DE102004010549A1 - Flying device used as a hot air balloon comprises a closed gas-impermeable chamber with an additional bendable separating wall - Google Patents

Flying device used as a hot air balloon comprises a closed gas-impermeable chamber with an additional bendable separating wall Download PDF

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Publication number
DE102004010549A1
DE102004010549A1 DE200410010549 DE102004010549A DE102004010549A1 DE 102004010549 A1 DE102004010549 A1 DE 102004010549A1 DE 200410010549 DE200410010549 DE 200410010549 DE 102004010549 A DE102004010549 A DE 102004010549A DE 102004010549 A1 DE102004010549 A1 DE 102004010549A1
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Germany
Prior art keywords
aircraft
gas
space
hot air
separating wall
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Ceased
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DE200410010549
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German (de)
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Alexander Schuster
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Individual
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Individual
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Priority to DE200410010549 priority Critical patent/DE102004010549A1/en
Priority to DE200410025795 priority patent/DE102004025795A1/en
Publication of DE102004010549A1 publication Critical patent/DE102004010549A1/en
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/04—Man-powered aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/70—Ballasting arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/30—Wings comprising inflatable structural components
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft

Abstract

Flying device comprises a closed gas-impermeable chamber (1) with an additional bendable separating wall (2). A light gas is filled in one side of the separating wall and atmospheric air is pumped into the other side or let out via a valve (4). Preferred Features: The gas chamber is dimensioned so that the flying device can be lifted to a determined height and landed using the required amount of atmospheric air.

Description

Die vorliegende Erfindung bezieht sich auf das Gebiet Fluggeräte, die ihr Gewicht während des Fluges ändern können.The The present invention relates to the field of aircraft that her weight during change the flight can.

Bekannt ist Steuerung der Schwerpunktlage eines Vakuum-Luftschiffes, Patentschrift DE 49763 C2 . In beiden gegenseitigen Enden gibt es zwei germetische Kammern 10 und 11, welche können abwechseln mit Luft anfüllen und mit dem steuern.Known is control of the center of gravity of a vacuum airship, patent DE 49763 C2 , In both mutual ends there are two germetic chambers 10 and 11 which can alternately fill with air and control with the.

Bekannt ist aerostatischer offener oder geschlossener Freiballon, Patentschrift DE 4023112 C2 , welcher kann Volumenbereiche vom Ballon durch Einschnürungen ändern und mit dem steuern.Is known aerostatic open or closed free balloon, patent DE 4023112 C2 which can change volume areas of the balloon by constrictions and control with that.

Bekannt ist auch Hybrid-Luftschiff, Auslegeschrift 25077514, welcher kann aerodynamische und aerostatische Auftriebanteile ändern auch mit dem steuern.Known is also a hybrid airship, Auslegeschrift 25077514, which can Aerodynamic and aerostatic lift components change as well with the steer.

Das Ziel der Erfindung ist Bildung Fluggeräte mit geschlossene, gasundurchlässige undehnbare, leichte Räumen, welche haben drinnen zusätzliche, biegsame Trennwände und können eine Seite von der Trennwand mit dem leichten Gas anfüllen, aber andere Seite mit dem Atmosphärengas aufpumpen. Die Trennwand kann dehnbar sein. Je mehr wird Atmosphärengas aufgepumpt, desto schwerer wird Fluggerät sein und niedriger geht das.The The aim of the invention is formation of aircraft with closed, gas impermeable, inextensible, lightweight rooms which ones have additional, flexible inside partitions and can fill one side of the partition with light gas, but others Side with the atmosphere gas Inflate. The partition can be stretchable. The more atmospheric gas is pumped up, the heavier becomes the aircraft be and lower is that.

Die Erfindung wird durch Zeichnungen erläutern:The The invention will be explained by drawings:

1 Ein Luftballon. 1 A balloon.

2 Ein Deltaflugzeug mit Muskelantrieb. 2 A delta airplane with muscle drive.

3 Ein Flugschiff. 3 A ship of the air.

4 Eine Wasserladung vom Flugschiff. 4 A water cargo from the ship.

Auf 1 ist ein Luftballon mit dem geschlossene, gasundurchlässige, undehnbare Ballon 1, der zusätzliche, bigsame Trennwand 2, dem Luftzuführungsrohr 3 mit der Pumpe und der Klappe 4 gezeigt. Der Trennwand 2 kann verschiedene Lage einnehmen: a) Die Klappe 4 ist offen, die Pumpe arbeitet nicht, der Ballon ist mit dem leichten Gas anfüllt, die Trennwand 2 ist zur unteren Wand vom Ballon angedrückt; b) Die Klappe 4 ist zu, Pumpe arbeitet bisschen, die Trennwand 2 nimmt, z.B., Lage A ein; c) der Ballon hat kein leichte Gas (nie angefüllt, oder unglücklicher weise durch welches Loch ausgegangen), die Klappe ist aus, die Pumpe und Luftheizer arbeiten, die Trennwand 2 nimmt Lage B ein und das Fluggerät verwandelt sich im Heizluftballon.On 1 is a balloon with the closed, gas-impermeable, inextensible balloon 1 , the extra, bigsame partition 2 , the air supply pipe 3 with the pump and the flap 4 shown. The partition 2 can take different positions: a) the flap 4 is open, the pump does not work, the balloon is filled with light gas, the partition 2 is pressed to the lower wall by the balloon; b) The flap 4 is too, pump works bit, the partition 2 takes, for example, position A; c) the balloon has no light gas (never filled, or unfortunately gone out through which hole), the flap is off, the pump and air heater work, the partition 2 takes position B and the aircraft turns into a hot air balloon.

Normalerweise, der Ballon ist mit bestimmte Menge vom leichten Gas angefüllt und Menge vom Atmosphärengas (Luft) unter der Trennwand kann ändern; mit dem ändert auch das Gewicht von Luftballon beim ungeänderter Volumen.Usually, the balloon is filled with a certain amount of light gas and Amount of the atmosphere gas (Air) under the partition can change; with that changes also the weight of balloon when unaltered volume.

Das Volumen vom Luftballon muss so berechnet sein, das ohne Luft kann sich Luftballon bis bestimmte Hohe erheben, mit Luftaufpumpen muss sich Luftballon senken und bei bestimmte Luftmenge muss Luftballon landen. Bei dem braucht man ganze Exploitierungsperiode keine Zugabe vom leichter Gas.The Volume of the balloon must be calculated so that can without air Balloon should rise to a certain height, with air pumps must Lower the balloon and with a certain amount of air balloon must land. With that one needs no addition of the whole exploitation period light gas.

Auf 2 ist ein Deltaflugzeug gezeigt. Ein Deltaflügel 5 ist mit leichtem Gas angefüllt. Unter Trennwand 6 kann man Luft aufpumpen. Ein Pilot 7 steuert mit Hände ein Trapez 8, gleichzeitig pedalirt er Luftschraube 9 oder Pumpe. Ohne Luft erhebt sich Deltaflugzeug, mit bestimmte Menge vom Luft wird das Gerät schwerer als Luft sein und muss vom Muskelantrieb vom Pilot fliegen.On 2 is shown a delta plane. A delta wing 5 is filled with light gas. Under partition 6 you can inflate air. A pilot 7 controls a trapeze with hands 8th At the same time he pedaled propeller 9 or pump. Without air, delta-type aircraft will rise, with certain amount of air the unit will be heavier than air and must fly from the pilot's muscle drive.

Auf 3 ist ein Flugschiff gezeigt. Volumen 10 ist mit leichtem Gas angefüllt. Unter der Trennwand 11 kann man Luft aufpumpen.On 3 is a ship shown. volume 10 is filled with light gas. Under the partition 11 you can inflate air.

Auf 4 ist eine Wasserlandung vom Flugschiff gezeigt. Passagiere aus germetischen, glasbedeckten Raum 12 können Unterwasserwelt beobachten. Mit der Treppe oder Aufzug 13 können Passagiere aussteigen.On 4 is a water landing shown by the ship. Passengers from germetic, glass-covered room 12 can watch underwater life. With the stairs or elevator 13 passengers can get off.

Ohne Luft unter Trennwand 11 muss der Flugschiff vom Wasser erheben.Without air under partition 11 the airship must raise from the water.

Es ist möglich, das vorgeschlagenes Fluggerät kann für Erforschungen anderen mit Atmosphäre bedeckten Planeten benutzen.It is possible, the proposed aircraft can for Use explorations in other atmosphere-covered planets.

Claims (6)

Das Fluggerät mit dem geschlossenen, gasundurchlässigen, undehnbaren, leichten Raum, dadurch gekennzeichnet, das der Raum hat drinnen zusätzliche biegsame Trennwand, in eine Seite von Trennwand ist leichter Gas angefüllt und in andere kann Atmosphärengas aufpumpen oder durch eine Klappe ausgehen lassen.The aircraft with the closed, gas-impermeable, ineptable, lightweight space, characterized in that the space inside has an additional flexible partition, in one side of the partition light gas is filled and in others atmospheric gas can be inflated or let out through a flap. Das Fluggerät nach Patentanspruch 1, dadurch gekennzeichnet, das Gasraum vom Fluggerät muss so berechnet sein, das Fluggerät mit angefülltem mit leichtem Gas Raum und ohne Atmosphärengas muss sich bis bestimmte Höhe erheben, während atmosphärengasaufpumpen muss sich senken und bei Bestimmten Menge vom Atmosphärengas muss das Fluggerät landen.The aircraft according to claim 1, characterized in that the gas space of the aircraft must be calculated so that the aircraft with filled with light gas space and without atmosphere gas must rise to a certain height, currency Atmospheric gas pumping must lower and at certain amount of atmospheric gas the aircraft must land. Das Fluggerät nach Patentansprüche 1 und 2, dadurch gekennzeichnet, das ohne leichter Gas bei offener Klappe kann man warmen Atmosphärengas aufpumpen und Fluggerät in ein Heizluftballon verwandeln.The aircraft according to claims 1 and 2, characterized in that without light gas when open Flap can inflate warm atmospheric gas and aircraft turn into a hot air balloon. Das Fluggerät nach Patentansprüche 1 und 2, dadurch gekennzeichnet, das Fluggerät z.B. ein Deltaflugzeug mit dem Deltaflügel (Gasraum), dem Luftschraube, der Pumpe, der Klappe, dem Pedalenantrieb ausgestattet ist und kann im Flug als Fluggerät schwerer als Luft von Pilotsmuskel antreiben.The aircraft according to claims 1 and 2, characterized in that the aircraft is e.g. a delta plane with the delta wing (Gas space), the propeller, the pump, the flap, the pedal drive is equipped and can in flight as an aircraft heavier than air from pilot muscle drive. Das Fluggerät nach Patentansprüche 1, 2 und 3, dadurch gekennzeichnet, das Passagierraum germetisch, mit Aufzug und (oder) mit Treppe anfertigt ist und kann auf Wasser landen und vom Wasser erheben.The aircraft according to claims 1, 2 and 3, characterized, the passenger compartment germetisch, Made with lift and (or) with stairs and can be on water land and rise from the water. Das Fluggerät nach Patentansprüche 1, 2, 3, 4 und 5, dadurch gekennzeichnet, das Fluggerät kann für Erforschungen anderen mit Atmosphären bedeckten Planeten benutzen.The aircraft according to claims 1, 2, 3, 4 and 5, characterized, the aircraft can for explorations others with atmospheres use covered planet.
DE200410010549 2004-03-04 2004-03-04 Flying device used as a hot air balloon comprises a closed gas-impermeable chamber with an additional bendable separating wall Ceased DE102004010549A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
DE200410010549 DE102004010549A1 (en) 2004-03-04 2004-03-04 Flying device used as a hot air balloon comprises a closed gas-impermeable chamber with an additional bendable separating wall
DE200410025795 DE102004025795A1 (en) 2004-03-04 2004-05-26 Air-water underwater craft comprises a closed gas-impermeable light chamber divided into two chambers by a flexible wall

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200410010549 DE102004010549A1 (en) 2004-03-04 2004-03-04 Flying device used as a hot air balloon comprises a closed gas-impermeable chamber with an additional bendable separating wall

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DE102004010549A1 true DE102004010549A1 (en) 2005-09-29

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007046412A1 (en) 2007-09-28 2009-05-28 Alexandra Schuster Aircraft C for use in muscular arm pushing mechanism, comprises hermetic space which is filled with light gas, where inner volume of space is increased or decreased with constant quantity of light gas
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

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1345288A (en) * 1972-10-10 1974-01-30 Pedrick A P Aerial ships supported by vacuum balls or other forms of evacuated vessels
FR2470049A1 (en) * 1979-11-26 1981-05-29 Onera (Off Nat Aerospatiale) Aerostatic balloon for exploration of planet atmosphere - carries altitude stabilising liquids changing between liquid and vapour states to maintain predetermined altitude
DE19722588A1 (en) * 1997-05-30 1998-12-03 Abb Patent Gmbh Aircraft based upon aerostatic lift
DE20108990U1 (en) * 2001-05-21 2001-12-06 John Helmut Zeppelin

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1345288A (en) * 1972-10-10 1974-01-30 Pedrick A P Aerial ships supported by vacuum balls or other forms of evacuated vessels
FR2470049A1 (en) * 1979-11-26 1981-05-29 Onera (Off Nat Aerospatiale) Aerostatic balloon for exploration of planet atmosphere - carries altitude stabilising liquids changing between liquid and vapour states to maintain predetermined altitude
DE19722588A1 (en) * 1997-05-30 1998-12-03 Abb Patent Gmbh Aircraft based upon aerostatic lift
DE20108990U1 (en) * 2001-05-21 2001-12-06 John Helmut Zeppelin

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007046412A1 (en) 2007-09-28 2009-05-28 Alexandra Schuster Aircraft C for use in muscular arm pushing mechanism, comprises hermetic space which is filled with light gas, where inner volume of space is increased or decreased with constant quantity of light gas
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

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8122 Nonbinding interest in granting licenses declared
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