DE19812704A1 - Double hull airship - Google Patents
Double hull airshipInfo
- Publication number
- DE19812704A1 DE19812704A1 DE1998112704 DE19812704A DE19812704A1 DE 19812704 A1 DE19812704 A1 DE 19812704A1 DE 1998112704 DE1998112704 DE 1998112704 DE 19812704 A DE19812704 A DE 19812704A DE 19812704 A1 DE19812704 A1 DE 19812704A1
- Authority
- DE
- Germany
- Prior art keywords
- airship
- supporting
- supporting structure
- double hull
- hulls
- Prior art date
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
Description
Gegenstand vorliegender Anmeldung ist ein Luftschiff, das im Gegensatz zu den herkömmlichen mit zwei (oder mehr) Tragkörpern ausgerüstet ist. Dadurch wird eine größere Sicherheit und höhere Tragfähigkeit des Luftschiffes erzielt.The subject of the present application is an airship which in contrast to the conventional with two (or more) supporting bodies is equipped. This will provide greater security and increased load capacity of the airship.
Auf dazugehöriger Zeichnung ist ein Ausführungsbeispiel dargestellt, bei dem das Traggerüst mit der (den) Gondel(n) 1 an den Tragkörpern 2 angeordnet ist.In the accompanying drawing, an exemplary embodiment is shown in which the supporting structure with the nacelle (s) 1 is arranged on the supporting bodies 2 .
Die Antriebsmotoren 3 können wie bisher am Ende der Tragkörper, aber auch am Traggerüst befestigt werden. Auf diese Weise könnte die Anzahl der Motoren und damit die Geschwindigkeit des Luftschiffes erhöht werden.As before, the drive motors 3 can be attached to the end of the supporting body, but also to the supporting structure. In this way, the number of engines and thus the speed of the airship could be increased.
Die Steuerruder 4 können ebenfalls an den Tragkörpern oder am Traggerüst angeordnet werden.The rudder 4 can also be arranged on the supporting bodies or on the supporting structure.
Innerhalb des Traggerüstes können wahlweise eine oder mehrere Gondeln aufgereiht werden.One or more can optionally be placed within the supporting structure Gondolas to be lined up.
Wie bereits eingangs erwähnt, können bei diesem Luftschiff-Typ zwei oder mehr Tragkörper verwendet werden. Auf diese Weise können Großraum-Luftschiffe gebaut werden, die bei den bisherigen Luftschiffen mit lediglich einem Tragkörper nicht möglich waren.As already mentioned at the beginning, this type of airship can two or more supporting bodies can be used. In this way Large-format airships can be built, as in the previous ones Airships with only one supporting body were not possible.
Claims (1)
- 1. es im Gegensatz zu den herkömmlichen mit zwei (oder mehr) Tragkörpern ausgerüstet ist, wodurch eine größere Sicherheit und höhere Tragfähigkeit des Luftschiffes erzielt wird,
- 2. ein Ausführungsbeispiel dieser Luftschiffart auf dazugehöriger Zeichnung dargestellt ist, bei dem das Traggerüst mit der (den) Gondel(n) (1) an den Tragkörpern (2) angeordnet ist,
- 3. die Antriebsmotoren (3) wie bisher am Ende der Tragkörper oder auch am Traggerüst befestigt werden können, wodurch die Anzahl der Motoren und damit die Reisegeschwindigkeit erhöht werden kann,
- 4. die Steuerruder (4) ebenfalls an den Tragkörpern oder am Traggerüst angeordnet werden können,
- 5. innerhalb des Traggerüstes wahlweise eine oder mehrere Gondeln aufgereiht werden können,
- 6. auf diese Art und Weise Großraum-Luftschiffe gebaut werden können, die völlig neue Perspektiven in der Luftschiffahrt ermöglichen.
- 1. in contrast to the conventional one, it is equipped with two (or more) supporting bodies, which results in greater security and higher carrying capacity of the airship,
- 2. an embodiment of this type of airship is shown in the accompanying drawing, in which the supporting structure with the nacelle (s) ( 1 ) is arranged on the supporting bodies ( 2 ),
- 3. the drive motors ( 3 ) can be fastened to the end of the support body or to the support frame as before, as a result of which the number of motors and thus the cruising speed can be increased,
- 4. the rudders ( 4 ) can also be arranged on the supporting bodies or on the supporting structure,
- 5. one or more gondolas can optionally be lined up within the supporting structure,
- 6. Large-scale airships can be built in this way, which open up completely new perspectives in airship travel.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1998112704 DE19812704A1 (en) | 1998-03-23 | 1998-03-23 | Double hull airship |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1998112704 DE19812704A1 (en) | 1998-03-23 | 1998-03-23 | Double hull airship |
Publications (1)
Publication Number | Publication Date |
---|---|
DE19812704A1 true DE19812704A1 (en) | 1999-10-07 |
Family
ID=7861982
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1998112704 Withdrawn DE19812704A1 (en) | 1998-03-23 | 1998-03-23 | Double hull airship |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE19812704A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2841531A1 (en) * | 2002-06-27 | 2004-01-02 | Christophe Loustaudaudine | LIGHTER-AIR AIRCRAFT COMPRISING SEVERAL BALLOONS CONNECTED BY A CHASSIS |
FR2841530A1 (en) * | 2002-06-27 | 2004-01-02 | Christophe Loustaudaudine | Stationary radar mission lighter-than-air aircraft having two balloons linked together forming chassis, with electromagnetic coupling formed between balloons |
-
1998
- 1998-03-23 DE DE1998112704 patent/DE19812704A1/en not_active Withdrawn
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2841531A1 (en) * | 2002-06-27 | 2004-01-02 | Christophe Loustaudaudine | LIGHTER-AIR AIRCRAFT COMPRISING SEVERAL BALLOONS CONNECTED BY A CHASSIS |
FR2841530A1 (en) * | 2002-06-27 | 2004-01-02 | Christophe Loustaudaudine | Stationary radar mission lighter-than-air aircraft having two balloons linked together forming chassis, with electromagnetic coupling formed between balloons |
WO2004002819A1 (en) * | 2002-06-27 | 2004-01-08 | Bertholet, Christophe | Lighter-than-air aircraft comprising several balloons linked by a chassis |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8139 | Disposal/non-payment of the annual fee |