DE102015012953A1 - ROOM GLIDER / AIR SPACE / Outer space (FLOOR / AIR / WORLD TRANSPORT) - Google Patents

ROOM GLIDER / AIR SPACE / Outer space (FLOOR / AIR / WORLD TRANSPORT) Download PDF

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Publication number
DE102015012953A1
DE102015012953A1 DE102015012953.8A DE102015012953A DE102015012953A1 DE 102015012953 A1 DE102015012953 A1 DE 102015012953A1 DE 102015012953 A DE102015012953 A DE 102015012953A DE 102015012953 A1 DE102015012953 A1 DE 102015012953A1
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Germany
Prior art keywords
orbiter
rotors
air
space
rocket
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Pending
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DE102015012953.8A
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German (de)
Inventor
Anmelder Gleich
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Individual
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Individual
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Priority to DE102015012953.8A priority Critical patent/DE102015012953A1/en
Publication of DE102015012953A1 publication Critical patent/DE102015012953A1/en
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/14—Space shuttles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2221—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the manner of deployment
    • B64G1/2227—Inflating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/409—Unconventional spacecraft propulsion systems

Abstract

Deltaflügler mit Turbinengetriebenen-Gegenläufigen-Doppel-Rotor (Mittelrotor) im Orbiter Gehäuse mit an den Seiten im Turbinenabgasstrom betriebenen Außenrotoren mittels Zentralsteuerungsklappenversteller Auftriebsschub bei gleichzeitiger Vortriebsschub in Bodenluftraumverhältnissen mit anschließenden Raketenvortriebsschubantrieben in den höheren Atmosphärenschichten. Sowie Plasmaphotonenantrieb im hinteren Bereich des Orbiters als Vorschub im Luftleeren Raum sowie im vorderen Bereich ein Plasma Photonenantrieb zur Abbremsung des Orbiters Raketenstrahldüsen zur Steuerung und Landeanflugspositsionierung. Bodenairbag als Sicherungseinrichtung bei Triebswerksausfall oder Wasserung. Ausgelegt als Delta Nurflügler oder Schwenkflügler mit Druckkabine. Neuheiten: Durch die Turbinen werden Mittelrotoren und Außenrotoren angetrieben und heben das Fluggerät bei gleichzeitigem Vortrieb an.Turbocharged counter-rotating double rotor (center rotor) in the orbiter housing with external rotors operated on the sides in the turbine exhaust stream by means of central control damper lift boost with simultaneous propulsion thrust in soil air space ratios followed by rocket propulsion thrusters in the higher atmosphere layers. As well as plasma photon drive in the rear area of the orbiter as feed in the evacuation space and in the front area a plasma photon drive for decelerating the orbiter rocket jet nozzles for the control and landing approach. Floor airbag as a safety device in case of engine failure or watering. Designed as a Delta flying wing or swinging wing with pressurized cabin. Innovations: The turbines propel center rotors and outer rotors and raise the aircraft while driving forward.

Description

Problem:Problem:

Der im Patentanspruch 1 angegebenen liegt das Problem zugrunde das herkömmliche Raumschiffe gleich welcher Art unter großem Energieaufwand vom Boden in den Luftraum bzw. Orbit starten und Landen müssen.The specified in claim 1 is based on the problem of the conventional spaceships of any kind under great energy expenditure from the ground in the airspace or orbit and start landing.

Die Vielzahl von Eigenschaften in einer Gesamtkonstruktion kostengünstig und sicher in einem Grundbaumuster Entwicklungsfähig zu vereinen.The variety of properties in an overall construction cost-effectively and safely in a basic model developable to unite.

Lösung:Solution:

Mithilfe von Mittelrotor doppelt Gegenläufig und Aussenrotoren in einem Düsenstrom zu beschleunigen und so einen gleichzeitigen Auftrieb als auch Vortrieb bei geringen Energieaufwand zu gewährleisten. Postionsdüsen zur Positionierung und Raketenantrieb zum Vortieb in großen Höhen; sowie Plasma Photonen Antrieb im Weltaum.Using center rotor double speed counter-rotating and external rotors in a jet flow, thus ensuring a simultaneous buoyancy and propulsion at low energy consumption. Positioning jets for positioning and rocket propulsion for pre-screening at high altitudes; as well as plasma photons drive in the space of the world.

Erreichte Vorteile:Achieved benefits:

Die mit der Erfindung erzielten Vorteile bestehen insbesondere darin das bei geringem Bauaufwand und Kostengünstiger Produktion mit geringem Gewicht die Schwerkraft der Erde oder Planeten und Monden am leichtsten überwunden werden kann.The advantages achieved by the invention are in particular that at low construction costs and cost-effective production with low weight, the gravity of the earth or planets and moons can be overcome most easily.

Weitere Ausgestaltung der Erfindung:Further embodiment of the invention:

Eine Vorteilhafte Ausgstaltung der Erfindung ist eine Regelbare Klappe im Abgasstrom die Drehzahl unabhängig den Auftrieb und Vortrieb steuern kann;
Beschreibung eines oder mehrerer Ausführungsbeispiele:An advantageous Ausgstaltung of the invention is a controllable flap in the exhaust stream, the speed can independently control the buoyancy and propulsion;
Description of one or more embodiments:

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
Turbineturbine
33
Cockpitcockpit
44
Plasma-Photonen-Antrieb-BremsePlasma-photon drive-brake
55
Raketenantriebrocket propulsion
66
AussenrotorenOutside rotors
77
Delta oder SchwenkflügelDelta or swing-wing
1010
SteurungsklappeSteurungsklappe
1111
Plasma PhotonenantriebPlasma photon drive
1212
Radwerk/GleitkufenRadwerk / skids
1414
Mittelrotor doppelt Gegenläufig/(Abgasschaufeln)Central rotor double counter-rotating / (exhaust gas blades)

Claims (1)

Deltaflügler mit Turbinengetriebenen-Gegenläufigen-Doppel-Rotor (Mittelrotor) im Orbiter Gehäuse mit an den Seiten im Turbinenabgasstrom betriebenen Außenrotoren mittels Zentralsteuerungsklappenversteller Auftriebsschub bei gleichzeitiger Vortriebsschub in Bodenluftraumverhältnissen mit anschließenden Raketenvortriebsschubantrieben in den höheren Atmosphärenschichten. Sowie Plasmaphotonenantrieb im hinteren Bereich des Orbiters als Vorschub im Luftleeren Raum sowie im vorderen Bereich ein Plasma Photonenantrieb zur Abbremsung des Orbiters Raketenstrahldüsen zur Steuerung und Landeanflugspositsionierung. Bodenairbag als Sicherungseinrichtung bei Triebswerksausfall oder Wasserung. Ausgelegt als Delta Nurflügler oder Schwenkflügler mit Druckkabine. Neuheiten: Durch die Turbinen werden Mittelrotoren und Außenrotoren angetrieben und heben das Fluggerät bei gleichzeitigem Vortrieb an.Turbocharged counter-rotating double rotor (center rotor) in the orbiter housing with external rotors operated on the sides in the turbine exhaust stream by means of central control damper lift boost with simultaneous propulsion thrust in soil air space ratios followed by rocket propulsion thrusters in the higher atmosphere layers. As well as plasma photon drive in the rear area of the orbiter as feed in the evacuation space and in the front area a plasma photon drive for decelerating the orbiter rocket jet nozzles for the control and landing approach. Floor airbag as a safety device in case of engine failure or watering. Designed as a Delta flying wing or swinging wing with pressurized cabin. New hits: The turbines drive mid-rotors and external rotors and raise the aircraft while driving forward.
DE102015012953.8A 2015-10-07 2015-10-07 ROOM GLIDER / AIR SPACE / Outer space (FLOOR / AIR / WORLD TRANSPORT) Pending DE102015012953A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE102015012953.8A DE102015012953A1 (en) 2015-10-07 2015-10-07 ROOM GLIDER / AIR SPACE / Outer space (FLOOR / AIR / WORLD TRANSPORT)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102015012953.8A DE102015012953A1 (en) 2015-10-07 2015-10-07 ROOM GLIDER / AIR SPACE / Outer space (FLOOR / AIR / WORLD TRANSPORT)

Publications (1)

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DE102015012953A1 true DE102015012953A1 (en) 2017-04-13

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DE102015012953.8A Pending DE102015012953A1 (en) 2015-10-07 2015-10-07 ROOM GLIDER / AIR SPACE / Outer space (FLOOR / AIR / WORLD TRANSPORT)

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4018369A1 (en) * 1990-06-08 1991-12-19 Poisel Otto Karl Spacecraft with adjustable speed based on tumbler-doll - has pointed structure with encircling glass cladding and total stability ensuring that axis is always vertical
WO1995011161A1 (en) * 1992-05-14 1995-04-27 Kunkel, Klaus Reusable spacecraft
WO1998056658A1 (en) * 1997-06-12 1998-12-17 Kaehler Kai Reusable spaceship
AT413977B (en) * 2002-07-29 2006-07-15 Firooz Kita AIR AND SPACE VEHICLE

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4018369A1 (en) * 1990-06-08 1991-12-19 Poisel Otto Karl Spacecraft with adjustable speed based on tumbler-doll - has pointed structure with encircling glass cladding and total stability ensuring that axis is always vertical
WO1995011161A1 (en) * 1992-05-14 1995-04-27 Kunkel, Klaus Reusable spacecraft
WO1998056658A1 (en) * 1997-06-12 1998-12-17 Kaehler Kai Reusable spaceship
AT413977B (en) * 2002-07-29 2006-07-15 Firooz Kita AIR AND SPACE VEHICLE

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