CN1412083A - Superhigh pressure pneumatic space aircraft - Google Patents
Superhigh pressure pneumatic space aircraft Download PDFInfo
- Publication number
- CN1412083A CN1412083A CN 02124986 CN02124986A CN1412083A CN 1412083 A CN1412083 A CN 1412083A CN 02124986 CN02124986 CN 02124986 CN 02124986 A CN02124986 A CN 02124986A CN 1412083 A CN1412083 A CN 1412083A
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- CN
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- Prior art keywords
- aerospace plane
- air
- superhigh pressure
- extra
- high pressure
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- Jet Pumps And Other Pumps (AREA)
Abstract
A superhigh pressure pneumatic space aircraft is a single-stage injection repeatedly-usable space carrier. Said invention provides a technical scheme which uses primary high-pressure pump to match it with superhigh pressure air pump and utilizes the explosive gas flow which not only can be used as power for driving superhigh pressure airpump piston and compressing superhigh pressure air to make the piston reciprocate, but also can be used as superhigh pressure air source to reciprocally circulate and generate superhigh pressure air.
Description
Superhigh pressure pneumatic space aircraft of the present invention is the reusable space launch vehicle technology scheme of a kind of Single Stage To Orbit.Belong to field of aerospace technology.
Aerospace plane in existing carrier rocket, space shuttle, the development all adopts the propulsion system of the thermal power transfer tractive power that is in operation.This propulsion system is subjected to the restriction of complex mechanism, fuel, specific impulse value, mass ratio.It is low to finish traffic cost height between the world, conveying efficiency, safety, reliability, usability.
Superhigh pressure pneumatic space aircraft of the present invention, adopting and formerly gathering the processing extra-high on ground is the finished product merit.Promote the Push Technology scheme of aerospace plane flight.
The collection of extra-high: as shown in Figure 1, the ultra high pressure gas pumping plant is by dry fil 1 elementary high-pressure pump 2 ultra high pressure gas cabins 3 ultra high pressure gas pump pistons, and cylinder 4 moves back air valve 5 and forms when graduated cylinder 6 advances thorax 7 return-air fils 8 return line 9 pistons 10.Its principle of work: the dry air that drying fil 1 filters, inflate to superhigh pressure air pump cylinder 4 ultra high pressure gas cabins 3 by elementary high-pressure pump 2.When superhigh pressure air pump cylinder 4 internal gas pressures reach 200 barometric pressures, advance in the thorax 7 and promote piston 10 with 200 barometric pressure high pressure gas when graduated cylinder 6 spurts the explosive blast air, compress into ultra high pressure gas cabin 3 and move back air valve 5 unlatchings, the explosive air-flow that work done finishes enters in the superhigh pressure air pump cylinder 4 through moving back air valve 5 return line 9 charing filters 8 again, promotes piston 10 and returns original position.When withdrawing from, graduated cylinder 6 advances thorax 7.The new graduated cylinder 6 of working as enters propelling thorax 7.Circulation processes 200,000 atmospheric ultra high pressure gas finished product merits and enters ultra high pressure gas cabin 3 and so forth.
Superhigh pressure pneumatic space aircraft structure and technical characterictic: 14 air cushion gas cabins, 13 ultra high pressure gas cabins, (see figure 2) conical fuselage 11 a four directions jet steering valve, 12 load cabins, 15 air cushion skirts, 16 propulsion jet valves 17 advance spout 18 to form.
The superhigh pressure pneumatic space aircraft principle of work: (see figure 3) is opened propulsion jet valve 7 ultra high pressure gas and taken off vertically with ten thousand meter per second jet velocities promotion aerospace plane through jet spout, and----orbital flight--reentry--adjustment vertical landing attitude rises and enters the orbit; the exhaust of air cushion cabin; the cushioning effect that produces in the aerospace plane air cushion skirt 6, the vertical soft landing landing of protection aerospace plane.
Also can utilize superhigh pressure pneumatic Push Technology design diving aircraft in the enforcement, the cosmic velocity guided missile.
Should note producing the safety of ultra high pressure gas in the enforcement.Choose reasonable ultra high pressure gas cabin, propulsion valve, propulsion jet gate material.The development of superhigh pressure read table.
Description of drawings: Fig. 1: be ultra high pressure gas pumping plant work scheme drawing
Fig. 2: be the superhigh pressure pneumatic space aircraft structural representation
Fig. 3: be superhigh pressure pneumatic space aircraft flight scheme drawing
Claims (4)
1, a kind of aerospace plane: adopt and formerly gather the processing extra-high promotes aerospace plane flight for the finished product merit Push Technology on ground, it is characterized in that cooperating superhigh pressure air pump by elementary high pressure pump, utilizing the explosive air-flow promptly is the power that promotes super-pressure pump Piston Compression extra-high reciprocating action, it is again the double action of extra-high source of the gas, reciprocation cycle is produced the ultra high pressure gas pumping plant of extra-high, utilize the Push Technology design aerospace plane of extra-high for thrust power, the diving aircraft, the cosmic velocity guided missile, the vertical air cushion soft landing of aerospace plane technology.
2, it is characterized in that according to the described aerospace plane of claim 1: the ultra high pressure gas pumping plant is because the elementary high-pressure pump of dry fil (1) (2) ultra high pressure gas cabin (3) super mausoleum grave air pump cylinder (4) moves back air valve (5) when graduated cylinder (6) propelling thorax (7) return-air fil (8) return line (9) piston (10) composition.
3, it is characterized in that according to the described aerospace plane of claim 1: conical fuselage (11) four air cushion gas cabin, ultra high pressure gas cabin, status of a sovereign jet steering valve (12) load cabin (13) (14) (15) air cushion skirt (16) propulsion jet valves (17) advance spout (18).
4, it is characterized in that according to the described aerospace plane of claim 1: vertical landing, the exhaust of air cushion cabin produces cushioning effect in the aerospace plane air cushion skirt (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02124986 CN1412083A (en) | 2002-06-25 | 2002-06-25 | Superhigh pressure pneumatic space aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02124986 CN1412083A (en) | 2002-06-25 | 2002-06-25 | Superhigh pressure pneumatic space aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1412083A true CN1412083A (en) | 2003-04-23 |
Family
ID=4745443
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 02124986 Pending CN1412083A (en) | 2002-06-25 | 2002-06-25 | Superhigh pressure pneumatic space aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1412083A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105228900A (en) * | 2013-04-05 | 2016-01-06 | 空中客车防务和空间公司 | The device of the speed during the aviation flight stage and relevant method of converting is become from space travel transition stage for controlling space shuttle |
| RU205688U1 (en) * | 2021-03-22 | 2021-07-28 | Валерий Иванович Зуев | LANDING DEVICE ON AIRBAG OF SPACE STATIONS |
-
2002
- 2002-06-25 CN CN 02124986 patent/CN1412083A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105228900A (en) * | 2013-04-05 | 2016-01-06 | 空中客车防务和空间公司 | The device of the speed during the aviation flight stage and relevant method of converting is become from space travel transition stage for controlling space shuttle |
| RU205688U1 (en) * | 2021-03-22 | 2021-07-28 | Валерий Иванович Зуев | LANDING DEVICE ON AIRBAG OF SPACE STATIONS |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |