CN105857641A - Extension-type orbital module - Google Patents
Extension-type orbital module Download PDFInfo
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- CN105857641A CN105857641A CN201610343164.3A CN201610343164A CN105857641A CN 105857641 A CN105857641 A CN 105857641A CN 201610343164 A CN201610343164 A CN 201610343164A CN 105857641 A CN105857641 A CN 105857641A
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- middle deck
- cabin
- stage casing
- interior cabin
- interior
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/12—Artificial satellites; Systems of such satellites; Interplanetary vehicles manned
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- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention relates to an extension-type orbital module comprising an inner cabin (1), a middle cabin (2) and an outer cabin (3). During the process of lifting off by a carrier rocket, the extension-type orbital module is in a fold-up state and its volume is approximately equal to the volume of the outer cabin (3). After entering the orbit, the extension-type orbital module extends outward, thus the space for astronauts to live or work is significantly enlarged. The use of multiple sealing measures ensures the safety of the astronauts inside the cabins. While constructing a space station of the same scale, launching the extension-type orbital module can reduce the number of launches, save launching costs, and save manpower as well as resources. The astronauts do not have to go out of the cabins while the extension-type orbital module is extending outwards; therefore, the operating procedure is simple, the strength is small, the time is short, no accessories are required to be taken along, and few tools are required to be carried.
Description
Technical field
The present invention relates to a kind of scalable orbital module, what after especially its lift-off is docked with space station, its dischargeable capacity can increase stretches
Contracting orbital module.
Background technology
The current orbital module docked with space station launched by carrier rocket only a cabin, the limited volume in a cabin, it is impossible to for relatively
The life of many spacemans and scientific experiments.For the scale at expansion space station, must repeatedly launch.Repeatedly launch, the most uneconomical, again
Consuming the plenty of time of large quantities of scientific and technical personnel, energy and painstaking effort, the benefit of carrier rocket fails maximum performance.
Summary of the invention
The technical problem to be solved in the present invention is to provide that a kind of dischargeable capacity can increase in space, operation sequence is simple, rocket is sent out
Penetrate high efficiency, safe and reliable scalable orbital module.
For solving above-mentioned technical problem, the technical scheme is that
A kind of scalable orbital module, it is transmitted into after space dock with known space station by carrier rocket, stations in the air for a long time, confession
Spaceman life or work.
Scalable orbital module is made up of interior cabin, middle deck, outer cabin.
The interior cabin of scalable orbital module is fastened knot by stage casing, known interior cabin, known interior cabin inner cone section, known interior cabin docking machinery
It is combined into entirety, and the dead in line of this three component.N it is evenly distributed with on the same circumference of the external peripheral surface in this stage casing, interior cabin
Interior cabin bolt hole, this interior cabin bolt hole is close to the rear end in this stage casing, interior cabin, and it extends radially through the barrel in this stage casing, interior cabin.Described
N is the integer more than 2, lower same.This interior cabin bolt hole communicates with the interior cabin screw cap hole of inner side, and this interior cabin screw cap hole is from this interior cabin
On the inner circumferential surface in stage casing in the barrel in this stage casing, interior cabin the most recessed, its axis and this corresponding interior cabin bolt hole
Dead in line, its internal diameter is more than the internal diameter of this interior cabin bolt hole.Bolt and nut, its diameter equals to or slightly less than this interior cabin bolt
The internal diameter in hole, its outer end is from inside to outside exposed through external peripheral surface from this stage casing, interior cabin after this interior cabin bolt hole and its inner
Nut can hide in this interior cabin screw cap hole.In annular, cabin seals gallbladder groove, and its external peripheral surface from this stage casing, interior cabin is radially
It is inwardly recessed in this stage casing, interior cabin barrel, the axis of its circular groove bottom and the dead in line in this stage casing, interior cabin, its longitudinal section
For rectangle.Having multiple interior cabin to seal gallbladder groove on this stage casing, interior cabin, backmost this interior cabin sealing gallbladder groove is positioned at this cabin bolt hole
Front and close to this interior cabin bolt hole, the axial distance that adjacent two these interior cabins seal gallbladder groove is tried one's best little but must be met and hereafter be correlated with
Requirement.This interior cabin each seals has an interior cabin tracheal orifice on gallbladder groove, and this interior cabin tracheal orifice seals the bottom land edge of gallbladder groove from this interior cabin
Extending radially through the barrel in this stage casing, interior cabin, these the interior cabin tracheal orifices whole on this stage casing, interior cabin are respectively positioned on this interior cabin bolt hole same
Dead ahead.This interior cabin tracheal orifice communicates with the interior cabin trachea nut bore of inner side, and this interior cabin trachea nut bore is from this stage casing, interior cabin
In inner circumferential surface this stage casing, interior cabin barrel the most recessed, its axis and the dead in line of this interior cabin tracheal orifice, its internal diameter is more than
The internal diameter of this interior cabin tracheal orifice.This interior cabin each has an interior cabin made by elastic soft material to seal gallbladder in sealing gallbladder groove, should
The structure that interior cabin seals gallbladder is identical with the structure of bicycle tyre inner bag, and it is looped around this interior cabin and seals in the groove bottom of gallbladder groove, its
Inner circumferential surface and this interior cabin seal the groove bottom of gallbladder groove and are in close contact, and it is close that its inner circumferential surface extends radially inward an interior cabin
Envelope courage pipe, the gallbladder chamber of inner chamber and this interior cabin sealing gallbladder that this interior cabin seals courage pipe communicates, and its opening is by this interior cabin trachea
Exposing behind hole in this interior cabin trachea nut bore, this cabin is sealed gallbladder by the cabin trachea nut being positioned in this cabin trachea nut bore
Trachea is tightened in this interior cabin tracheal orifice.The outlet side of known valve cock seals the opening of courage pipe and puts in this from this interior cabin
Interior cabin seals in courage pipe, and this valve cock is pressed abd fixed on this interior cabin and seals on courage pipe by known valve cock nut, but this valve
The inlet end of mouth will not expose from the inner circumferential surface in this stage casing, interior cabin.Public pump connects with the inlet end of this valve cock
Connecing, seal this interior cabin after gallbladder squeezes into gas by this valve cock to this interior cabin and seal the volumetric expansion of gallbladder, the gas squeezed into will not be let out
Go out, if but this valve cock nut is unscrewed, the gas squeezed into will seal courage pipe by this interior cabin and automatically release.In this interior cabin
Being evenly distributed with n location, interior cabin straight trough vertically on the external peripheral surface of section, location, this interior cabin straight trough is the most recessed
In the barrel in this stage casing, interior cabin, its transverse section is rectangle, and end face is arc surface and seals gallbladder groove close to this interior cabin preceding thereafter,
Its front end face is arc surface and the front end close to this stage casing, interior cabin.
On scalable orbital module, the middle deck stage casing of middle deck is cylindric, and it is set in outside Shang Neicang stage casing, interior cabin, and its axis is interior with this
The external peripheral surface movable contact in the dead in line in stage casing, cabin, its inner circumferential surface and this stage casing, interior cabin, its axial length is equal to being somebody's turn to do
The axial length in stage casing, interior cabin.N middle deck bolt hole it is evenly distributed with on the same circumference of the external peripheral surface in this middle deck stage casing,
This middle deck bolt hole is close to the rear end in this middle deck stage casing, and it extends radially through the barrel in this middle deck stage casing.This middle deck bolt hole is with interior
The middle deck screw cap hole of side communicates, and this middle deck screw cap hole is this middle deck stage casing the most recessed from the inner circumferential surface in this middle deck stage casing
In barrel, the dead in line of its axis and this corresponding middle deck bolt hole, its internal diameter is more than the internal diameter of this middle deck bolt hole.Band spiral shell
Cap bolt, its diameter equal to or slightly less than the internal diameter of this middle deck bolt hole, its outer end from inside to outside through after this middle deck bolt hole from
The external peripheral surface in this middle deck stage casing exposes and the nut of its inner can hide in this middle deck screw cap hole.Annular middle deck seals gallbladder
Groove, its external peripheral surface from this middle deck stage casing this middle deck stage casing barrel the most recessed, the axle of its circular groove bottom
Line and the dead in line in this stage casing, interior cabin, its longitudinal section is rectangle.Multiple middle deck is had to seal gallbladder groove, finally on this middle deck stage casing
This middle deck of one, face seals gallbladder groove and is positioned at the front of this middle deck bolt hole and close to this middle deck bolt hole, and adjacent two these middle decks seal
The axial distance of gallbladder groove is tried one's best little but must be met hereafter related request.This middle deck each seals has a middle deck tracheal orifice on gallbladder groove,
The bottom land that this middle deck tracheal orifice seals gallbladder groove from this middle deck extends radially through the barrel in this middle deck stage casing, whole on this middle deck stage casing
This middle deck tracheal orifice is respectively positioned on the dead ahead of this middle deck bolt hole same.This middle deck tracheal orifice and the middle deck trachea nut bore of inner side
Communicate, the barrel in this middle deck trachea nut bore inner circumferential surface from this middle deck stage casing this middle deck stage casing the most recessed, its axle
Line and the dead in line of this middle deck tracheal orifice, its internal diameter is more than the internal diameter of this middle deck tracheal orifice.This middle deck each has in sealing gallbladder groove
The middle deck that one is made by elastic soft material seals gallbladder, and this middle deck seals the structure of gallbladder and the structure phase of bicycle tyre inner bag
With, it is looped around this middle deck and seals in the groove bottom of gallbladder groove, and the groove bottom that its inner circumferential surface seals gallbladder groove with this middle deck closely connects
Touch, its inner circumferential surface extend radially inward middle deck and seals courage pipe, this middle deck seal the inner chamber of courage pipe with in this
Cabin seals the gallbladder chamber of gallbladder and communicates, and its opening, by exposing after this middle deck tracheal orifice in this middle deck trachea nut bore, is positioned in this
This middle deck sealing courage pipe is tightened in this middle deck tracheal orifice by the middle deck trachea nut in the trachea nut bore of cabin.Known valve
The opening that the outlet side of mouth seals courage pipe from this middle deck puts in this middle deck sealing courage pipe, and known valve cock nut is by this gas
Door mouth is pressed abd fixed on this middle deck and seals on courage pipe, but the inlet end of this valve cock will not be from the inner circumferential surface in this middle deck stage casing
Expose.Public pump is connected with the inlet end of this valve cock and by this valve cock after this middle deck sealing gallbladder squeezes into gas
This middle deck seals the volumetric expansion of gallbladder, and the gas squeezed into will not release, if but this valve cock nut is unscrewed, the gas squeezed into is just
Courage pipe can be sealed by this middle deck automatically to release.Be evenly distributed with on the external peripheral surface in this middle deck stage casing n vertically in
Location, cabin straight trough, this middle deck location straight trough, in the barrel in its this middle deck stage casing the most recessed, its transverse section is rectangle,
Thereafter end face is arc surface and seals gallbladder groove close to this middle deck preceding, and its front end face is arc surface and close to before this middle deck stage casing
End.N middle deck preceding thread hole it is evenly distributed with, this middle deck preceding thread hole on the same circumference of the inner circumferential surface in this middle deck stage casing
Between the waist and front end in this middle deck stage casing, it radially gos deep in the barrel in this middle deck stage casing, but does not extends through this
The barrel in middle deck stage casing.Screw thread is had, this screw thread and the screw-threaded engagement on bolt and nut in this middle deck preceding thread hole.In this middle deck
Being evenly distributed with n middle deck rear thread hole on the same circumference of the inner circumferential surface of section, this middle deck rear thread hole is close in this middle deck
The rear end of section, it radially gos deep in the barrel in this middle deck stage casing, but does not extends through the barrel in this middle deck stage casing.This middle deck
Rear thread has screw thread in hole, this screw thread and the screw-threaded engagement on bolt and nut.One of n this middle deck preceding thread hole should with n
The projection on this scalable orbital module transverse section of one of the middle deck rear thread hole overlapping and with n on this interior cabin in one of cabin bolt hole
Be projected in same radially.N middle deck positioning threads it is evenly distributed with on the same circumference of the external peripheral surface in this middle deck stage casing
Hole, this middle deck positioning spiro pit extends radially through the barrel in this middle deck stage casing, and it is close to the front end in this middle deck stage casing.Without nut
Middle deck bolt is by extroversion part and interior forms to part, the screw thread of this extroversion part and the screw thread in this middle deck positioning spiro pit
Engagement, this extroversion part fastens and is arranged in this middle deck positioning spiro pit, and this is interior to being partly non-threaded cylinder, this non-threaded
Cylindrical diameter equal to this Shang Nei cabin, interior cabin location straight trough width, this non-threaded cylinder be positioned at this cabin location straight trough in and
Its end face positions the groove bottom movable contact of straight trough with this interior cabin.This middle deck positioning spiro pit, this middle deck bolt hole, this interior cabin spiral shell
Keyhole projection on this scalable orbital module transverse section not same radially.This stage casing, interior cabin is fully contracted in this middle deck stage casing
Time middle, the front end face in this stage casing, interior cabin flushes with the front end face in this middle deck stage casing, the front end face of location, this interior cabin straight trough and corresponding positions
The cylindrical face of cylinder of non-threaded of this middle deck bolt put coincide contact, the axis of this interior cabin bolt hole with in corresponding this
The axis in rear thread hole, cabin just overlaps.When this stage casing, interior cabin is the most fully stretched out from this middle deck stage casing, location, this interior cabin straight trough
The cylindrical face of cylinder of non-threaded of rear end face and this middle deck bolt of relevant position coincide and contact, this interior cabin bolt hole
Axis just overlaps with the axis in this corresponding middle deck preceding thread hole.
" axial distance that adjacent two these interior cabins seal gallbladder groove is tried one's best little but must be met hereafter related request " mentioned above, Yi Jisuo
State " adjacent two these middle decks seal the axial distance of gallbladder groove and try one's best little but must meet hereafter related request ", described " be hereafter correlated with
Require " refer to: when in the middle deck stage casing that the stage casing, interior cabin on interior cabin is fully contracted on middle deck, seal gallbladder groove phase with this middle deck
The axial location of logical middle deck trachea nut bore mutually must stagger with the axial location of the interior cabin sealing gallbladder groove on this interior cabin.
The outer cabin of scalable orbital module is by boring section, known outer cabin docking machinery fastening knot behind stage casing, known outer cabin, known outer cabin
It is combined into entirety, and the dead in line of this three component.This stage casing, outer cabin is set on middle deck outside middle deck stage casing, its axis and this middle deck
The external peripheral surface movable contact in the dead in line in stage casing, its inner circumferential surface and this middle deck stage casing, its axial length is equal in this
The axial length in stage casing, cabin.N preceding thread hole, outer cabin it is uniformly distributed on the same circumference of the inner circumferential surface in this stage casing, outer cabin, should
Preceding thread hole, outer cabin is between waist and the front end in this stage casing, outer cabin, and it radially gos deep in the barrel in this stage casing, outer cabin,
But do not extend through the barrel in this stage casing, outer cabin.Having screw thread in this preceding thread hole, outer cabin, this screw thread is nibbled with the screw thread on bolt and nut
Close.N rear thread hole, outer cabin, this rear thread hole, outer cabin it is evenly distributed with on the same circumference of the inner circumferential surface in this stage casing, outer cabin
Close to the rear end in this stage casing, outer cabin, it radially gos deep in the barrel in this stage casing, outer cabin, but does not extends through this stage casing, outer cabin
Barrel.Screw thread is had, this screw thread and the screw-threaded engagement on bolt and nut in this rear thread hole, outer cabin.N this preceding thread hole, outer cabin
One of overlapping with the projection on this scalable orbital module transverse section of one of n this rear thread hole, outer cabin and individual with n on this middle deck in
One of cabin bolt hole be projected in same radially.N it is evenly distributed with on the same circumference of the external peripheral surface in this stage casing, outer cabin
Outer cabin positioning spiro pit, this outer cabin positioning spiro pit extends radially through the barrel in this stage casing, outer cabin, and it is close to before this stage casing, outer cabin
End.Outer cabin bolt without nut by extroversion part and interior forms to part, and the screw thread of this extroversion part positions spiral shell with this outer cabin
Screw-threaded engagement in pit, this extroversion part fastens and is arranged in this outer cabin positioning spiro pit, this interior to part be non-threaded cylinder
Body, the cylindrical diameter of this non-threaded is equal to the width of middle deck location straight trough on this middle deck, and this non-threaded cylinder is positioned at this middle deck
Position in straight trough and its end face positions the groove bottom movable contact of straight trough with this middle deck.On this outer cabin positioning spiro pit, this middle deck
Middle deck bolt hole on middle deck positioning spiro pit, this middle deck, the interior cabin bolt hole on this interior cabin, cross-section at this scalable orbital module
Projection on face not same radially.When this middle deck stage casing is fully contracted in this stage casing, outer cabin, the front end face in this middle deck stage casing
Flush with the front end face in this stage casing, outer cabin, this outer cabin bolt of front end face and the relevant position of this middle deck location straight trough without spiral shell
The cylindrical face of cylinder of stricture of vagina coincide and contacts, and the axis of this middle deck bolt hole just weighs with the axis in this corresponding rear thread hole, outer cabin
Close.When this middle deck stage casing is the most fully stretched out from this stage casing, outer cabin, the rear end face of this middle deck location straight trough should with relevant position
The cylindrical face of cylinder of non-threaded of outer cabin bolt coincide and contacts, the axis of this middle deck bolt hole and spiral shell before this corresponding outer cabin
The axis of pit just overlaps.
The assembly program of scalable orbital module is such that
The first step, by the inner chamber in middle deck stage casing on Shang Neicang stage casing, interior cabin insertion middle deck, makes the middle deck positioning threads on this middle deck
Location, the interior cabin straight trough that hole is directed on this stage casing, interior cabin, then screws in middle deck bolt, when this in this middle deck positioning spiro pit
When the cylindrical end face of non-threaded of middle deck bolt positions the groove bottom gentle touchdown of straight trough with this interior cabin, this middle deck is positioned
Bolt and this middle deck positioning spiro pit fasten and combine, now this middle deck bolt not external peripheral surface dew from this middle deck stage casing
Go out.
Second step, inserts middle deck stage casing on middle deck in the inner chamber in Shang Waicang stage casing, outer cabin, makes the outer cabin positioning threads on this outer cabin
The middle deck location straight trough that hole is directed on this middle deck stage casing, then screws in outer cabin bolt, when this in this outer cabin positioning spiro pit
When the cylindrical end face of non-threaded of outer cabin bolt positions the groove bottom gentle touchdown of straight trough with this middle deck, this outer cabin is positioned
Bolt fastens with this outer cabin positioning spiro pit and combines, now this outer cabin bolt not external peripheral surface dew from this stage casing, outer cabin
Go out.
3rd step, on middle deck, the rear end face in middle deck stage casing aligns with the rear end face in Shang Waicang stage casing, outer cabin, the stage casing, interior cabin on interior cabin
Remove forward, after the outer end of one of n bolt and nut screws in the outer cabin on this outer cabin after passing the middle deck bolt hole on this middle deck
In screwed hole, this middle deck is fastened with this outer cabin and is combined into entirety.Pump is connected also with the inlet end of the valve cock on this middle deck
Seal gallbladder by this valve cock middle deck on this middle deck and squeeze into gas, after the volumetric expansion of this middle deck sealing gallbladder, this middle deck is sealed in
In this outer cabin.
4th step, the rear end face in Shang Neicang stage casing, interior cabin aligns with the rear end face in middle deck stage casing on middle deck, another n bolt and nut
One of outer end screw in the middle deck rear thread hole on this middle deck after the interior cabin bolt hole on this interior cabin, by this interior cabin with in this
Cabin fastens and is combined into entirety.Pump is connected and by this valve cock on this interior cabin with the inlet end of the valve cock on this interior cabin
Interior cabin seals gallbladder and squeezes into gas, is sealed in this middle deck in this interior cabin after the volumetric expansion of this interior cabin sealing gallbladder.
5th step, docks the outer cabin on outer cabin machinery and docks machinery docking with the known propelling module on known propelling module.
After completing above-mentioned installation, spaceman can be moved in interior cabin by the known hatch door on Shang Nei cabin, interior cabin docking machinery, then closes
Close this hatch door.At this moment this scalable orbital module just can be launched by carrier rocket.
Scalable orbital module enter the orbit after known relevant rocket firing on propelling module, this scalable orbital module is carried out posture adjustment or boosting,
The docking machinery of the interior cabin on interior cabin is made to dock machinery docking with the known space station on space station;Then it is to stretch to be somebody's turn to do
In scalable orbital module is allowed to cabin, space increases, and operation sequence is divided into stretching, extension preparation, for the first time stretching, extension, second time to stretch, structure
The programs such as life or working environment.
Stretch and prepare: in interior cabin, stretch unrelated spaceman with scalable orbital module, dock machinery by this Shang Nei cabin, interior cabin
On hatch door transfer to space station, be then shut off this hatch door.The spaceman carrying out stretching operation in staying this interior cabin is dressed known
Spacesuit.
Stretching for the first time: unscrew the valve cock nut on interior cabin, in interior cabin seals gallbladder, gas is released, the most scalable rail
In cabin, road, air releases the most therewith.Again from this after the bolt and nut on this interior cabin middle deck rear thread hole from middle deck being screwed out
Interior cabin bolt hole on interior cabin exits.Under the promotion of mobile device, this middle deck the most slowly slides relative to this interior cabin,
When the non-threaded cylinder of the middle deck bolt on this middle deck contacts with the rear end face of location, the interior cabin straight trough on this interior cabin, will
The outer end of this bolt and nut is by the interior cabin bolt hole on this interior cabin, in the middle deck preceding thread hole being then threaded on this middle deck, and will
This interior cabin and this middle deck again fasten and are combined into entirety.Pump is connected with the inlet end of the valve cock on this interior cabin and passes through this gas
Door mouth seals gallbladder and again squeezes into gas to this interior cabin, again this interior cabin is sealed in this middle deck after the volumetric expansion of this interior cabin sealing gallbladder
In.
Second time stretches: unscrew the valve cock nut on middle deck, and in middle deck on this middle deck seals gallbladder, gas is released.By this middle deck
On bolt and nut rear thread hole, outer cabin on outer cabin in screw out after again the middle deck bolt hole from this middle deck exits.Moving
Under the promotion of dynamic device, the most slowly slide relative to this middle deck in this outer cabin, when the nothing of the outer cabin bolt on this outer cabin
When threaded cylinder contacts with the rear end face of the middle deck location straight trough on this middle deck, by the outer end of this bolt and nut by this middle deck
On middle deck bolt hole, in the preceding thread hole, outer cabin being then threaded on this outer cabin, this middle deck is fastened again with this outer cabin and is combined into
Overall.Pump is connected with the inlet end of the valve cock on this middle deck and seals gallbladder by this valve cock to this middle deck squeezes into gas again
Body, is sealed in this middle deck in this outer cabin again after the volumetric expansion of this middle deck sealing gallbladder.
Build life or working environment: in scalable orbital module, again inject air.
Hereafter spaceman just can be lived in scalable orbital module or work, but in it, space has expanded many.
Mobile device mentioned above is the known retro-rocket on propelling module, and after this retro-rocket is lighted a fire, the thrust of generation overcomes
Frictional resistance, can make outer cabin slide backward relative to middle deck, or makes middle deck internal cabin mutually slide backward.
For extending the working life of scalable orbital module, the interior cabin on this scalable orbital module seals gallbladder, middle deck seals gallbladder badly
In spatial environments, the palpus energy long period is the most aging.
For ensureing spaceman safety, having the component in the space of spaceman life or work in scalable orbital module, corner should be adopted
Use fillet structure.
Scalable orbital module in stretching process in order to not damage, the size of the thrust produced after the igniting of retro-rocket on propelling module
Must strictly control with the duration of ignition:
When stretching for the first time, incipient stage thrust acts on the stiction of middle deck slightly larger than interior cabin.This middle deck relative to this interior cabin to
When the most slowly sliding, by the size adjustment of thrust to the force of sliding friction acting on this middle deck equal to this interior cabin.In on this middle deck
When the non-threaded cylinder of cabin bolt soon contacts with the rear end face of location, the interior cabin straight trough on this interior cabin, this retro-rocket stops
Only work, after this middle deck continues slip one section the most relatively because of inertia, the non-threaded cylinder of this middle deck bolt and this interior cabin
When the rear end face of location straight trough contacts, this middle deck is just reduced to zero with the relative velocity in this interior cabin.
When second time stretches, incipient stage thrust acts on the stiction in outer cabin slightly larger than middle deck.This outer cabin relative to this middle deck to
When the most slowly sliding, by the size adjustment of thrust to the force of sliding friction acting on this outer cabin equal to this middle deck.Outside on this outer cabin
When the non-threaded cylinder of cabin bolt soon contacts with the rear end face of the middle deck location straight trough on this middle deck, this retro-rocket stops
Only work, after slip one section the most relatively is continued because of inertia in this outer cabin, the non-threaded cylinder of this outer cabin bolt and this middle deck
When the rear end face of location straight trough contacts, this outer cabin is just reduced to zero with the relative velocity of this middle deck.
Owing to the size of frictional force is non-constant, retro-rocket may need repeatedly to light a fire and control well the time lighted a fire, and constantly carries out
Regulation.
As required, the external peripheral surface in the outer Shang Waicang stage casing, cabin of scalable orbital module can install solar panel.
In order to reduce impact force in the stretching process of scalable orbital module, following buffer structure can be used:
The cylindrical diameter of non-threaded of the middle deck bolt on reduction middle deck, then one, set has on this non-threaded cylinder
Elastic soft overcoat, but on this non-threaded cylinder of holster, after this overcoat, the external diameter of this overcoat positions straight trough still equal to Shang Nei cabin, interior cabin
Width.
Reduce the cylindrical diameter of non-threaded of outer cabin bolt on outer cabin, then on this non-threaded cylinder, overlap one have
Elastic soft overcoat, but on this non-threaded cylinder of holster, after this overcoat, the external diameter of this overcoat positions straight trough still equal to middle deck on middle deck
Width.
After using such structure, the lift-off of scalable orbital module is passed through to stretch after entering the orbit, and its dischargeable capacity significantly increases, and is available for relatively
Many aerospace are within it lived or work.Build identical scale spatial station, compare single cabin and launch, launch scalable orbital module and can reduce
Emitting times, saves transmitting funds, uses manpower and material resources sparingly, large number of ground scientific research personnel can be allowed to have the more time to be engaged in scientific research.
This core technology can be greatly improved the transmitting benefit of rocket.
After using such structure, seal, due between middle deck and interior cabin owing to there being multiple middle deck to seal gallbladder between outer cabin and middle deck
Have multiple interior cabin to seal gallbladder to seal, multi-sealed meaning multiple security.This core technology can ensure that spaceman is at scalable orbital module
Interior safety.
After using such structure, spaceman need not go out cabin, just can complete the stretching, extension of scalable orbital module in scalable orbital module,
Program is simple, and intensity is little, and the operating time is the longest, needs the instrument carried few.
Accompanying drawing explanation
Below in conjunction with the accompanying drawings the detailed description of the invention of the present invention is described in further detail.
Fig. 1 is scalable orbital module longitudinal sectional drawing when being in contraction state, has interior cabin bolt hole, middle deck on this profile
Preceding thread hole, middle deck rear thread hole.
Fig. 2 is scalable orbital module longitudinal sectional drawing when being in contraction state, has middle deck bolt hole, outer cabin on this profile
Preceding thread hole, rear thread hole, outer cabin.
Fig. 3 is scalable orbital module longitudinal sectional drawing when being in contraction state, this profile has middle deck positioning spiro pit and
Location, interior cabin straight trough.
Fig. 4 is scalable orbital module longitudinal sectional drawing when being in contraction state, this profile has outer cabin positioning spiro pit and
Middle deck location straight trough.
Fig. 5 is the interior cabin bolt hole on scalable orbital module, middle deck preceding thread hole, middle deck rear thread hole, middle deck bolt hole, outer
Preceding thread hole, cabin, rear thread hole, outer cabin, middle deck positioning spiro pit, location, interior cabin straight trough, outer cabin positioning spiro pit, middle deck location
Straight trough projection on the transverse section of this scalable orbital module.
Fig. 6 is the longitudinal sectional drawing after scalable orbital module shown in Fig. 1 stretches for the first time.
Fig. 7 is the longitudinal sectional drawing after scalable orbital module shown in Fig. 2 stretches for the first time.
Fig. 8 is the longitudinal sectional drawing after the second time of scalable orbital module shown in Fig. 1 stretches.
Fig. 9 is the longitudinal sectional drawing after the second time of scalable orbital module shown in Fig. 2 stretches.
Detailed description of the invention
A kind of scalable orbital module, it is transmitted into after space dock with known space station by carrier rocket, stations in the air for a long time, confession
Spaceman life or work.
As shown in Fig. 1 to Fig. 9 respectively schemes, scalable orbital module is made up of interior cabin 1, middle deck 2, outer cabin 3.
As shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 4, Fig. 6, Fig. 7, Fig. 8, Fig. 9 respectively scheme, the interior cabin 1 of scalable orbital module by
In known, stage casing, cabin 1a, known interior cabin inner cone section 6, known interior cabin docking machinery 7 fasten and are combined into entirety, and this three structure
The dead in line of part;As shown in Fig. 1, Fig. 5, Fig. 6, Fig. 8 respectively scheme, the same circle of the external peripheral surface of this interior cabin stage casing 1a
Cabin bolt hole 1d in being evenly distributed with n on week, this interior cabin bolt hole 1d is close to the rear end of this interior cabin stage casing 1a, and it is radially
Run through the barrel of this interior cabin stage casing 1a;Described n is the integer more than 2, lower same;This interior cabin bolt hole 1d and the interior cabin of inner side
Screw cap hole 1e communicates, and this interior cabin screw cap hole 1e is from the inner circumferential surface of this interior cabin stage casing 1a in this interior cabin the most recessed
In the barrel of section 1a, the dead in line of its axis and this corresponding interior cabin bolt hole 1d, its internal diameter is more than this interior cabin bolt hole 1d
Internal diameter;Bolt and nut 9, its diameter internal diameter equal to or slightly less than this interior cabin bolt hole 1d, its outer end from inside to outside passes
Expose from the external peripheral surface of this interior cabin stage casing 1a after this interior cabin bolt hole 1d and the nut of its inner can hide in this interior cabin spiral shell
In cap aperture 1e;In annular, cabin seals gallbladder groove 1b, and it is from external peripheral surface this interior cabin the most recessed of this interior cabin stage casing 1a
In the 1a barrel of stage casing, the axis of its circular groove bottom and the dead in line of this interior cabin stage casing 1a, its longitudinal section is rectangle;
Having multiple interior cabin to seal gallbladder groove 1b on the stage casing 1a of this interior cabin, backmost this interior cabin sealing gallbladder groove 1b is positioned at this cabin bolt hole
The front of 1d and close to this interior cabin bolt hole 1d, the axial distance that adjacent two these interior cabins seal gallbladder groove 1b is tried one's best little but must be met
Hereafter related request;This interior cabin each seals has an interior cabin tracheal orifice 1k on gallbladder groove 1b, and this interior cabin tracheal orifice 1k is from this interior cabin
The bottom land sealing gallbladder groove 1b extends radially through the barrel of this interior cabin stage casing 1a, these the interior cabin tracheas whole on the stage casing 1a of this interior cabin
Hole 1k is respectively positioned on the dead ahead of this interior cabin bolt hole 1d same;This interior cabin tracheal orifice 1k and the interior cabin trachea nut bore of inner side
1c communicates, and this interior cabin trachea nut bore 1c is from the inner circumferential surface of this interior cabin stage casing 1a this stage casing, interior cabin 1a cylinder the most recessed
In wall, its axis and the dead in line of this interior cabin tracheal orifice 1k, its internal diameter internal diameter more than this interior cabin tracheal orifice 1k;Each should
Interior cabin seals in gallbladder groove 1b the interior cabin having to be made by elastic soft material and seals gallbladder 8, this interior cabin seal the structure of gallbladder 8 with from
The structure of driving tire inner bag is identical, and it is looped around this interior cabin and seals in the groove bottom of gallbladder groove 1b, and its inner circumferential surface is interior with this
Cabin seals the groove bottom of gallbladder groove 1b and is in close contact, and its inner circumferential surface extends radially inward an interior cabin and seals courage pipe 8a;
The gallbladder chamber of inner chamber and this interior cabin sealing gallbladder 8 that this interior cabin seals courage pipe 8a communicates, and its opening is by this interior cabin tracheal orifice 1k
After expose in this interior cabin trachea nut bore 1c, the cabin trachea nut 8b being positioned in this cabin trachea nut bore 1c is by this cabin
Seal courage pipe 8a to be fixed in this interior cabin tracheal orifice 1k;The outlet side of known valve cock seals courage pipe 8a's from this interior cabin
Opening puts in this interior cabin and seals in courage pipe 8a, and this valve cock is pressed abd fixed on this interior cabin and seals courage by known valve cock nut
On pipe 8a, but the inlet end of this valve cock will not expose from the inner circumferential surface of this interior cabin stage casing 1a;Public pump with
The inlet end of this valve cock connects, and seals this interior cabin after gallbladder 8 squeezes into gas by this valve cock to this interior cabin and seals the volume of gallbladder 8
Expanding, the gas squeezed into will not release, if but this valve cock nut is unscrewed, the gas squeezed into will seal gallbladder by this interior cabin
Trachea 8a releases automatically;As shown in Fig. 3, Fig. 5, the external peripheral surface of this interior cabin stage casing 1a is evenly distributed with n along axle
To interior cabin location straight trough 1g, this interior cabin location straight trough 1g this interior cabin the most recessed stage casing 1a barrel in, it is cross-section
Face is rectangle, thereafter end face be arc surface and close to this interior cabin preceding seal gallbladder groove 1b, its front end face be arc surface and close to should
The front end of interior cabin stage casing 1a.
Illustrate:
In each figure of Fig. 1 to Fig. 9, all take n=4;In each figure of Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7, Fig. 8, Fig. 9,
In on interior cabin 1, the interior cabin of stage casing, cabin 1a seals gallbladder groove 1b is 3.
Owing to the structure of interior cabin sealing gallbladder 8 is identical with the structure of bicycle tyre inner bag, on it, accessory is just known, thus does not makees
Describe in detail, as valve cock and interior cabin seal the respective outer side edges of courage pipe 8a.
As shown in Fig. 1 to Fig. 9 respectively schemes, on scalable orbital module, the middle deck stage casing 2a of middle deck 2 is cylindric, and it is set in interior cabin
In on 1 outside the 1a of stage casing, cabin, its axis and the dead in line of this interior cabin stage casing 1a, its inner circumferential surface is with this interior cabin stage casing 1a's
External peripheral surface movable contact, its axial length axial length equal to this interior cabin stage casing 1a;Such as Fig. 2, Fig. 5, Fig. 7, Fig. 9
Shown in each figure, the same circumference of the external peripheral surface of this middle deck stage casing 2a is evenly distributed with n middle deck bolt hole 2d, in this
Cabin bolt hole 2d is close to the rear end of this middle deck stage casing 2a, and it extends radially through the barrel of this middle deck stage casing 2a;This middle deck bolt
Hole 2d communicates with the middle deck screw cap hole 2e of inner side, this middle deck screw cap hole 2e from the inner circumferential surface of this middle deck stage casing 2a along footpath
In the barrel of recessed this middle deck stage casing 2a, the dead in line of its axis and corresponding this middle deck bolt hole 2d, its internal diameter is more than
The internal diameter of this middle deck bolt hole 2d;Bolt and nut 9, its diameter internal diameter equal to or slightly less than this middle deck bolt hole 2d, its
Outer end is from inside to outside through exposing from the external peripheral surface of this middle deck stage casing 2a after this middle deck bolt hole 2d and the nut of its inner can
To hide in this middle deck screw cap hole 2e;As shown in Fig. 2, Fig. 7, Fig. 9 respectively scheme, annular middle deck seals gallbladder groove 2b, and it is from this
In external peripheral surface this middle deck stage casing 2a barrel the most recessed of middle deck stage casing 2a, the axis of its circular groove bottom with
The dead in line of this interior cabin stage casing 1a, its longitudinal section is rectangle;Multiple middle deck is had to seal gallbladder groove 2b on the 2a of this middle deck stage casing,
Backmost this middle deck seals gallbladder groove 2b and is positioned at the front of this middle deck bolt hole 2d and close to this middle deck bolt hole 2d, and adjacent two
The axial distance of this middle deck individual sealing gallbladder groove 2b is tried one's best little but must be met hereafter related request;This middle deck each seals on gallbladder groove 2b
The bottom land having a middle deck tracheal orifice 2k, this middle deck tracheal orifice 2k to seal gallbladder groove 2b from this middle deck extends radially through this middle deck stage casing
The barrel of 2a, whole this middle deck tracheal orifice 2k on the 2a of this middle deck stage casing be respectively positioned on same this middle deck bolt hole 2d just before
Side;This middle deck tracheal orifice 2k communicates with middle deck trachea nut bore 2c of inner side, and this middle deck trachea nut bore 2c is from this middle deck stage casing
In the barrel of inner circumferential surface this middle deck stage casing the most recessed 2a of 2a, its axis and the dead in line of this middle deck tracheal orifice 2k,
Its internal diameter internal diameter more than this middle deck tracheal orifice 2k;This middle deck each has one to be made by elastic soft material in sealing gallbladder groove 2b
Middle deck seal gallbladder 12, this middle deck seal gallbladder 12 structure identical with the structure of bicycle tyre inner bag, it is looped around this middle deck
Sealing in the groove bottom of gallbladder groove 2b, its inner circumferential surface and this middle deck seal the groove bottom of gallbladder groove 2b and are in close contact, its inner periphery
Extending radially inward a middle deck on surface and seal courage pipe 12a, the inner chamber that this middle deck seals courage pipe 12a is close with this middle deck
The gallbladder chamber of envelope gallbladder 12 communicates, and its opening, by exposing in this middle deck trachea nut bore 2c after this middle deck tracheal orifice 2k, is positioned at
This middle deck sealing courage pipe 12a is fixed on this middle deck tracheal orifice by the middle deck trachea nut 12b in this middle deck trachea nut bore 2c
In 2k;The opening that the outlet side of known valve cock seals courage pipe 12a from this middle deck puts in this middle deck sealing courage pipe 12a,
This valve cock is pressed abd fixed on this middle deck and seals on courage pipe 12a by known valve cock nut, but the inlet end of this valve cock will not
Expose from the inner circumferential surface of this middle deck stage casing 2a;Public pump is connected with the inlet end of this valve cock and by this valve
Mouth seals this middle deck after gallbladder 12 squeezes into gas to this middle deck and seals the volumetric expansion of gallbladder 12, and the gas squeezed into will not release, if but
Being unscrewed by this valve cock nut, the gas squeezed into will seal courage pipe 12a by this middle deck and automatically release;As shown in Figure 4,
N middle deck location straight trough 2g vertically it is evenly distributed with on the external peripheral surface of this middle deck stage casing 2a;This middle deck location straight trough
2g, in the barrel of its most recessed this middle deck stage casing 2a, its transverse section is rectangle, and end face is arc surface and close thereafter
This middle deck preceding seals gallbladder groove 2b, and its front end face is arc surface and the front end close to this middle deck stage casing 2a;As Fig. 1, Fig. 5,
Fig. 6, Fig. 8 are evenly distributed with n middle deck preceding thread on the same circumference of the inner circumferential surface of this middle deck stage casing 2a shown in respectively scheming
Hole 2h, this middle deck preceding thread hole 2h is between waist and the front end of this middle deck stage casing 2a, and it radially gos deep into this middle deck
In the barrel of stage casing 2a, but do not extend through the barrel of this middle deck stage casing 2a;Screw thread is had, this spiral shell in this middle deck preceding thread hole 2h
Stricture of vagina and the screw-threaded engagement on bolt and nut 9;It is evenly distributed with n on the same circumference of the inner circumferential surface of this middle deck stage casing 2a
Individual middle deck rear thread hole 2i, this middle deck rear thread hole 2i is close to the rear end of this middle deck stage casing 2a, and it radially gos deep in this
In the barrel of stage casing, cabin 2a, but do not extend through the barrel of this middle deck stage casing 2a;Screw thread is had, this spiral shell in this middle deck rear thread hole 2i
Stricture of vagina and the screw-threaded engagement on bolt and nut 9;One of n this middle deck preceding thread hole 2h and n this middle deck rear thread hole 2i it
One projection on this scalable orbital module transverse section overlapping and with n on this interior cabin 1 in being projected in of one of cabin bolt hole 1d
Same radially;As shown in Fig. 3, Fig. 5, the same circumference of the external peripheral surface of this middle deck stage casing 2a is evenly distributed with n
Middle deck positioning spiro pit 2f, this middle deck positioning spiro pit 2f extend radially through the barrel of this middle deck stage casing 2a, and it is close to this middle deck
The front end of stage casing 2a;Middle deck bolt 14 without nut by extroversion part and interior forms to part, the screw thread of this extroversion part
With the screw-threaded engagement in this middle deck positioning spiro pit 2f, this extroversion part fastens and is arranged in this middle deck positioning spiro pit 2f, should
Interior is non-threaded cylinder to part, and the cylindrical diameter of this non-threaded is the width of interior cabin location straight trough 1g equal on this interior cabin 1,
This non-threaded cylinder is positioned in the straight trough 1g of location, this cabin and its end face positions the groove bottom movable contact of straight trough 1g with this cabin;
As it is shown in figure 5, this middle deck positioning spiro pit 2f, this middle deck bolt hole 2d, this interior cabin bolt hole 1d are at this scalable orbital module
Projection on transverse section not same radially;As shown in Fig. 1, Fig. 3 respectively scheme, this interior cabin stage casing 1a is fully contracted in this middle deck
Time in the 2a of stage casing, the front end face of this interior cabin stage casing 1a flushes with the front end face of this middle deck stage casing 2a, location, this interior cabin straight trough 1g
The cylindrical face of cylinder of non-threaded of front end face and this middle deck bolt 14 of relevant position coincide and contact, this interior cabin bolt hole
The axis of 1d just overlaps with the axis of corresponding this middle deck rear thread hole 2i;As shown in Fig. 3, Fig. 6, Fig. 8 respectively scheme, this is interior
When stage casing, cabin 1a the most fully stretches out from the 2a of this middle deck stage casing, the rear end face of location, this interior cabin straight trough 1g should with relevant position
The cylindrical face of cylinder of non-threaded of middle deck bolt 14 coincide contact, the axis of this interior cabin bolt hole 1d with in corresponding this
The axis of preceding thread hole, cabin 2h just overlaps.
Illustrate:
In each figure of Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7, Fig. 8, Fig. 9, the middle deck of middle deck stage casing 2a on middle deck 2
Sealing gallbladder groove 2b is 3.
Owing to the structure of middle deck sealing gallbladder 12 is identical with the structure of bicycle tyre inner bag, on it, accessory is just known, thus does not makees
Describe in detail, as valve cock and middle deck seal the respective outer side edges between courage pipe 12a.
" axial distance that adjacent two these interior cabins seal gallbladder groove 1b is tried one's best little but must be met hereafter related request " mentioned above, with
And described " axial distance that adjacent two these middle decks seal gallbladder groove 2b is tried one's best little but must be met hereafter related request ", described " under
Literary composition related request " refer to: as in figure 2 it is shown, when the middle deck stage casing that the interior cabin stage casing 1a on interior cabin 1 is fully contracted on middle deck 2
Time in 2a, the axial location sealing middle deck trachea nut bore 2c that gallbladder groove 2b communicates with this middle deck must be with the interior cabin on this interior cabin 1
The axial location sealing gallbladder groove 1b mutually staggers.
As shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 4, Fig. 6, Fig. 7, Fig. 8, Fig. 9 respectively scheme, the outer cabin 3 of scalable orbital module by
Bore section 4 behind known outer cabin stage casing 3a, known outer cabin, known outer cabin docking machinery 5 fastens and is combined into entirety, and this three structure
The dead in line of part;As shown in Fig. 1 to Fig. 9 respectively schemes, this outer cabin stage casing 3a is set on middle deck 2 outside the 2a of middle deck stage casing, its
Axis and the external peripheral surface movable contact of the dead in line of this middle deck stage casing 2a, its inner circumferential surface and this middle deck stage casing 2a,
Its axial length axial length equal to this middle deck stage casing 2a;As shown in Fig. 2, Fig. 5, Fig. 7 Fig. 9 respectively schemes, this stage casing, outer cabin
Being uniformly distributed n outer cabin preceding thread hole 3d on the same circumference of the inner circumferential surface of 3a, it is outer that this outer cabin preceding thread hole 3d is positioned at this
Between waist and the front end of stage casing, cabin 3a, it radially gos deep in the barrel of this outer cabin stage casing 3a, but it is outer not extend through this
The barrel of stage casing, cabin 3a;Screw thread is had, this screw thread and the screw-threaded engagement on bolt and nut 9 in the preceding thread hole 3d of this outer cabin;Should
N outer cabin rear thread hole 3e, this rear thread hole, outer cabin it is evenly distributed with on the same circumference of the inner circumferential surface of outer cabin stage casing 3a
3e is close to the rear end of this outer cabin stage casing 3a, and it radially gos deep in the barrel of this outer cabin stage casing 3a, but it is outer not extend through this
The barrel of stage casing, cabin 3a;Screw thread is had, this screw thread and the screw-threaded engagement on bolt and nut 9 in the rear thread hole 3e of this outer cabin;As
Shown in Fig. 5, one of one of n this outer cabin preceding thread hole 3d and n this outer cabin rear thread hole 3e is horizontal at this scalable orbital module
Projection on section overlapping and with one of n middle deck bolt hole 2d on this middle deck 2 be projected in same radially;Such as Fig. 4, figure
Shown in 5, the same circumference of the external peripheral surface of this outer cabin stage casing 3a being evenly distributed with n outer cabin positioning spiro pit 3f, this is outer
Cabin positioning spiro pit 3f extends radially through the barrel of this outer cabin stage casing 3a, and it is close to the front end of this outer cabin stage casing 3a;Without nut
Outer cabin bolt 13 is by extroversion part and interior forms to part, the screw thread of this extroversion part with in this outer cabin positioning spiro pit 3f
Screw-threaded engagement, this extroversion part fastens and is arranged in this outer cabin positioning spiro pit 3f, this interior to part be non-threaded cylinder,
The cylindrical diameter of this non-threaded is equal to the width of middle deck location straight trough 2g on this middle deck 2, and this non-threaded cylinder is positioned at this middle deck
Position in straight trough 2g and its end face positions the groove bottom movable contact of straight trough 2g with this middle deck;As it is shown in figure 5, location, this outer cabin
Interior on middle deck positioning spiro pit 2f on screwed hole 3f, this middle deck 2, the middle deck bolt hole 2d on this middle deck 2, this interior cabin 1
Cabin bolt hole 1d, the projection on this scalable orbital module transverse section not same radially;As shown in Fig. 2, Fig. 4, Fig. 7,
When this middle deck stage casing 2a is fully contracted in the stage casing 3a of this outer cabin, the front end face of this middle deck stage casing 2a is with this outer cabin stage casing 3a's
Front end face flushes, the front end face of this middle deck location straight trough 2g and the non-threaded cylinder of this outer cabin bolt 13 of relevant position
The face of cylinder coincide contact, the axis of this middle deck bolt hole 2d just overlaps with the axis of corresponding this outer cabin rear thread hole 3e;
As shown in Fig. 4, Fig. 9, when this middle deck stage casing 2a the most fully stretches out from the stage casing 3a of this outer cabin, this middle deck location straight trough 2g
The cylindrical face of cylinder of non-threaded of rear end face and this outer cabin bolt 13 of relevant position coincide and contact, this middle deck bolt hole
The axis of 2d just overlaps with the axis of corresponding this outer cabin preceding thread hole 3d.
The assembly program of scalable orbital module is such that
The first step, as it is shown on figure 3, by the inner chamber of middle deck stage casing 2a on stage casing, cabin 1a insertion middle deck 2 interior on interior cabin 1, make
Location, the interior cabin straight trough 1g that middle deck positioning spiro pit 2f on this middle deck 2 is directed on the stage casing 1a of this interior cabin, then fixed to this middle deck
Position screwed hole 2f screws in middle deck bolt 14, when the cylindrical end face of the non-threaded of this middle deck bolt 14 and this interior cabin
When positioning the groove bottom gentle touchdown of straight trough 1g, this middle deck bolt 14 is fastened with this middle deck positioning spiro pit 2f and combines,
Now this middle deck bolt 14 does not exposes from the external peripheral surface of this middle deck stage casing 2a;
Second step, as shown in Figure 4, by the inner chamber of outer cabin stage casing 3a on the outer cabin 3 of middle deck stage casing 2a insertion on middle deck 2, makes
The middle deck location straight trough 2g that outer cabin positioning spiro pit 3f on this outer cabin 3 is directed on the 2a of this middle deck stage casing, then fixed to this outer cabin
Position screwed hole 3f screws in outer cabin bolt 13, when the cylindrical end face of non-threaded and this middle deck of this outer cabin bolt 13
When positioning the groove bottom gentle touchdown of straight trough 2g, this outer cabin bolt 13 is fastened with this outer cabin positioning spiro pit 3f and combines,
Now this outer cabin bolt 13 does not exposes from the external peripheral surface of this outer cabin stage casing 3a;
3rd step, as in figure 2 it is shown, the rear end face of middle deck stage casing 2a and the rear end face of outer cabin stage casing 3a on outer cabin 3 on middle deck 2
Alignment, the interior cabin stage casing 1a on interior cabin 1 removes forward, during the outer end of one of n bolt and nut 9 passes on this middle deck 2
Screw in the outer cabin rear thread hole 3e on this outer cabin 3 after the bolt hole 2d of cabin, this middle deck 2 and the fastening of this outer cabin 3 are combined into whole
Body;Pump is connected with the inlet end of the valve cock on this middle deck 2 and seals gallbladder 12 by this valve cock middle deck on this middle deck 2
Squeeze into gas, after the volumetric expansion of this middle deck sealing gallbladder 12, this middle deck 2 is sealed in this outer cabin 3;
4th step, as it is shown in figure 1, the rear end face of stage casing, cabin 1a and the rear end face of middle deck stage casing 2a on middle deck 2 on interior cabin 1
Alignment, the outer end of one of another n bolt and nut 9 screws on this middle deck 2 after the interior cabin bolt hole 1d on this interior cabin 1
Middle deck rear thread hole 2i in, this interior cabin 1 is fastened with this middle deck 2 and is combined into entirety;Pump and the valve on this interior cabin 1
The inlet end of mouth connects and seals gallbladder 8 by this valve cock interior cabin on this interior cabin 1 squeezes into gas, and this interior cabin seals gallbladder 8
After volumetric expansion, this interior cabin 1 is sealed in this middle deck 2;
5th step, as shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 4 respectively scheme, docks machinery 5 with known by the outer cabin on outer cabin 3
Known propelling module docking machinery 11 on propelling module 10 docks;After completing above-mentioned installation, spaceman can be by interior cabin 1
Known hatch door on interior cabin docking machinery 7 is moved in interior cabin 1, is then shut off this hatch door;At this moment this scalable orbital module is just
Can be launched by carrier rocket.
Scalable orbital module enter the orbit after known relevant rocket firing on propelling module 10, this scalable orbital module is carried out posture adjustment or helps
Push away, make the docking machinery 7 of the interior cabin on interior cabin 1 dock machinery docking with the known space station on space station;Then
Being to stretch space in this scalable orbital module is allowed to cabin to increase, operation sequence is divided into stretching, extension to prepare, first time stretches, second time is stretched
The programs such as exhibition, structure life or working environment;
Stretch and prepare: in interior cabin 1, stretch unrelated spaceman with scalable orbital module, by cabin docking machinery interior on this interior cabin 1
Hatch door on device 7 transfers to space station, is then shut off this hatch door;The spaceman carrying out stretching operation in staying this interior cabin 1 is worn
Wear known spacesuit;
Stretch for the first time: as it is shown in figure 1, the valve cock nut unscrewed on interior cabin 1, in interior cabin seals gallbladder 8, gas is released,
In the most scalable orbital module, air releases the most therewith;By the middle deck from middle deck 2 of the bolt and nut 9 on this interior cabin 1
Again the interior cabin bolt hole 1d from this interior cabin 1 exits after rear thread hole 2i screws out;Under the promotion of mobile device, in this
The most slowly slide in this interior cabin 1 relative, cabin 2, as it is shown on figure 3, when the nothing of the middle deck bolt 14 on this middle deck 2
When threaded cylinder contacts with the rear end face of location, the interior cabin straight trough 1g on this interior cabin 1, as shown in Figure 6 by this bolt and nut 9
Outer end by the interior cabin bolt hole 1d on this interior cabin 1, be then threaded in the middle deck preceding thread hole 2h on this middle deck 2, should
Interior cabin 1 again fastens with this middle deck 2 and is combined into entirety;Pump is connected with the inlet end of the valve cock on this interior cabin 1 and passes through
This valve cock seals gallbladder 8 and again squeezes into gas to this interior cabin, is sealed in this interior cabin 1 again after the volumetric expansion of this interior cabin sealing gallbladder 8
In this middle deck 2;
Second time stretches: as it is shown in fig. 7, the valve cock nut unscrewed on middle deck 2, middle deck on this middle deck 2 is sealed gallbladder 12
Interior gas is released;After the bolt and nut 9 on this middle deck 2 outer cabin rear thread hole 3e on outer cabin 3 being screwed out again from this
Middle deck bolt hole 2d on cabin 2 exits;Under the promotion of mobile device, this outer cabin 3 this middle deck 2 relative is axially rearward
Slowly slide, as shown in Figure 4, on the non-threaded cylinder and this middle deck 2 of the outer cabin bolt 13 on this outer cabin 3
During the rear end face contact of location, cabin straight trough 2g, as it is shown in figure 9, by the outer end of this bolt and nut 9 by this middle deck 2
Cabin bolt hole 2d, is then threaded in the outer cabin preceding thread hole 3d on this outer cabin 3, is again fastened with this outer cabin 3 by this middle deck 2
It is combined into entirety;Pump is connected with the inlet end of the valve cock on this middle deck 2 and seals gallbladder 12 by this valve cock to this middle deck
Again squeeze into gas, again this middle deck 2 is sealed in this outer cabin 3 after the volumetric expansion of this middle deck sealing gallbladder 12;
Build life or working environment: as shown in Figure 8, Figure 9, in scalable orbital module, again inject air;
Hereafter spaceman just can be lived in scalable orbital module or work, but in it, space has expanded many.
Mobile device mentioned above is the known retro-rocket on propelling module 10, after this retro-rocket is lighted a fire, and the thrust gram of generation
Take frictional resistance, the relative middle deck 2 in outer cabin 3 can be made to slide backward, or make the mutually internal cabin of middle deck 21 slide backward.
For extending the working life of scalable orbital module, the interior cabin on this scalable orbital module seals gallbladder 8, middle deck seals gallbladder 12 and exists
In severe spatial environments, the palpus energy long period is the most aging.
As shown in Fig. 8, Fig. 9 respectively scheme, for ensureing spaceman safety, in scalable orbital module, there are spaceman life or the sky of work
Component between, corner should use fillet structure.
Scalable orbital module is not in order to damage in stretching process, and after the retro-rocket igniting on propelling module 10, the thrust of generation is big
Little and the duration of ignition must strictly control:
When stretching for the first time, incipient stage thrust acts on the stiction of middle deck 2 slightly larger than interior cabin 1;This middle deck 2 relatively should
Time the most slowly slip in interior cabin 1, by the size adjustment of thrust to the force of sliding friction acting on this middle deck 2 equal to this interior cabin 1;
The rear end face that the non-threaded cylinder of the middle deck bolt 14 on this middle deck 2 positions straight trough 1g with the interior cabin on this interior cabin 1 is fast
Time to be contacted, this retro-rocket quits work, after this middle deck 2 continues slip one section the most relatively because of inertia, and this middle deck location spiral shell
When the non-threaded cylinder of bolt 14 contacts with the rear end face of location, this interior cabin straight trough 1g, this middle deck 2 speed relative with this interior cabin 1
Degree is just reduced to zero;
When second time stretches, incipient stage thrust acts on the stiction in outer cabin 3 slightly larger than middle deck 2;Relatively should in this outer cabin 3
When middle deck 2 the most slowly slides, by the size adjustment of thrust to the force of sliding friction acting on this outer cabin 3 equal to this middle deck 2;
The rear end face that the non-threaded cylinder of the outer cabin bolt 13 on this outer cabin 3 positions straight trough 2g with the middle deck on this middle deck 2 is fast
Time to be contacted, this retro-rocket quits work, after slip one section the most relatively is continued because of inertia in this outer cabin 3, and location, this outer cabin spiral shell
When the non-threaded cylinder of bolt 13 contacts with the rear end face of this middle deck location straight trough 2g, this outer cabin 3 speed relative with this middle deck 2
Degree is just reduced to zero;
Owing to the size of frictional force is non-constant, retro-rocket may need repeatedly to light a fire and control well the time lighted a fire, and constantly carries out
Regulation.
As required, solar panel can be installed on the external peripheral surface of outer cabin stage casing 3a in scalable orbital module outer cabin 3.
In order to reduce impact force in the stretching process of scalable orbital module, following buffer structure can be used:
As shown in Fig. 3, Fig. 5 respectively scheme, the cylindrical diameter of non-threaded of the middle deck bolt 14 on reduction middle deck 2, then
A resilient soft overcoat of tool is overlapped on this non-threaded cylinder, as it is shown in figure 5, but this overcoat on this non-threaded cylinder of holster
After this overcoat external diameter still equal on interior cabin 1 interior cabin position straight trough 1g width;
As shown in Figure 4, Figure 5, reduce the cylindrical diameter of non-threaded of outer cabin bolt 13 on outer cabin 3, then in this nothing
A resilient soft overcoat of tool is overlapped on threaded cylinder, as it is shown in figure 5, but should after this overcoat on this non-threaded cylinder of holster
The external diameter of overcoat positions the width of straight trough 2g still equal to the middle deck on middle deck 2.
Illustrate:
The design idea of the present invention is described below.Understand design idea, just grasp technical key point and manufacture requirements.
One. scalable orbital module is made up of interior cabin 1, middle deck 2, outer cabin 2, and during launching, three cabins are in contraction state,
Structure on it of entering the orbit after docking with space station ensures that it passes through stretching, extension and can expand inner space.
Two. although on interior cabin 1, the structure of cabin sealing gallbladder 8 is identical with the structure of bicycle tyre inner bag, but the use mesh of the two
Difference.After the inflation of bicycle tyre inner bag, cover tire is propped up, utilize its elasticity to having collided cushioning effect in riding;Should
After interior cabin seals gallbladder 8 inflation, utilize it elastic and flexibility is by the external peripheral surface of stage casing, cabin 1a on interior cabin 1 and middle deck 2
Gap between the inner circumferential surface of upper middle deck stage casing 2a blocks, and plays positive sealing effect.Have any different in the relative position of the two.From
Trachea, trachea nut, valve cock inlet end and valve cock nut on driving tire inner bag are all exposed;Interior cabin seals gallbladder 8
On interior cabin seal courage pipe 8a, interior cabin trachea nut 8b, valve cock, valve cock nut are all hidden in stage casing, interior cabin 1a barrel
Hole in, design it is intended that these accessories do not hinder the activity of spaceman in scalable orbital module.Interior cabin does not has in sealing gallbladder 8
When having gas, it is flat, utilizes its elasticity to be allowed to be contracted in interior cabin and seals in gallbladder groove 1b, because of without stage casing, cabin in hindering
1a and the middle deck stage casing 2a on middle deck 2 relative slip in stretching process.
Although the structure of middle deck sealing gallbladder 12 is identical with the structure of bicycle tyre inner bag on middle deck 2, but the application target of the two is not
With.After the inflation of bicycle tyre inner bag, cover tire is propped up, utilize its elasticity to having collided cushioning effect in riding;Middle deck is close
After envelope gallbladder 12 inflation, utilize it elastic and flexibility is by the external peripheral surface of middle deck stage casing 2a on middle deck 2 and outer cabin on outer cabin 3
Gap between the inner circumferential surface of stage casing 3a blocks, and plays positive sealing effect.Have any different in the relative position of the two, bicycle quick
Trachea, trachea nut, valve cock inlet end and valve cock nut on tire inner bag are all exposed;During middle deck seals on gallbladder 12
Cabin sealing courage pipe 12a, middle deck trachea nut 12b, valve cock, valve cock nut are all hidden in the barrel of middle deck stage casing 2a,
Design it is intended that the inner circumferential surface of this outer cabin stage casing 3a can contact with the external peripheral surface of this middle deck stage casing 2a and stretch
During exhibition the two can axially opposed slip, middle deck seals in gallbladder 12 when not having gas it and for flat and is contracted in middle deck and seals
In gallbladder groove 2b, because of without hindering outer cabin stage casing 3a and the middle deck stage casing 2a on middle deck 2 relative slip in stretching process.
Multiple interior cabin on interior cabin 1 seals gallbladder 8, and the multiple middle decks on middle deck 2 seal gallbladder 12, all play multi-sealed effect, many
Resealing is multiple security.Being intended to of this design guarantees the safety of spaceman in scalable orbital module.
Interior cabin seals the length of service of the quality scalable orbital module of decision of gallbladder 8 or middle deck sealing gallbladder 12.In the spatial environments of place
It is elastic and flexibility palpus holding was not lost efficacy for more than 10 years and its structure is not damaged.
Three. the middle deck bolt 14 on middle deck 2 and location, the interior cabin straight trough 1g reliable fit to be had on interior cabin 1, just can make
Can only slide vertically in limited range in this middle deck 2 this interior cabin 1 relative, it is impossible to relatively rotate, it is impossible to diametrically opposite movement,
Will not be separated from one another.
Outer cabin bolt 13 on outer cabin 3 and the middle deck location straight trough 2g reliable fit to be had on middle deck 2, just can make this outer
Cabin 3 this middle deck 2 relative can only slide vertically in limited range, it is impossible to relatively rotates, it is impossible to diametrically opposite movement, no
Can be separated from one another.
Four. when the middle deck bolt 14 on middle deck 2 contacts with the front end face of location, the interior cabin straight trough 1g on interior cabin 1, this is interior
In on cabin 1, the axis of cabin bolt hole 1d just overlaps with the axis of middle deck rear thread hole 2i on this middle deck 2;This middle deck location spiral shell
When bolt 14 contacts with the rear end face of location, this interior cabin straight trough 1g, spiral shell before middle deck on this interior cabin bolt hole 1d axis and this middle deck 2
The axis of pit 2h just overlaps;The purpose of this design is to make assembling or stretching smoothly, quickly.
When outer cabin bolt 13 on outer cabin 3 contacts with the front end face of the middle deck location straight trough 2g on middle deck 2, this middle deck 2
The axis of upper middle deck bolt hole 2d just overlaps with the axis of outer cabin rear thread hole 3e on this outer cabin 3;This outer cabin bolt 13
When contacting with the rear end face of this middle deck location straight trough 2g, the axis of this middle deck bolt hole 2d and preceding thread hole, outer cabin on this outer cabin 3
The axis of 3d just overlaps.The purpose of this design is also for making assembling or stretching smoothly, quickly.
Five. the interior cabin tracheal orifice 1k on interior cabin 1 is respectively positioned on the dead ahead of same interior cabin bolt hole 1d, middle deck on this interior cabin 1
Middle deck tracheal orifice 2k on 2 is respectively positioned on the dead ahead of same middle deck bolt hole 2d on this middle deck 2.This design purpose be for
Make assembling or stretch easily and fast.
Six. the axial distance that on interior cabin 1, adjacent two interior cabins seal gallbladder groove 1b is the least, and on middle deck 2, adjacent two middle decks are close
The axial distance of envelope gallbladder groove 2b is the least.The purpose of this design is that in making scalable orbital module stretch rear deck, space is the biggest.
Seven. when in the middle deck stage casing 2a that the interior cabin stage casing 1a on interior cabin 1 is fully contracted on middle deck 2, with middle deck 2 in
Cabin seals the axial location of middle deck trachea nut bore 2c that gallbladder groove 2b communicates must seal gallbladder groove 1b's with the interior cabin on this interior cabin 1
Axial location mutually staggers.Purpose of this design is in order to the sealing function after allowing cabin on this interior cabin 1 seal gallbladder 8 inflation does not loses
Effect.
Eight. the middle deck preceding thread hole 2h on middle deck 2, middle deck rear thread hole 2i go deep into the barrel of middle deck stage casing 2a on this middle deck 2
In but not through;Outer cabin preceding thread hole 3d on outer cabin 3, outer cabin rear thread hole 3e go deep into outer cabin stage casing 3a on this outer cabin 3
In barrel but not through.The purpose of this design is in order in preventing scalable orbital module, air leaks.
Nine. the middle deck bolt 14 on middle deck 2 must fasten combination with middle deck positioning spiro pit 2f and it is not from this middle deck stage casing
The external peripheral surface of 2a exposes;Outer cabin bolt on outer cabin 3 13 and outer cabin positioning spiro pit 3f must fasten combine and its not
Expose from the external peripheral surface of this outer cabin stage casing 3a.The intention of this design: one, prevents this middle deck bolt 14 or this is outer
Cabin bolt 13 loses positioning action or disintegrates when stretching because being displaced outwardly;Its two, prevent this middle deck bolt 14
Because hindering this outer cabin 3 this middle deck 2 relative to slide when being displaced outwardly and cause and stretching;Its three, prevent this middle deck bolt 14 because of to
Interior movement causes hindering this middle deck 2 this interior cabin 1 relative to slide when stretching;Its four, this outer cabin bolt 13 is from this stage casing, outer cabin
The external peripheral surface of 3a exposes the assembling being unfavorable for scalable orbital module, affects again attractive in appearance.
Ten. the outer cabin positioning spiro pit 3f of outer cabin stage casing 3a, the middle deck positioning threads of middle deck stage casing 2a on middle deck 2 on outer cabin 3
Hole 2f, middle deck bolt hole 2d, the interior cabin bolt hole 1d of interior stage casing, cabin 1a on interior cabin 1, on scalable orbital module transverse section
Projection the most not same radially.The purpose of this design is to make this outer cabin stage casing 3a, this middle deck stage casing 2a, this stage casing, interior cabin
1a force dispersion, uniformly.
11.In stretching process, it is necessary for allowing air in scalable orbital module outwards release.If air does not releases,
Owing to being vacuum out of my cabin in stretching process, outer cabin 3 or middle deck 2 under the inner air pressure effect of cabin will mutually internally cabin 1 quickly to
Rear motion, is then sharp impacts, causes structural deterioration.Air releases can get rid of this sharp impacts.But owing to not having in cabin
The spaceman having air, operation to stretch work must dress spacesuit, and the life-support system on spacesuit can ensure its safety.
12.Have a talk below the extension effects of scalable orbital module.
If on outer cabin 3, the axial length of outer cabin stage casing 3a is h=5.0m, external diameter is d=4.4m, this outer cabin stage casing 3a, in
On cabin 2 on middle deck stage casing 2a, interior cabin 1 in the radial thickness of stage casing, cabin 1a be a=0.15m, on the 2a of this middle deck stage casing
Above a middle deck seals gallbladder groove 2b and interior cabin, one, foremost on the distance of this 2a rear end, middle deck stage casing, this interior cabin stage casing 1a
The distance sealing gallbladder groove 1b and this 1a rear end, stage casing, interior cabin is b=0.3m.
Utilize formula
Calculate to obtain the volume V in space in the stage casing 3a of this outer cabin3=66m3。
Utilize formula
Calculate scalable orbital module be fully extended after outer cabin stage casing 3a on it, middle deck stage casing 2a, 1a inner space, stage casing, interior cabin
Total measurement (volume) V=163.4m3, it is about 2.5 times of stage casing, outer cabin 3a interior space volume.It is to say, for increasing space station
Scale, the scalable orbital module of twice emitting, can support when the orbital module in five transmitting only one of which cabins.Data above shows, can
Expansion rail cabin has real practical value.
Along with emerging of new nacelle material, the thickness of bulkhead is expected to be greatly reduced.If scalable orbital module is made up of 9 single cabins,
The radial thickness of bulkhead is reduced to a '=0.05m, axial length in outermost list cabin and external diameter is constant and the structure in each single cabin
In the case of constant,
Utilize formula
Calculate the volume of inner space, outermost list cabin is VOutward=72.6m3。
Utilize formula
Calculate scalable orbital module be fully extended after the total measurement (volume) V '=510m of inner space on it3, about outermost list cabin is internal empty
Between 7 times of volume.It is to say, be the scale increasing space station, the scalable orbital module of primary emission, can support when seven times are launched
The orbital module in only one of which cabin.Imagining accordingly, current space station and current orbital module need not be launched respectively and dock,
Can two combine into one that primary emission is just crowned with success, if so will save huge research funding and huge human cost.The most also may be used
The imagination, by the application extension of scalable orbital module, its alternative satellite being currently loaded with spaceman, also replace and currently investigate row
Star or the spacecraft being loaded with spaceman of survey of deep space, the title of scalable orbital module need only be changed into " scalable satellite "
Or " scalable airship ".
Certainly, according to operation principle and the core technology of scalable orbital module, this scalable orbital module can by more single cabins or relatively
Few single cabin composition, or substitute current manned satellite or manned spaceship with this scalable orbital module, these changes all fall within this
Within the protection domain of invention.
Claims (6)
1. a scalable orbital module, it is transmitted into after space docks with space station by carrier rocket, stations aerial for a long time, supply
Spaceman life or work;It is characterized in that:
Scalable orbital module is made up of interior cabin (1), middle deck (2), outer cabin (3);
The interior cabin (1) of scalable orbital module is by stage casing, interior cabin (1a), interior cabin inner cone section (6), interior cabin docking machinery (7)
Fastening is combined into entirety, and the dead in line of this three component;On the same circumference of the external peripheral surface in stage casing, described interior cabin (1a)
Be evenly distributed with cabin bolt hole (1d) in n, described interior cabin bolt hole (1d) close to the rear end in stage casing, described interior cabin (1a),
It extends radially through the barrel in stage casing, described interior cabin (1a);Described n is the integer more than 2, lower same;Described interior cabin bolt hole
(1d) communicate with interior cabin screw cap hole (1e) of inner side, interior from stage casing, described interior cabin (1a) of described interior cabin screw cap hole (1e)
On circumferential surface in the barrel of the most recessed stage casing, described interior cabin (1a), its axis and corresponding described interior cabin bolt hole
(1d) dead in line, its internal diameter is more than the internal diameter of described interior cabin bolt hole (1d);Bolt and nut (9), its diameter etc.
In or be slightly less than the internal diameter of described interior cabin bolt hole (1d), its outer end from inside to outside through after described interior cabin bolt hole (1d) from
The external peripheral surface in stage casing, described interior cabin (1a) exposes and the nut of its inner can hide in described interior cabin screw cap hole (1e);
In annular, cabin seals gallbladder groove (1b), the most recessed described interior cabin of its external peripheral surface from stage casing, described interior cabin (1a)
In stage casing (1a) barrel, the axis of its circular groove bottom and the dead in line in stage casing, described interior cabin (1a), its longitudinal section
For rectangle;Having multiple interior cabin to seal gallbladder groove (1b) on stage casing, described interior cabin (1a), backmost a described interior cabin seals gallbladder groove
(1b) front in described cabin bolt hole (1d) it is positioned at and close to described cabin bolt hole (1d), adjacent two described interior cabins
The axial distance of sealing gallbladder groove (1b) is tried one's best little but must be met hereafter related request;Each described interior cabin seals on gallbladder groove (1b)
Having interior cabin tracheal orifice (1k), described interior cabin tracheal orifice (1k) seals the bottom land of gallbladder groove (1b) radially from described interior cabin
Run through the barrel in stage casing, described interior cabin (1a), all positions of whole described interior cabin tracheal orifice (1k) on stage casing, described interior cabin (1a)
Dead ahead in same described interior cabin bolt hole (1d);Described interior cabin tracheal orifice (1k) and the interior cabin trachea nut bore of inner side
(1c) communicate, described interior cabin trachea nut bore (1c) the most recessed institute of inner circumferential surface from stage casing, described interior cabin (1a)
Stating in stage casing, interior cabin (1a) barrel, its axis and the dead in line of described interior cabin tracheal orifice (1k), its internal diameter is interior more than described
The internal diameter of cabin tracheal orifice (1k);There is an interior cabin made by elastic soft material in each described interior cabin in sealing gallbladder groove (1b)
Sealing gallbladder (8), the structure that described interior cabin seals gallbladder (8) is identical with the structure of bicycle tyre inner bag, and it is looped around described interior cabin
Sealing in the groove bottom of gallbladder groove (1b), its inner circumferential surface and described interior cabin seal the groove bottom of gallbladder groove (1b) and are in close contact,
Its inner circumferential surface extends radially inward an interior cabin and seals courage pipe (8a);Described interior cabin seals the inner chamber of courage pipe (8a)
The gallbladder chamber sealing gallbladder (8) with described interior cabin communicates, and its opening exposes in described by after described interior cabin tracheal orifice (1k)
In cabin trachea nut bore (1c), it is positioned at cabin trachea nut (8b) in described cabin trachea nut bore (1c) by described
Cabin seals courage pipe (8a) and is fixed in described interior cabin tracheal orifice (1k);The outlet side of valve cock seals courage from described interior cabin
The opening of pipe (8a) puts in described interior cabin and seals in courage pipe (8a), and described valve cock is pressed abd fixed on by valve cock nut
Described interior cabin seals on courage pipe (8a), but the inlet end of described valve cock will not be from the inner periphery in stage casing, described interior cabin (1a)
Surface is exposed;Pump is connected with the inlet end of described valve cock, seals gallbladder (8) by described valve cock to described interior cabin and beats
After entering gas, described interior cabin seals the volumetric expansion of gallbladder (8), and the gas squeezed into will not release, if but by described valve cock nut
Unscrewing, the gas squeezed into will seal courage pipe (8a) by described interior cabin and automatically release;Outside stage casing, described interior cabin (1a)
Being evenly distributed with n location straight trough, interior cabin (1g) vertically on circumferential surface, location straight trough, described interior cabin (1g) is radially
Being inwardly recessed in the barrel in stage casing, described interior cabin (1a), its transverse section is rectangle, and end face is arc surface and close to preceding thereafter
Described interior cabin seals gallbladder groove (1b), and its front end face is arc surface and the front end close to stage casing, described interior cabin (1a);
On scalable orbital module, the middle deck stage casing (2a) of middle deck (2) is cylindric, and it is set in upper interior stage casing, cabin, interior cabin (1)
(1a) outward, its axis and the dead in line in stage casing, described interior cabin (1a), its inner circumferential surface and stage casing, described interior cabin (1a)
External peripheral surface movable contact, its axial length is equal to the axial length in stage casing, described interior cabin (1a);Described middle deck stage casing (2a)
External peripheral surface same circumference on be evenly distributed with n middle deck bolt hole (2d), described middle deck bolt hole (2d) is close
The rear end of described middle deck stage casing (2a), it extends radially through the barrel of described middle deck stage casing (2a);Described middle deck bolt hole (2d)
Communicating with the middle deck screw cap hole (2e) of inner side, described middle deck screw cap hole (2e) is from the inner circle weekly form of described middle deck stage casing (2a)
On face in the barrel of the most recessed described middle deck stage casing (2a), the axle of its axis and corresponding described middle deck bolt hole (2d)
Line overlaps, and its internal diameter is more than the internal diameter of described middle deck bolt hole (2d);Bolt and nut (9), its diameter equals to or slightly less than
The internal diameter of described middle deck bolt hole (2d), its outer end from inside to outside through after described middle deck bolt hole (2d) from described middle deck
The external peripheral surface of section (2a) exposes and the nut of its inner can hide in described middle deck screw cap hole (2e);Annular middle deck
Sealing gallbladder groove (2b), it is from the most recessed described middle deck stage casing (2a) of the external peripheral surface of described middle deck stage casing (2a)
In barrel, the axis of its circular groove bottom and the dead in line in stage casing, described interior cabin (1a), its longitudinal section is rectangle;Institute
Stating and have multiple middle deck to seal gallbladder groove (2b) on middle deck stage casing (2a), backmost described middle deck sealing gallbladder groove (2b) is positioned at
The front of described middle deck bolt hole (2d) and close to described middle deck bolt hole (2d), adjacent two described middle decks seal gallbladder groove (2b)
Axial distance try one's best little but hereafter related request must be met;Each described middle deck seals has a middle deck trachea on gallbladder groove (2b)
Hole (2k), the bottom land that described middle deck tracheal orifice (2k) seals gallbladder groove (2b) from described middle deck extends radially through described middle deck
Section (2a) barrel, the whole described middle deck tracheal orifice (2k) on described middle deck stage casing (2a) be respectively positioned on same described in
The dead ahead of cabin bolt hole (2d);Described middle deck tracheal orifice (2k) communicates with middle deck trachea nut bore (2c) of inner side, institute
State middle deck trachea nut bore (2c) from the most recessed described middle deck stage casing (2a) of the inner circumferential surface of described middle deck stage casing (2a)
Barrel in, the dead in line of its axis and described middle deck tracheal orifice (2k), its internal diameter is more than described middle deck tracheal orifice (2k)
Internal diameter;Each described middle deck has a middle deck made by elastic soft material to seal gallbladder (12) in sealing gallbladder groove (2b),
The structure that described middle deck seals gallbladder (12) is identical with the structure of bicycle tyre inner bag, and it is looped around described middle deck and seals gallbladder groove (2b)
Groove bottom on, its inner circumferential surface and described middle deck seal the groove bottom of gallbladder groove (2b) and are in close contact, on its inner circumferential surface
Extend radially inward a middle deck and seal courage pipe (12a);Described middle deck seals the inner chamber of courage pipe (12a) and described middle deck
The gallbladder chamber sealing gallbladder (12) communicates, and its opening exposes at described middle deck trachea nut by after described middle deck tracheal orifice (2k)
In hole (2c), described middle deck is sealed courage by middle deck trachea nut (12b) being positioned in described middle deck trachea nut bore (2c)
Pipe (12a) is fixed in described middle deck tracheal orifice (2k);The outlet side of valve cock seals courage pipe (12a) from described middle deck
Opening put in described middle deck and seal in courage pipe (12a), described valve cock is pressed abd fixed on described middle deck by valve cock nut
Seal on courage pipe (12a), but the inlet end of described valve cock will not expose from the inner circumferential surface of described middle deck stage casing (2a);
Pump is connected with the inlet end of described valve cock and passes through described valve cock institute after described middle deck sealing gallbladder (12) squeezes into gas
Stating middle deck and seal the volumetric expansion of gallbladder (12), the gas squeezed into will not release, if but described valve cock nut is unscrewed, squeeze into
Gas will by described middle deck seal courage pipe (12a) automatically release;On the external peripheral surface of described middle deck stage casing (2a)
It is evenly distributed with n middle deck location straight trough (2g) vertically;Described middle deck location straight trough (2g), it is the most recessed
In the barrel of described middle deck stage casing (2a), its transverse section is rectangle, and end face is arc surface and close to preceding described middle deck thereafter
Sealing gallbladder groove (2b), its front end face is arc surface and the front end close to described middle deck stage casing (2a);Described middle deck stage casing (2a)
Inner circumferential surface same circumference on be evenly distributed with n middle deck preceding thread hole (2h), described middle deck preceding thread hole (2h)
Being positioned between waist and the front end of described middle deck stage casing (2a), it radially gos deep into the barrel of described middle deck stage casing (2a)
In, but do not extend through the barrel of described middle deck stage casing (2a);Have screw thread in described middle deck preceding thread hole (2h), this screw thread with
Screw-threaded engagement on bolt and nut (9);It is evenly distributed with on the same circumference of the inner circumferential surface of described middle deck stage casing (2a)
N middle deck rear thread hole (2i), described middle deck rear thread hole (2i) is close to the rear end of described middle deck stage casing (2a), and it is along footpath
In the barrel outwards going deep into described middle deck stage casing (2a), but do not extend through the barrel of described middle deck stage casing (2a);In described
Screw thread is had, this screw thread and the screw-threaded engagement on bolt and nut (9) in rear thread hole, cabin (2i);N described middle deck preceding thread
One of hole (2h) is overlapping with the projection on described scalable orbital module transverse section of one of n the described middle deck rear thread hole (2i)
And in upper with described interior cabin (1) n one of cabin bolt hole (1d) be projected in same radially;Described middle deck stage casing (2a)
External peripheral surface same circumference on be evenly distributed with n middle deck positioning spiro pit (2f), described middle deck positioning spiro pit (2f)
Extending radially through the barrel of described middle deck stage casing (2a), it is close to the front end of described middle deck stage casing (2a);Middle deck without nut
Bolt (14) is by extroversion part and interior forms to part, the screw thread of described export-oriented part and described middle deck positioning spiro pit (2f)
In screw-threaded engagement, described export-oriented part fastens and is arranged in this middle deck positioning spiro pit (2f), described interior to part be without spiral shell
Stricture of vagina cylinder, the cylindrical diameter of described non-threaded cabin positions the width of straight trough (1g) equal to described interior cabin (1) in upper, described
Non-threaded cylinder is positioned in location straight trough, described cabin (1g) and its end face positions the groove bottom of straight trough (1g) with described cabin
Movable contact;Described middle deck positioning spiro pit (2f), described middle deck bolt hole (2d), described interior cabin bolt hole (1d) are in institute
State the projection on scalable orbital module transverse section not same radially;Stage casing, described interior cabin (1a) is fully contracted in described middle deck
Time in stage casing (2a), the front end face in stage casing, described interior cabin (1a) flushes with the front end face of described middle deck stage casing (2a), described
The front end face in location straight trough, interior cabin (1g) and the cylindrical cylinder of non-threaded of the described middle deck bolt (14) of relevant position
Face coincide and contacts, and the axis of described interior cabin bolt hole (1d) just weighs with the axis of corresponding described middle deck rear thread hole (2i)
Close;When stage casing, described interior cabin (1a) is the most fully stretched out from described middle deck stage casing (2a), location straight trough, described interior cabin (1g)
The cylindrical face of cylinder of non-threaded of rear end face and the described middle deck bolt (14) of relevant position coincide and contact, described interior
The axis of cabin bolt hole (1d) just overlaps with the axis of corresponding described middle deck preceding thread hole (2h);
" axial distance that adjacent two described interior cabins seal gallbladder groove (1b) is tried one's best little but must be met hereafter related request " mentioned above,
And described " axial distance that adjacent two described middle decks seal gallbladder groove (2b) is tried one's best little but must be met hereafter related request ",
Described " hereafter related request " refers to: in the stage casing, interior cabin (1a) on interior cabin (1) is fully contracted on middle deck (2)
Time in stage casing, cabin (2a), with the axial location palpus that described middle deck seals middle deck trachea nut bore (2c) that gallbladder groove (2b) communicates
The axial location sealing gallbladder groove (1b) with the interior cabin on described interior cabin (1) mutually staggers;
The outer cabin (3) of scalable orbital module is by boring section (4), outer cabin docking machinery (5) behind stage casing, outer cabin (3a), outer cabin
Fastening is combined into entirety, and the dead in line of this three component;Stage casing, described outer cabin (3a) is set in the upper middle deck stage casing of middle deck (2)
(2a) outward, its axis and the dead in line of described middle deck stage casing (2a), its inner circumferential surface and described middle deck stage casing (2a)
External peripheral surface movable contact, its axial length is equal to the axial length of described middle deck stage casing (2a);Stage casing, described outer cabin (3a)
Inner circumferential surface same circumference on be uniformly distributed n preceding thread hole, outer cabin (3d), preceding thread hole (3d) position, described outer cabin
Between waist and the front end in stage casing, described outer cabin (3a), it radially gos deep in the barrel in stage casing, described outer cabin (3a),
But do not extend through the barrel in stage casing, described outer cabin (3a);Screw thread is had, this screw thread and band spiral shell in described preceding thread hole, outer cabin (3d)
Screw-threaded engagement on cap bolt (9);It is evenly distributed with n on the same circumference of the inner circumferential surface in stage casing, described outer cabin (3a)
Individual rear thread hole, outer cabin (3e), described rear thread hole, outer cabin (3e) is close to the rear end in stage casing, described outer cabin (3a), and it is radially
Outwards go deep in the barrel in stage casing, described outer cabin (3a), but do not extend through the barrel in stage casing, described outer cabin (3a);Described outer cabin
Screw thread is had, this screw thread and the screw-threaded engagement on bolt and nut (9) in rear thread hole (3e);N preceding thread hole, described outer cabin
(3d) one of overlapping with the projection on described scalable orbital module transverse section of one of n described rear thread hole, the outer cabin (3e) and
One of n middle deck bolt hole (2d) upper with described middle deck (2) be projected in same radially;Stage casing, described outer cabin (3a)
External peripheral surface same circumference on be evenly distributed with n outer cabin positioning spiro pit (3f), described outer cabin positioning spiro pit (3f)
Extending radially through the barrel in stage casing, described outer cabin (3a), it is close to the front end in stage casing, described outer cabin (3a);Outer cabin without nut
Bolt (13) is by extroversion part and interior forms to part, the screw thread of described export-oriented part and described outer cabin positioning spiro pit (3f)
In screw-threaded engagement, described export-oriented part fastens and is arranged in this outer cabin positioning spiro pit (3f), described interior to part be without spiral shell
Stricture of vagina cylinder, the cylindrical diameter of described non-threaded is equal to the width of upper middle deck location straight trough (2g) of described middle deck (2), described
Non-threaded cylinder is positioned in described middle deck location straight trough (2g) and its end face positions the groove bottom of straight trough (2g) with described middle deck
Movable contact;Middle deck positioning spiro pit (2f) on described outer cabin positioning spiro pit (3f), described middle deck (2), described middle deck
(2) the middle deck bolt hole (2d) on, interior cabin bolt hole (1d) on described interior cabin (1), horizontal at described scalable orbital module
Projection on section not same radially;Described middle deck stage casing (2a) be fully contracted in stage casing, described outer cabin (3a) interior time,
The front end face of described middle deck stage casing (2a) flushes with the front end face in stage casing, described outer cabin (3a), described middle deck location straight trough (2g)
The cylindrical face of cylinder of non-threaded in front end face and described outer cabin bolt (13) of relevant position coincide and contact, described in
The axis of cabin bolt hole (2d) just overlaps with the axis in corresponding rear thread hole, described outer cabin (3e);Described middle deck stage casing (2a)
When the most fully stretching out from stage casing, described outer cabin (3a), the rear end face of described middle deck location straight trough (2g) and relevant position
The cylindrical face of cylinder of non-threaded of described outer cabin bolt (13) coincide and contacts, the axis of described middle deck bolt hole (2d)
Just overlap with the axis in corresponding preceding thread hole, described outer cabin (3d);
The assembly program of scalable orbital module is such that
The first step, inserts upper to interior cabin (1) interior stage casing, cabin (1a) in the inner chamber in the upper middle deck stage casing (2a) of middle deck (2), makes
Location straight trough, the interior cabin (1g) that middle deck positioning spiro pit (2f) on described middle deck (2) is directed on stage casing, described interior cabin (1a),
Then in described middle deck positioning spiro pit (2f), middle deck bolt (14) is screwed in, when described middle deck bolt (14)
When the cylindrical end face of non-threaded positions the groove bottom gentle touchdown of straight trough (1g) with described interior cabin, by described middle deck bolt
(14) fastening combination with described middle deck positioning spiro pit (2f), the most described middle deck bolt (14) is not from described middle deck
The external peripheral surface in stage casing (2a) exposes;
Second step, inserts upper for middle deck (2) middle deck stage casing (2a) in the inner chamber in upper stage casing, outer cabin (3a), outer cabin (3), makes
Middle deck location straight trough (2g) that outer cabin positioning spiro pit (3f) on described outer cabin (3) is directed on described middle deck stage casing (2a),
Then in described outer cabin positioning spiro pit (3f), outer cabin bolt (13) is screwed in, when described outer cabin bolt (13)
When the cylindrical end face of non-threaded positions the groove bottom gentle touchdown of straight trough (2g) with described middle deck, by described outer cabin bolt
(13) fastening combination with described outer cabin positioning spiro pit (3f), the most described outer cabin bolt (13) is not from described outer cabin
The external peripheral surface in stage casing (3a) exposes;
3rd step, the rear end face in the rear end face outer cabin stage casing (3a) upper with outer cabin (3) in the upper middle deck stage casing (2a) of middle deck (2)
Aliging, the stage casing, interior cabin (1a) on interior cabin (1) is removed forward, and the outer end of one of n bolt and nut (9) is through described
Middle deck bolt hole (2d) on middle deck (2) screws in rear thread hole, the outer cabin (3e) on described outer cabin (3) afterwards, by described
Middle deck (2) fastens with described outer cabin (3) and is combined into entirety;Pump connects with the inlet end of the valve cock on described middle deck (2)
Connecing and pass through described valve cock and squeeze into gas to upper middle deck sealing gallbladder (12) of described middle deck (2), described middle deck seals gallbladder (12)
Volumetric expansion after described middle deck (2) is sealed in described outer cabin (3);
4th step, the rear end face in the rear end face in stage casing, cabin (1a) middle deck stage casing (2a) upper with middle deck (2) in interior cabin (1) is upper
Alignment, the outer end of one of another n bolt and nut (9) screws in afterwards through interior cabin bolt hole (1d) on described interior cabin (1)
In middle deck rear thread hole (2i) on described middle deck (2), described interior cabin (1) and described middle deck (2) fastening are combined into whole
Body;Pump is connected with the inlet end of the valve cock on described interior cabin (1) and passes through described valve cock on described interior cabin (1)
Interior cabin seal gallbladder (8) and squeeze into gas, described interior cabin (1) is sealed in institute after sealing the volumetric expansion of gallbladder (8) by described interior cabin
State in middle deck (2);
5th step, docks machinery (5) by the outer cabin on outer cabin (3) and docks machinery with the propelling module on propelling module (10)
Device (11) docks;After completing above-mentioned installation, spaceman can be by upper interior cabin docking machinery (7) in interior cabin (1)
Hatch door is moved in described interior cabin (1), is then shut off described hatch door;The most described scalable orbital module just can be sent out by carrier rocket
Penetrate lift-off;
Scalable orbital module enter the orbit after relevant rocket firing on propelling module (10), described scalable orbital module is carried out posture adjustment or
Boosting, makes docking machinery of the interior cabin on interior cabin (1) (7) dock machinery docking with the space station on space station;Connect
Is to stretch described scalable orbital module to be allowed to space in cabin and increase, and operation sequence is divided into stretching, extension to prepare, stretches for the first time, the
Secondary stretches, builds the programs such as life or working environment;
Stretching, extension prepares: stretch unrelated spaceman with scalable orbital module in interior cabin (1), by the upper interior cabin of described interior cabin (1)
Hatch door in docking machinery (7) transfers to space station, is then shut off described hatch door;Carry out in staying described interior cabin (1)
The spaceman stretching operation has dressed spacesuit;
Stretch for the first time: unscrew the valve cock nut on interior cabin (1), interior cabin is sealed gallbladder (8) interior gas and releases, same with this
Time scalable orbital module in air release the most therewith;By the bolt and nut (9) on described interior cabin (1) from middle deck (2)
Again interior cabin bolt hole (1d) from described interior cabin (1) is exited after middle deck rear thread hole (2i) screws out;In mobile device
Promotion under, the most described interior cabin of described middle deck (2) (1) the most slowly slides, on described middle deck (2)
When the non-threaded cylinder of cabin bolt (14) contacts with the rear end face in location straight trough, the interior cabin (1g) on described interior cabin (1),
By the outer end of described bolt and nut (9) by interior cabin bolt hole (1d) on described interior cabin (1), be then threaded into described in
In middle deck preceding thread hole (2h) on cabin (2), described interior cabin (1) is fastened again with described middle deck (2) be combined into whole
Body;Pump is connected with the inlet end of the valve cock on described interior cabin (1) and passes through described valve cock to described interior cabin sealing gallbladder
(8) again squeeze into gas, after the volumetric expansion in described interior cabin sealing gallbladder (8), again described interior cabin (1) is sealed in described middle deck
(2) in;
Second time stretches: unscrew the valve cock nut on middle deck (2), is sealed in gallbladder (12) by upper for described middle deck (2) middle deck
Gas is released;By rotation in rear thread hole, the outer cabin (3e) on outer cabin (3) of the bolt and nut (9) on described middle deck (2)
Again the middle deck bolt hole (2d) from described middle deck (2) exits after going out;Under the promotion of mobile device, described outer cabin (3)
The most described middle deck (2) the most slowly slides, when outer cabin bolt (13) on described outer cabin (3) without spiral shell
When stricture of vagina cylinder contacts with the rear end face of middle deck location straight trough (2g) on described middle deck (2), by described bolt and nut (9)
Outer end by the middle deck bolt hole (2d) on described middle deck (2), be then threaded into the outer cabin preceding thread on described outer cabin (3)
In hole (3d), described middle deck (2) and described outer cabin (3) are fastened again and is combined into entirety;Pump and described middle deck (2)
On the inlet end of valve cock connect and pass through described valve cock and seal gallbladder (12) to described middle deck and again squeeze into gas, described in
Again described middle deck (2) is sealed in described outer cabin (3) after the volumetric expansion in cabin sealing gallbladder (12);
Build life or working environment: in scalable orbital module, again inject air;
Hereafter spaceman just can be lived in scalable orbital module or work, but in it, space has expanded many;
Mobile device mentioned above is the retro-rocket on propelling module (10), after described retro-rocket is lighted a fire, and the thrust of generation
Overcome frictional resistance, outer cabin (3) middle deck (2) relatively can be made to slide backward, or make middle deck (2) internal cabin (1) mutually backward
Slide.
2. according to orbital module scalable described in claim 1, it is characterised in that:
For extending the working life of scalable orbital module, the interior cabin on described scalable orbital module seals gallbladder (8), middle deck seals gallbladder
(12) in severe spatial environments, the palpus energy long period is the most aging.
3. according to orbital module scalable described in claim 1, it is characterised in that:
For ensureing spaceman safety, in described scalable orbital module, there are the component in the space of spaceman life or work, corner
Fillet structure should be used.
4. according to orbital module scalable described in claim 1, it is characterised in that:
Scalable orbital module in stretching process in order to not damage, the thrust produced after the igniting of retro-rocket on propelling module (10)
Size and must strictly control the duration of ignition:
When stretching for the first time, incipient stage thrust acts on the stiction of middle deck (2) slightly larger than interior cabin (1);Described middle deck
(2), when the most described interior cabin (1) is the most slowly slided, the size adjustment of thrust is acted on institute to equal to described interior cabin (1)
State the force of sliding friction of middle deck (2);The non-threaded cylinder of the middle deck bolt (14) on described middle deck (2) is with described
When the rear end face in location straight trough, the interior cabin (1g) on interior cabin (1) soon contacts, described retro-rocket quits work, described middle deck
(2) after continuing slip one section the most relatively because of inertia, the non-threaded cylinder of described middle deck bolt (14) and described interior cabin
When the rear end face of location straight trough (1g) contacts, described middle deck (2) is just reduced to zero with the relative velocity of described interior cabin (1);
When second time stretches, incipient stage thrust acts on the stiction of outer cabin (3) slightly larger than middle deck (2);Described outer cabin
(3), when the most described middle deck (2) the most slowly slides, the size adjustment of thrust is acted on institute to equal to described middle deck (2)
State the force of sliding friction of outer cabin (3);The non-threaded cylinder in outer cabin bolt (13) on described outer cabin (3) is with described
When the rear end face of middle deck location straight trough (2g) on middle deck (2) soon contacts, described retro-rocket quits work, described outer cabin
(3) after continuing slip one section the most relatively because of inertia, the non-threaded cylinder of described outer cabin bolt (13) and described middle deck
When the rear end face of location straight trough (2g) contacts, described outer cabin (3) is just reduced to zero with the relative velocity of described middle deck (2);
Owing to the size of frictional force is non-constant, retro-rocket may need repeatedly to light a fire and control well the time lighted a fire, and constantly carries out
Regulation.
5. according to orbital module scalable described in claim 1, it is characterised in that:
As required, the external peripheral surface in upper stage casing, outer cabin (3a), the outer cabin (3) of scalable orbital module can install solaode
Plate.
6. according to orbital module scalable described in claim 1, it is characterised in that:
In order to reduce impact force in the stretching process of scalable orbital module, following buffer structure can be used:
The cylindrical diameter of non-threaded of the middle deck bolt (14) in reduction middle deck (2), then at described non-threaded cylinder
The resilient soft overcoat of one, upper set tool, but on described non-threaded cylinder of holster after described overcoat the external diameter of this overcoat still equal to interior
The width in location straight trough, the interior cabin (1g) on cabin (1);
Reduce the cylindrical diameter of non-threaded in outer cabin bolt (13) on outer cabin (3), then at described non-threaded cylinder
The resilient soft overcoat of one, upper set tool, but on described non-threaded cylinder of holster after described overcoat the external diameter of this overcoat still equal in
The width of middle deck location straight trough (2g) on cabin (2).
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CN107963241A (en) * | 2017-12-21 | 2018-04-27 | 中国科学院沈阳自动化研究所 | Developing space inflation bay section |
CN108528762A (en) * | 2018-04-13 | 2018-09-14 | 哈尔滨工业大学 | A kind of stretching type can open up space bay section skeleton structure |
CN110508332A (en) * | 2019-08-21 | 2019-11-29 | 中国航空制造技术研究院 | A kind of net gas cabin device of combined type flexible |
WO2023024311A1 (en) * | 2021-08-27 | 2023-03-02 | 鲁东大学 | Flexible space capsule |
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