DE246199C - - Google Patents
Info
- Publication number
- DE246199C DE246199C DENDAT246199D DE246199DA DE246199C DE 246199 C DE246199 C DE 246199C DE NDAT246199 D DENDAT246199 D DE NDAT246199D DE 246199D A DE246199D A DE 246199DA DE 246199 C DE246199 C DE 246199C
- Authority
- DE
- Germany
- Prior art keywords
- balloons
- spherical
- ring
- cross
- section
- 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.)
- Active
Links
- 239000003351 stiffener Substances 0.000 claims description 2
- 210000002356 Skeleton Anatomy 0.000 claims 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminum Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Classifications
-
- 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
- B64B1/60—Gas-bags surrounded by separate containers of inert gas
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Description
KAISERLICHESIMPERIAL
PATENTAMT.PATENT OFFICE.
Luftschiffe mit mehreren im Innern des Ballons befindlichen Einzelballons in Kugelform sind bereits bekannt.Airships with several individual balloons in the shape of a sphere inside the balloon are already known.
Gegenstand der Erfindung ist ein Luftschiff, bei dem die Zwischenräume zwischen den in dem Tragkörperhohlraum untergebrachten Kugelballons durch Ringballons von dreieckigem, elliptischem oder kreisförmigem Querschnitt ausgefüllt werden, wobei die Ringballons zwischen geeignete Querversteifungen eingebaut sind.The invention relates to an airship in which the spaces between the ball balloons accommodated in the support body cavity by ring balloons from triangular, elliptical or circular cross-section, the ring balloons suitable cross stiffeners are installed between them.
Die Zeichnung veranschaulicht den Erfindungsgegenstand in beispielsweiser Ausführungsform. The drawing illustrates the subject matter of the invention in an exemplary embodiment.
Fig. ι zeigt den Ballon in senkrechtem Längsschnitt; die Kugelballons sind in Ansicht, die Ringballons durchgeschnitten gezeichnet. Fig. Ι shows the balloon in a vertical longitudinal section; the spherical balloons are in view, the ring balloons drawn cut through.
Fig. 2 stellt den Querschnitt in der Ebene x-y dar.Fig. 2 shows the cross section in the xy plane.
Die äußere Hülle Hx des Luftschiffes vorliegender Erfindung (Fig. 1) spannt sich über Längsträger L aus Aluminium, Holz oder sehr dünnem Stahl, die den Hüllkurven entsprechen. Der zwischen den Trägern verbleibende Hohlraum ist mit einer Reihe gewöhnlicher Kugelballons B ausgefüllt. Die Längsträger sind untereinander durch ringförmige Gitterträger G1 bis G12 verbunden, die senkrecht zur Längsschiffmittelachse stehen. Diese ringförmigen Träger G1 bis G12 sind wiederum durch rundumlaufende Dreiecksverbände versteift, derart, daß die Streben S dieses DreiecKsverbandes als Tangenten von einem innen liegenden Ringe an die Oberfläche der Kugelballons B oder diesen Tangenten parallel geführt sind. Zwischen den Kugelballons B, die wegen ihrer gleichmäßigen Beanspruchung besonders geeignet erscheinen, verbleiben also ringförmige Hohlräume R von dreieckigem Querschnitt. Diese ringförmigen Hohlräume werden durch eine Reihe von sogenannten Ringballons B'', die sich entweder der Dreiecksform anpassen oder elliptischen oder kreisförmigen Querschnitt haben können, ausgefüllt. The outer shell H x of the airship of the present invention (Fig. 1) spans over longitudinal beams L made of aluminum, wood or very thin steel, which correspond to the envelope curves. The cavity remaining between the beams is filled with a series of ordinary spherical balloons B. The longitudinal girders are connected to one another by ring-shaped lattice girders G 1 to G 12 , which are perpendicular to the central axis of the longitudinal ship. These annular supports G 1 to G 12 are in turn stiffened by circumferential triangular associations in such a way that the struts S of this triangular association are guided as tangents from an inner ring to the surface of the spherical balloons B or these tangents. Thus, annular cavities R of triangular cross-section remain between the spherical balloons B, which appear particularly suitable because of their uniform stress. These annular cavities are filled by a series of so-called ring balloons B ″, which either adapt to the triangular shape or can have an elliptical or circular cross section.
Claims (2)
Publications (1)
Publication Number | Publication Date |
---|---|
DE246199C true DE246199C (en) |
Family
ID=505098
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DENDAT246199D Active DE246199C (en) |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE246199C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4023112A1 (en) * | 1990-07-20 | 1992-01-23 | Dornier Luftfahrt | Balloon for operating at high altitude - is divided into part volumes by circumferential cords |
-
0
- DE DENDAT246199D patent/DE246199C/de active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4023112A1 (en) * | 1990-07-20 | 1992-01-23 | Dornier Luftfahrt | Balloon for operating at high altitude - is divided into part volumes by circumferential cords |
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