breathing duct---------many pieces of head mouses--------multiple induction chamber 4--------many Laval nozzle 5-------many fuel adding points 10 in fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------1 anemostat 22-------1 rocket nozzle/many branch fork dendroids, fuel adding point 11------many anemostat 6-----many outer air-breathing ducts 16, suction hole 17--------many fuel addings 13, fuel adding point 14--------many igniting place 18-------many punching press air intake duct 19---------many combustion chamber 7------many Laval nozzle 20------many vacuum chamber 21----------many anemostat 22-------1 rocket nozzle.
8. after head mouse 1 (being the traditional rocket needing liquid oxygen to carry out work) startup work, the 1st cover jet suction means is driven (can vacuum to be produced, please read examination as to substances reference sparger part) time row the 1st air-breathing, filling rocket fuel, burn in rocket chamber 7 after igniting, when rocket flight speed can meet punching press condition, whether head mouse quits work (can quit work according to flight survey formula determination head mouse), atmospheric air is stamped to the 1st cover jet suction means and the 2nd cover jet suction means, burn in rocket chamber 7 after filling rocket fuel and igniting, meanwhile another part air is stamped to two punching press sucking pipes 19, import the typhon place of diffusing tube 15, after igniting place 18 is lighted a fire, enter in rocket chamber 7 and burn, select the open/close states of valve 8 as required.
9. Laval nozzle 20 sprays into Laval nozzle means for influencing (please read examination as to substances reference Laval nozzle part), makes the faster of rocket flight.
10. active inspiration and fueling are that something or somebody to fall back on portion mouse 1 (needing traditional rocket of liquid oxygen) drives two cover jet suction meanss to complete, closeall valve 8 when entering space, traditional liquid hydrogen and liquid oxygen combustion manner is used to fly, at the complete reentry of space work, head mouse is lighted a fire again, start Laval nozzle effect superposition ram rocket and return to ground, this rocket is can the rocket of Reusability.
CN201510409699.1A 2015-07-12 2015-07-12 Working method of Laval nozzle effect stacking ram rocket Pending CN105156230A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510409699.1A CN105156230A (en) 2015-07-12 2015-07-12 Working method of Laval nozzle effect stacking ram rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510409699.1A CN105156230A (en) 2015-07-12 2015-07-12 Working method of Laval nozzle effect stacking ram rocket

Publications (1)

Publication Number Publication Date
CN105156230A true CN105156230A (en) 2015-12-16

Family

ID=54797230

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510409699.1A Pending CN105156230A (en) 2015-07-12 2015-07-12 Working method of Laval nozzle effect stacking ram rocket

Country Status (1)

Country Link
CN (1) CN105156230A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101149028A (en) * 2007-11-14 2008-03-26 哈尔滨工业大学 Cooling heat transferring channel for ultra-combustion ramjet engine and rocket engine
CN102400814A (en) * 2011-10-27 2012-04-04 北京航空航天大学 Solid-liquid hybrid rocket ramjet for test
CN103244309A (en) * 2013-04-28 2013-08-14 湖北航天技术研究院总体设计所 Solid rocket punching composite engine shell
CN104595058A (en) * 2015-01-05 2015-05-06 杜善骥 Working method of ram rocket
CN104727978A (en) * 2015-01-06 2015-06-24 杜善骥 Working method of superimposed ram rocket
CN105114209A (en) * 2015-07-22 2015-12-02 杜善骥 Working method of rocket having Laval nozzle effect detonation superposed with pressing oxygen generation functions
CN105134410A (en) * 2015-08-09 2015-12-09 杜善骥 Operating method of detonation superposition ram propulsion and oxygen generation rocket based on Laval nozzle effect

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101149028A (en) * 2007-11-14 2008-03-26 哈尔滨工业大学 Cooling heat transferring channel for ultra-combustion ramjet engine and rocket engine
CN102400814A (en) * 2011-10-27 2012-04-04 北京航空航天大学 Solid-liquid hybrid rocket ramjet for test
CN103244309A (en) * 2013-04-28 2013-08-14 湖北航天技术研究院总体设计所 Solid rocket punching composite engine shell
CN104595058A (en) * 2015-01-05 2015-05-06 杜善骥 Working method of ram rocket
CN104727978A (en) * 2015-01-06 2015-06-24 杜善骥 Working method of superimposed ram rocket
CN105114209A (en) * 2015-07-22 2015-12-02 杜善骥 Working method of rocket having Laval nozzle effect detonation superposed with pressing oxygen generation functions
CN105134410A (en) * 2015-08-09 2015-12-09 杜善骥 Operating method of detonation superposition ram propulsion and oxygen generation rocket based on Laval nozzle effect

Similar Documents

Publication Publication Date Title
CN104727978A (en) Working method of superimposed ram rocket
CN104675558A (en) Stacked suction rocket operation method
CN104675561A (en) Working method of air-breathing rocket
CN104775935A (en) Working method of superposition pressing oxygen production rocket
CN104632467B (en) Rocket thrust chamber provided with acoustic cavity and applied to supersonic airliner and supply system thereof
CN104781143B (en) The aircraft promoted by the turbojet of the fan with reversion
CN104696102A (en) Working method of rocket capable of generating oxygen through superposition aspiration
CN104675557A (en) Working method of air-breathing and oxygen generation rocket
CN104295406B (en) A kind of rocket punching press combined engine with ring-like ejection structure
CN105736178B (en) Combined cycle engine
CN103758663B (en) A kind of rocket based combined cycle Ejector Mode performance test motor
CN103790735B (en) A kind of rocket based combined cycle motor structure changes jet pipe
CN103216361B (en) Novel small-size duct turbofan engine
CN105065138A (en) Working method of detonation punching oxygen-generation rocket based on Laval nozzle effect
CN104595058A (en) Working method of ram rocket
CN103612751A (en) Air amplification type aircraft propulsion device
CN105114209A (en) Working method of rocket having Laval nozzle effect detonation superposed with pressing oxygen generation functions
CN105041508A (en) Working method of Laval nozzle effect superposition ram oxygen production rocket
CN105065137A (en) Working method of Laval nozzle effect detonation superposition ram rocket
CN104929809A (en) Working method of detonation ram rocket
CN104963789A (en) Working method of Laval nozzle effect stamping oxygen production rocket
CN105620751A (en) Saucer type vertical lifting type flight device
CN105156230A (en) Working method of Laval nozzle effect stacking ram rocket
CN104948348A (en) Working method of continuous detonation stamping oxygen production rocket
CN105201688A (en) Working method of air-breathing propulsion and oxygen generation rocket based on De Laval nozzle effect

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20151216

WD01 Invention patent application deemed withdrawn after publication