DE371954C - Gas discharge for rigid airships - Google Patents

Gas discharge for rigid airships

Info

Publication number
DE371954C
DE371954C DEL46168D DEL0046168D DE371954C DE 371954 C DE371954 C DE 371954C DE L46168 D DEL46168 D DE L46168D DE L0046168 D DEL0046168 D DE L0046168D DE 371954 C DE371954 C DE 371954C
Authority
DE
Germany
Prior art keywords
gas discharge
rigid airships
gas
air
shaft
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.)
Expired
Application number
DEL46168D
Other languages
German (de)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
LUFTFAHRZEUGBAU SCHUETTE LANZ
Original Assignee
LUFTFAHRZEUGBAU SCHUETTE LANZ
Publication date
Priority to DEL46168D priority Critical patent/DE371954C/en
Application granted granted Critical
Publication of DE371954C publication Critical patent/DE371954C/en
Expired legal-status Critical Current

Links

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
    • B64B1/64—Gas valve operating mechanisms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Lowering Means (AREA)

Description

Gasabführung für Starrluftschiffe. Zusatz zum Patent 303968. Gegenüber der durch das Hauptpatent geschützten Vorrichtung besteht das Neue dieser Schachtanordnung in der völligen Ab.-schließung des gasführenden Kanals gegen das Innere des Luftschiffes; die zur Verdünnung des Gases notwendige Luft wird von außen mittels Druckhaube entnommen und in einem besonderen Kanal bis unter die Überdruckventile der Zellen geführt. Abb. r der Zeichnung zeigt einen Gasabführungsschacht a irre Längs- und Querschnitt durch das Luftschiff b; c ist der Luftkanal. Die gestrichelten Pfeile zeigen den Weg der von außen einströmenden Luft, die ausgezogenen Pfeile den Weg des Gas- und Luftgemisches im Schacht a an. Bei Abb. z der Zeichnung erfolgt die Luftzufuhr durch das von oben mündende Rohr c; das Rohr c kann auch seitlich der Mittellinie des Schiffsrumpfes münden. Die Vorteile der neuen Anordnung bestehen in der Zwangläufigkeit der Bewegung der an den Ventilen freiwerdenden Gasmengen, in der besseren Regulierbarkeit der Verdünnung des Gases und in der vollkommenen Ventilierung des Schachtes mittels der zwangläufig eingeführten Luft; die Explosionsgefahr wird hierbei erheblich eingeschränkt.Gas evacuation for rigid airships. Addition to patent 303968. Compared to the device protected by the main patent, the novelty of this shaft arrangement consists in the complete closure of the gas-carrying channel from the interior of the airship; the air required to dilute the gas is taken from the outside by means of a pressure hood and guided in a special channel under the pressure relief valves of the cells. Fig. R of the drawing shows a gas discharge shaft a wrong longitudinal and cross-section through the airship b; c is the air duct. The dashed arrows show the path of the air flowing in from the outside, the solid arrows the path of the gas and air mixture in shaft a. In Fig. Z of the drawing, the air is supplied through the tube c opening from above; the pipe c can also open laterally to the center line of the ship's hull. The advantages of the new arrangement consist in the inevitability of the movement of the gas quantities released at the valves, in the better controllability of the dilution of the gas and in the perfect ventilation of the shaft by means of the inevitably introduced air; the risk of explosion is considerably reduced.

Claims (1)

PATENTANSPRUCH: Gasabführung für Starrluftschiffe nach Patent 303968, dadurch gekennzeichnet, daß der Abführungsschacht als völlig gegen das Innere des Luftschiffes abeschk>ssener Kanal (c) ausgebildet ist, dem die Außenluft durch eine oberhalb, unterhalb oder seitlich aus dem Tragkörper hervorrageirde, gegen die Fahrtrichtung gestellte Einmündungshaube zugeführt wird. PATENT CLAIM: Gas discharge for rigid airships according to patent 303968, characterized in that the discharge shaft is designed as a duct (c) which is completely cut off from the interior of the airship and through which the outside air protrudes through an above, below or to the side of the supporting body, against the direction of travel provided confluence hood is supplied.
DEL46168D Gas discharge for rigid airships Expired DE371954C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEL46168D DE371954C (en) Gas discharge for rigid airships

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEL46168D DE371954C (en) Gas discharge for rigid airships

Publications (1)

Publication Number Publication Date
DE371954C true DE371954C (en) 1923-03-22

Family

ID=7271479

Family Applications (1)

Application Number Title Priority Date Filing Date
DEL46168D Expired DE371954C (en) Gas discharge for rigid airships

Country Status (1)

Country Link
DE (1) DE371954C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623721A (en) * 1945-12-18 1952-12-30 George P Harrington Aircraft structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623721A (en) * 1945-12-18 1952-12-30 George P Harrington Aircraft structure

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