DE102006031981A1 - Aircraft for use as underwater vessel, has wings with space that is filled with atmospheric gas or light gas, where weight of aircraft is lighter and heavier than atmospheric gas in dependence of amount of inflated atmospheric gas - Google Patents

Aircraft for use as underwater vessel, has wings with space that is filled with atmospheric gas or light gas, where weight of aircraft is lighter and heavier than atmospheric gas in dependence of amount of inflated atmospheric gas Download PDF

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Publication number
DE102006031981A1
DE102006031981A1 DE200610031981 DE102006031981A DE102006031981A1 DE 102006031981 A1 DE102006031981 A1 DE 102006031981A1 DE 200610031981 DE200610031981 DE 200610031981 DE 102006031981 A DE102006031981 A DE 102006031981A DE 102006031981 A1 DE102006031981 A1 DE 102006031981A1
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Germany
Prior art keywords
aircraft
gas
atmospheric gas
wings
filled
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Ceased
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DE200610031981
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German (de)
Inventor
Alexandra Schuster
Alexander Schuster
Maria-Elisabet Schuster
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Individual
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Individual
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Priority to DE200610031981 priority Critical patent/DE102006031981A1/en
Publication of DE102006031981A1 publication Critical patent/DE102006031981A1/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/06Rigid airships; Semi-rigid airships
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/06Rigid airships; Semi-rigid airships
    • B64B1/20Rigid airships; Semi-rigid airships provided with wings or stabilising surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B2201/00Hybrid airships, i.e. airships where lift is generated aerodynamically and statically

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Photovoltaic Devices (AREA)
  • Toys (AREA)

Abstract

The aircraft has wings (2) filled with gas. The wings have a space that is formed with flexible partitions. The space is filled with atmospheric gas or light gas, where weight of the aircraft is lighter and heavier than the atmospheric gas in dependence of amount of inflated/pumped atmospheric gas. The aircraft is lowered through weight expansion by pumping/inflating of the atmospheric gas in the space, and through volume reduction of the space. An ellipsoid or drop-shaped balloon (1) and a tail control gear (4) are provided in the aircraft.

Description

Die Erfindung betrifft das Fluggerät A mit Flügeln, das während des Fluges abwechselnd leichter oder schwerer werden kann, nach dem Oberbegriff des Anspruchs 1. Das Ziel der Erfindung ist die Herstellung eines Fluggeräts, welches ohne Brennstoff, Muskel- oder Elektroantrieb fliegen kann und dennoch den Gleitflug in beliebigen Richtungen mit Flugsteuerung, bei abwechselndem Aufsteigen und Sinken des Fluggeräts, ermöglicht. Es sind bekannt (Fluggerät DE 10 2004 010 549 A1 , Fluggerät B 102005056099.7, Solarwindkraftwerk DE 10 2004 055 212 A1 ) Fluggeräte mit einem geschlossenen, gasundurchlässigen, undehnbaren, leichten Raum, welcher im Inneren eine (oder zwei) zusätzliche, biegsame Trennwände enthält. Ein durch die Trennwand entstehende Raum muss mit leichtem Gas gefüllt werden. Der andere auf der anderen Seite entstehende Raum kann mit Atmosphären gas aufgepumpt werden oder diesen wider ausströmen lassen.The invention relates to the aircraft A with wings, which can be alternately lighter or heavier during the flight, according to the preamble of claim 1. The object of the invention is the production of an aircraft that can fly without fuel, muscle or electric drive and yet the Gliding in any direction with flight control, with alternating ascent and descent of the aircraft enabled. It is known (aircraft DE 10 2004 010 549 A1 , Aircraft B 102005056099.7, solar wind power plant DE 10 2004 055 212 A1 ) Aircraft having a closed, gas-impermeable, inextensible, lightweight space containing internally one (or two) additional flexible partitions. A space created by the partition must be filled with light gas. The other on the other side resulting space can be pumped with atmospheric gas or let it flow against.

Die Erfindung wird durch Zeichnungen erläutert:The The invention is illustrated by drawings:

1 Fluggerät A mit Trennwand (wänden). 1 Aircraft A with partition (walls).

2. Fluggerät A bei Zusammendrückung. 2 , Aircraft A at compression.

Fluggerät A besteht aus einen ellipsoid- oder tropfenförmigen oder andersförmigen germetischen Ballon 1 aus einem undehnbaren Stoff (Kunststoff, dünnes Metall u.a.), welcher mit leichtem Gas gefüllt ist. Die Flügel 2 können einschichtige oder flügelförmige germetische Räume mit leichtem Gas sein. Das Fluggerät kann mit einem Schwanzleitwerk 4 ausgestattet sein. Auftrieb dieses Geräts inklusive Pilot und Ladung ermöglicht einen Aufstieg bis zu einer bestimmten Höhe.Aircraft A consists of an ellipsoidal or teardrop-shaped or otherwise shaped hermetic balloon 1 of an inextensible material (plastic, thin metal, etc.), which is filled with light gas. The wings 2 may be single-layered or wing-shaped germetic spaces with light gas. The aircraft can with a tail tail 4 be equipped. Buoyancy of this device including pilot and cargo allows for ascent to a certain altitude.

Senkung des Geräts erfolgt durch a) Gewichtvergrößerung (Aufpumpung von Atmosphärengase in einen der Räume zwischen Außenwand und biegsamer Trennwand, wie 1 zeigt) oder durch b) Volumenverminderung des, mit leichtem Gas gefüllten, Raums. b) geschieht beim zusammendrücken des germetischen Raums (wie 2. zeigt). Während der Absenkung gleitet das Fluggerät wie ein Segelflugzeug, während des Anstieges strömt Luft durch die hintere Klappe aus und stellt so einen Düsenantrieb dar. Auf diese Weise fliegt das Fluggerät vorwärts nach oben. Oberhalb der Wolkendecke produzieren die Solarzellen Strom, durch den der Elektromotor angetrieben wird, welcher die Luftpumpe aktiviert, welche wiederum Luft in den unteren Raum pumpt. Bei Überschuss an Luft indem Raum wird diese al Düsenantrieb ausgestoßen und dient somit zur Fortbewegung.The device is lowered by a) Increasing the weight (inflation of atmospheric gases into one of the spaces between the outer wall and the flexible partition, such as 1 shows) or by b) volume reduction of, filled with light gas space. b) happens when squeezing the germetic space (like 2 , shows). During lowering, the aircraft glides like a glider, while during the ascent air flows through the rear flap, thus providing a jet propulsion. In this way, the aircraft flies forward. Above the cloud cover, the solar cells produce electricity that drives the electric motor, which activates the air pump, which in turn pumps air into the lower space. When there is excess air in the room, this al nozzle drive is expelled and thus serves for locomotion.

Aufpumpen und Zusammendrücken kann von Pilotenhand oder mit Elektroantrieb von den Solarzellenelektrostromerzeuger bewerkstelligt werden.inflation and squeezing can by pilot's hand or with electric drive from the solar cell electric power generator be accomplished.

Dieses Gerät kann auch unter Wasser benutzt werden. Der einzige unterschied in der Funktionsweise besteht darin, das statt Luft Wasser als Ballast verwändet wird.This Device can also be used under water. The only difference in the Functionality is that instead of air water as ballast verwändet becomes.

Claims (6)

Fluggerät A ist mit leichtem Gas angefüllten, ein germetischer Raum, mit Flügel, einer oder zwei biegsamen Trennwänden, die in den Räumen leichten Gas von Atmosphärengas trennen, dadurch gekennzeichnet, das das Gewicht des Fluggerätes leichter oder schwerer als Atmosphärengas sein kann, in Abhängigkeit von der Menge des aufgepumpten Atmosphärengases (Ballast),Aircraft A is light gas filled, a glazed space, with wings, one or two flexible partitions which separate light gas from atmosphere gas in the spaces, characterized in that the weight of the aircraft may be lighter or heavier than atmospheric gas, depending on the amount of the inflated atmosphere gas (ballast), Fluggerät A nach Anspruch 1, dadurch gekennzeichnet, das Flügel mit leichtem Gas angefüllt sein können,aircraft A according to claim 1, characterized in that the wing with be filled with light gas can, Fluggerät A nach Ansprüche 1 und 2, ist dadurch gekennzeichnet, das während abfallender Flugbahn, wenn Fluggerät schwerer als Atmosphärengas ist, man es mit den Flügeln so steuern kann, dass das Fluggerät horizontale Bestandteile von Flugbahnen in bestimmten Richtungen haben wird,aircraft A according to claims 1 and 2, characterized in that during descending trajectory, if aircraft heavier than atmospheric gas is it, with the wings so that the aircraft can control horizontal components of trajectories in certain directions, Fluggerät A nach Ansprüche 1, 2 und 3, dadurch gekennzeichnet, das man im Flugbahnscheitel per Hand, oder mechanisch (z.B. von Sonnenzellenstromantrieb) Atmosphärengas als Ballast aufpumpen und im Tiefsten Punkt der Flugbahn hintere Klappe öffnen muss, um Atmosphärengas (Ballast) hinauszulassen und somit Düsenantrieb zu gewährleisten,aircraft A according to claims 1, 2 and 3, characterized in that in the trajectory vertex per Hand, or mechanically (e.g., from solar cell power propulsion) atmospheric gas as Pump up ballast and open the rear flap at the lowest point of the trajectory, to atmosphere gas (Ballast) to let out and thus ensure nozzle drive, Fluggerät A nach Ansprüchen 1, 2, 3 und 4, dadurch gekennzeichnet, das Gerät auch als Unterwasserschiff funktionieren kann, wenn statt Luft-Wasser als Ballast benutzt wird.aircraft A according to claims 1, 2, 3 and 4, characterized, the device also as underwater vessel can work if instead of air-water is used as ballast. Fluggerät A nach Ansprüchen 1, 2, 3 und 4, dadurch gekennzeichnet, dass, wenn die Sonne scheint man mit Solarzellenstromantrieb Atmosphärengas aufpumpen und gleichzeitig durch hintere Klappe(-n) hinauslassen und somit Düsenantrieb und Flug gewährleisten kann.aircraft A according to claims 1, 2, 3 and 4, characterized in that when the sun shines one with solar cell electric drive Inflate atmosphere gas and at the same time through the rear flap (-n) and thus let nozzle drive and ensure flight can.
DE200610031981 2006-07-11 2006-07-11 Aircraft for use as underwater vessel, has wings with space that is filled with atmospheric gas or light gas, where weight of aircraft is lighter and heavier than atmospheric gas in dependence of amount of inflated atmospheric gas Ceased DE102006031981A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE200610031981 DE102006031981A1 (en) 2006-07-11 2006-07-11 Aircraft for use as underwater vessel, has wings with space that is filled with atmospheric gas or light gas, where weight of aircraft is lighter and heavier than atmospheric gas in dependence of amount of inflated atmospheric gas

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DE200610031981 DE102006031981A1 (en) 2006-07-11 2006-07-11 Aircraft for use as underwater vessel, has wings with space that is filled with atmospheric gas or light gas, where weight of aircraft is lighter and heavier than atmospheric gas in dependence of amount of inflated atmospheric gas

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DE102006031981A1 true DE102006031981A1 (en) 2008-01-24

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008055842A1 (en) 2008-11-04 2010-05-12 Alexandra Schuster Aircraft i.e. glider, has body and wings, where volume of body is varied with constant weight of body by using hand lever or hand screw mechanism, and lifting of aircraft is controlled by pilot
WO2011117619A3 (en) * 2010-03-23 2011-11-17 Athene Works Limited Aerial vehicle and method of flight

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1860087A (en) * 1931-01-17 1932-05-24 Fehrenbach Anton Superlight plane
US5516235A (en) * 1991-01-25 1996-05-14 Controlled Lifting International Limited Method and apparatus of raising objects from the sea bed
DE19722588A1 (en) * 1997-05-30 1998-12-03 Abb Patent Gmbh Aircraft based upon aerostatic lift
EP1600370A2 (en) * 2004-05-24 2005-11-30 The Boeing Company High-aspect ratio hybrid airship

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1860087A (en) * 1931-01-17 1932-05-24 Fehrenbach Anton Superlight plane
US5516235A (en) * 1991-01-25 1996-05-14 Controlled Lifting International Limited Method and apparatus of raising objects from the sea bed
DE19722588A1 (en) * 1997-05-30 1998-12-03 Abb Patent Gmbh Aircraft based upon aerostatic lift
EP1600370A2 (en) * 2004-05-24 2005-11-30 The Boeing Company High-aspect ratio hybrid airship

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008055842A1 (en) 2008-11-04 2010-05-12 Alexandra Schuster Aircraft i.e. glider, has body and wings, where volume of body is varied with constant weight of body by using hand lever or hand screw mechanism, and lifting of aircraft is controlled by pilot
WO2011117619A3 (en) * 2010-03-23 2011-11-17 Athene Works Limited Aerial vehicle and method of flight

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