US1724009A - Rigid airship with separate gas cells - Google Patents

Rigid airship with separate gas cells Download PDF

Info

Publication number
US1724009A
US1724009A US603603A US60360322A US1724009A US 1724009 A US1724009 A US 1724009A US 603603 A US603603 A US 603603A US 60360322 A US60360322 A US 60360322A US 1724009 A US1724009 A US 1724009A
Authority
US
United States
Prior art keywords
gas
cells
ship
separate gas
cell
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 - Lifetime
Application number
US603603A
Inventor
Eckener Hugo
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.)
Luftschiffbau Zeppelin GmbH
Original Assignee
Luftschiffbau Zeppelin GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Luftschiffbau Zeppelin GmbH filed Critical Luftschiffbau Zeppelin GmbH
Application granted granted Critical
Publication of US1724009A publication Critical patent/US1724009A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/58Arrangements or construction of gas-bags; Filling arrangements
    • B64B1/62Controlling gas pressure, heating, cooling, or discharging gas

Definitions

  • My invention has reference/to air ships, more particularly of the rigid type, with separate gas cells, and it particularly refers to means for preventing destruction of ships of this kind by. fire and lightning.
  • the suggestions heretofore made for the utilization of a non-inflammable carrying gas for air ships were objectionable both on account of the comparative rarity and the resulting high costs of production of such gases, and in view of the increased specific gravity which, for instance in the case of helium, is the double of hydrogen.
  • the suggestions heretofore made of providing ⁇ the air ship with a jacket of nitrogen surrounding the gas cells because the loss of buoyancy incumbent thereon is excessive, aside from the complicated constructionand the high costs of a complete jacketof nitro-.-
  • My invention contemplates the utilization of non-inflammable carrying gases by providing non-infiammable gas of low specific gravity such as helium only at such points of the ship which are particularly exposed to lightning strokes, especially the front or bow portion, and at the sections above the Engines which are particularly liable to take Strokes of lightning, as shown by experience, 'are liable to occur at the ends of the air ship only.
  • non-infiammable gas of low specific gravity such as helium only at such points of the ship which are particularly exposed to lightning strokes, especially the front or bow portion, and at the sections above the Engines which are particularly liable to take Strokes of lightning, as shown by experience, 'are liable to occur at the ends of the air ship only.
  • the widely projecting portions of the balancing and steering surfaces which are not filled with gas, keep the lightning away from the gas in the hull so that at this point there is no obvious necessity of special protec-A tion by an incombustiblegas.
  • Such gas of low specific gravity should
  • Means are also prvided in the practice of my invention for the preyention of losses of the expensive carrying gas caused by expansion due to the outer air pressure While the air ship rises or when the temperature of the gas increases. Such losses of gas can be prevented by a reinforcement of the walls of the particular cells or compartments, thus rendering them capable of withstanding a higher pressure, and further by the provision of special expansion chambers into which the incombustible carrying gas is linfiammable gas.
  • Fig. l is a longitudinal section, while Fig. 2' illustrates the bow of the ship on a somewhat enlarged scale.
  • an air ship of the rigid type is shown with the outer envelop t surrounding the skeleton hull (not shown).
  • the cells Z) are filled with hydrogen gas, while the cells c at the bow of the ship for about a quarter up to about one-fifth of the length of the ship are filled with an incombustible gas of low specific gravity, suchV -as helium.
  • the motor gondolas are indicated at d'. Above these gondolas separate small helium cells'e are arranged, and similar separatephelium cells may also be provided above the passenger-cabins.
  • the helium cells c are provided with a protective coating f.
  • the three helium cells c communicate by way of openings la, with a collapsible cell g mounted in the interior of the hydrogen cell b. f
  • An airship comprising a motor gondola
  • An airship comprising a plurality of gas cells, a bow cell being filled with a noninflammable carrying gas, other cells with an inflammable gas, the Walls of said bow cell being stronger than those of the other cells.

Description

Aug. 13, 1929. H. ECKENER RIGID AIRSHIP WITH SEPARATE GAS CELLS Filed Nov. 27. 1922 JNVENTR'.
Patented Aug. v13, 1929.
UNITED STATES v1,724,009 PATENT OFFICE.
HUGO ECKENER, 0F FRIEDRICHSHAFEN-O-THE-BODENSEIEL GERMANY, ASSIGNOR TO LUFTSCHIFFBAU ZEPPELIN GESELLSCHAFT MIT BESCHRNKTER HAFTUNG, OF 'FRIEDRICHSHAFEN-ON-THE-BGDENSEE, GERMANY.
RIGID .AIRSHIP WITH SEPARATE GAS CELLS.
Application led November 27, 1922, Serial No. 603,603, and n/GermanytSeptember 18, 1522.
My invention has reference/to air ships, more particularly of the rigid type, with separate gas cells, and it particularly refers to means for preventing destruction of ships of this kind by. fire and lightning. The suggestions heretofore made for the utilization of a non-inflammable carrying gas for air ships were objectionable both on account of the comparative rarity and the resulting high costs of production of such gases, and in view of the increased specific gravity which, for instance in the case of helium, is the double of hydrogen. Nor was it possible to arrive at practical results with the suggestions heretofore made of providing `the air ship with a jacket of nitrogen surrounding the gas cells because the loss of buoyancy incumbent thereon is excessive, aside from the complicated constructionand the high costs of a complete jacketof nitro-.-
'gen or a non-combustible carrying gas.
My invention contemplates the utilization of non-inflammable carrying gases by providing non-infiammable gas of low specific gravity such as helium only at such points of the ship which are particularly exposed to lightning strokes, especially the front or bow portion, and at the sections above the Engines which are particularly liable to take Strokes of lightning, as shown by experience, 'are liable to occur at the ends of the air ship only. At the rear end of the ship the widely projecting portions of the balancing and steering surfaces which are not filled with gas, keep the lightning away from the gas in the hull so that at this point there is no obvious necessity of special protec-A tion by an incombustiblegas. Such gas of low specific gravity should accordingly be applied only at the bow and above the motor gondolas.
Means are also prvided in the practice of my invention for the preyention of losses of the expensive carrying gas caused by expansion due to the outer air pressure While the air ship rises or when the temperature of the gas increases. Such losses of gas can be prevented by a reinforcement of the walls of the particular cells or compartments, thus rendering them capable of withstanding a higher pressure, and further by the provision of special expansion chambers into which the incombustible carrying gas is linfiammable gas.
the ship, by providing a fire-proof insertion or coating above the helium-filled cells with a .View to preventing fluid metal which might be detached from the metal skeleton of the air ship by melting in consequence of Y a stroke of lightning, from perforating the walls of the cells and allowing the gas to escape through the perforations.
Inasmuch as the special protective means employed may be restricted to those sections of the air ship which is particularly exposed to danger, the additional weight resulting therefrom is so small that it does not appreciably interfere with the carrying capacity of the air ship.
An airship embodying my invention is shown diagrammatically by way of exampletin the drawings annexed to this specification and forming part thereof.
Fig. l is a longitudinal section, while Fig. 2' illustrates the bow of the ship on a somewhat enlarged scale.
ln the drawing an air ship of the rigid type is shown with the outer envelop t surrounding the skeleton hull (not shown). The cells Z) are filled with hydrogen gas, while the cells c at the bow of the ship for about a quarter up to about one-fifth of the length of the ship are filled with an incombustible gas of low specific gravity, suchV -as helium. The motor gondolas are indicated at d'. Above these gondolas separate small helium cells'e are arranged, and similar separatephelium cells may also be provided above the passenger-cabins. In the modification shown inFigure 2 the helium cells c are provided with a protective coating f. The three helium cells c communicate by way of openings la, with a collapsible cell g mounted in the interior of the hydrogen cell b. f
My invention has been described with reference to its principal features Without limiting it to the particular forms of embodiment herein shown and described, for alterations and modications of such embodiments may occur Within the spirit of my invention as lthe conditions of utilization will direct, and
Within said latter cell communicating with said former cell and means connected with said latter cell for allowing the escape of inflammable gas therefrom.
2. An airship comprising a motor gondola,
a cell filled with a non-inflammable carrying gas, another cell-filled With inflammable gas, a collapsible cell Within said latter cell communicating Withsaid former cell and a communication between said latter cell and the motor gondola.
3. An airship comprising a plurality of gas cells, a bow cell being filled with a noninflammable carrying gas, other cells with an inflammable gas, the Walls of said bow cell being stronger than those of the other cells.
In testimony whereof I affix my signature.
HUGO ECKENER.
US603603A 1922-09-18 1922-11-27 Rigid airship with separate gas cells Expired - Lifetime US1724009A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1724009X 1922-09-18

Publications (1)

Publication Number Publication Date
US1724009A true US1724009A (en) 1929-08-13

Family

ID=7740694

Family Applications (1)

Application Number Title Priority Date Filing Date
US603603A Expired - Lifetime US1724009A (en) 1922-09-18 1922-11-27 Rigid airship with separate gas cells

Country Status (1)

Country Link
US (1) US1724009A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5285986A (en) * 1991-04-18 1994-02-15 Luftschiffbau Zeppelin Gmbh Rigid airship with a carrier frame of ribs and beams enclosed by skin sections forming an envelope

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5285986A (en) * 1991-04-18 1994-02-15 Luftschiffbau Zeppelin Gmbh Rigid airship with a carrier frame of ribs and beams enclosed by skin sections forming an envelope

Similar Documents

Publication Publication Date Title
GB1191321A (en) Airship
JPS62501407A (en) steerable aerostatic balloon
ATE457264T1 (en) UNMANNED AERIAL VEHICLE AS A PLATFORM FOR TELECOMMUNICATIONS OR OTHER SCIENTIFIC PURPOSES
US3185411A (en) Multiple celled airship
US1724009A (en) Rigid airship with separate gas cells
US3180590A (en) Pressurized airship
US1553087A (en) Lightning protection for aircraft
US1729020A (en) Airship
US1376121A (en) Kite, captive, or observation balloon
GB885298A (en) Improvements in or relating to tanker vessels
US1548336A (en) Gas cell of airships
US3210933A (en) Nozzle
US1679564A (en) Gas container for airships
US1900744A (en) Airship
US1695394A (en) Airship with mixed sustentation
US1642026A (en) Airship
US1857963A (en) Airship
GB228201A (en) Improvements in or relating to airships
CN212163750U (en) Shielding extension metal mesh for aircraft window
US1571833A (en) Submarine
RU2178370C1 (en) Airship
GB191400660A (en) Improvements in the Construction of Airships.
US1900743A (en) Airship
US1637774A (en) Gas-inflated airship
SU126382A1 (en) Ship pontoon