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US1620449A - Airship - Google Patents

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Publication number
US1620449A
US1620449A US43833A US4383325A US1620449A US 1620449 A US1620449 A US 1620449A US 43833 A US43833 A US 43833A US 4383325 A US4383325 A US 4383325A US 1620449 A US1620449 A US 1620449A
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US
United States
Prior art keywords
hull
axis
airship
cars
power car
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
US43833A
Inventor
Durr Ludwig
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.)
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Publication date
Application filed by Luftschiffbau Zeppelin GmbH filed Critical Luftschiffbau Zeppelin GmbH
Application granted granted Critical
Publication of US1620449A publication Critical patent/US1620449A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft

Definitions

  • My invention relates to gas inflated air-. ships having cars with motors and propellers for driving the ship through the air. Such airships generally have a huge gas inflated bag or hull from which the power cars are suspended. With big ships several power cars have to be arranged. The more-power units there are the greater is the reliability. On the other hand the propellers of such cars should not be too close together neither longitudinally or laterally because of the possibility of being influenced by each other.
  • Object of my invention is to do away with such drawbacks by inclining the axis of the propeller so that this axis and the tangent to the adjacent portion of the outer cover of the airship diverge towards the ships tail. This may be attained by lowering the rear end of the power car from its horizontal axis and also by moving its rear end outwardly from its normal position parallel to the airships axis. Or both of the described ways may be made use of at'the same time. The effect will always be that the air current of increased speed behind eachpropeller will have a direction outwardly from the airship.
  • Fig. 1 is the side view of an airship and Fig. 2*is a corresponding top view, the latter showing the suspended cars in dotted lines.
  • the airship hull is designated-by the let ter a.
  • Control car I and power cars 0, (Z, 6 and f are suspended from the hull a.
  • the axes of such cars are designated by the letters 0, d, e, and f respectively; while the corresponding propellers are shown at c", d", e", and f respectively.
  • the floor in the vertically inclined cars may be excepted from the inclination so that a horizontal floor may facilitate walking and 'working for the mechanician.
  • An airship comprising a hull; and a powercar suspended from said hull in fixed relation thereto; the axis of said power car being vertically inclined so that said axis and the axis of said hull diverge towards the ships tail.
  • An airship comprising a hull; and a power car suspended from said hull in fixed relation thereto; the horizontal axis of said power car and the horizontal axis of said hull diverging towards the ships tail.
  • An airship comprising a hull; and a power car suspended from said hull; the longitudinal axis of said hull and the longitudinal axis of said power car diverging horizontally and vertically towards the ships tail.
  • An airship comprising a hull; a power car suspended from said hull; and a propeller attached to said power car; the axis of said hull and the axis of said propeller being in fixed relation to each other and horlizontally diverging towards the ships tai 5.
  • An airship comprising a hull; a power car suspended from said hull; and a propeller attached to said power car; the axis of said hull and the axis of said propeller being in fixed relation to each other and vertically diverging towards the ships tail.
  • An airship comprising a hull; a power car suspended from said hull; and a propeller attached to said power car; the axis of said hull and the axis of said propellerbeing. in fixed relation to each other and diverging, towards the ships tail.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Description

March 8. 1927. 1,620,449
L. DURR AIRSHIP Filed July 15, 1925 imam/a r ydwzy JzZrrf Z13 Mir-hers Patented Mar. 8, 1927.
UNITED STATES PATENT OFFICE.
LUDWIG Dlj'RR, OF FRIEDRICHSHAFEN, GERMANY,\ASSIGNR To LUFTSGHIFFBAU ZEPIELIN GESELLSOHAFT MIT IBESCHRANKTER HAFTUNG, OF FBIEDRIGHSHAFEN,
IBODENSEE GERMANY. v
AIRSHIP.
Application filed July 15, 1925, Serial No. 48,833, and in Germany July 31, 1924.
My invention relates to gas inflated air-. ships having cars with motors and propellers for driving the ship through the air. Such airships generally have a huge gas inflated bag or hull from which the power cars are suspended. With big ships several power cars have to be arranged. The more-power units there are the greater is the reliability. On the other hand the propellers of such cars should not be too close together neither longitudinally or laterally because of the possibility of being influenced by each other.
Furthermore the air current increased in its speed behind each propeller will cause an increase of friction on the outer cover of the gas bag or hull and will also create an increase in its swinging movements.
Object of my invention is to do away with such drawbacks by inclining the axis of the propeller so that this axis and the tangent to the adjacent portion of the outer cover of the airship diverge towards the ships tail. This may be attained by lowering the rear end of the power car from its horizontal axis and also by moving its rear end outwardly from its normal position parallel to the airships axis. Or both of the described ways may be made use of at'the same time. The effect will always be that the air current of increased speed behind eachpropeller will have a direction outwardly from the airship.
Having given a general description of my invention I now want to explain it more in detail referring to the drawings which embody an example thereof.
Fig. 1 is the side view of an airship and Fig. 2*is a corresponding top view, the latter showing the suspended cars in dotted lines.
The airship hull is designated-by the let ter a. Control car I) and power cars 0, (Z, 6 and f are suspended from the hull a. The axes of such cars are designated by the letters 0, d, e, and f respectively; while the corresponding propellers are shown at c", d", e", and f respectively.
From Fig. 1 it will be seen in which manner the vertical inclination of the power car axis may be designed.- In this example car 0 is even more inclined than car e, which is not absolutely necessary as both cars are laterally distanced from each other as may be seen from Fig. 2. In this figure the horizontal divergency of the axis of the different cars is shown, which needs no special explanation.
' According to my invention the floor in the vertically inclined cars may be excepted from the inclination so that a horizontal floor may facilitate walking and 'working for the mechanician.
I do not want to limit myself to the ex ample described orshown in the drawings as many variations will occur to those skilled in the art.
What I claim is: g
1. An airship comprisinga hull; and a powercar suspended from said hull in fixed relation thereto; the axis of said power car being vertically inclined so that said axis and the axis of said hull diverge towards the ships tail.
2. An airship comprising a hull; and a power car suspended from said hull in fixed relation thereto; the horizontal axis of said power car and the horizontal axis of said hull diverging towards the ships tail.
3. An airship comprising a hull; and a power car suspended from said hull; the longitudinal axis of said hull and the longitudinal axis of said power car diverging horizontally and vertically towards the ships tail. v
4. An airship comprising a hull; a power car suspended from said hull; and a propeller attached to said power car; the axis of said hull and the axis of said propeller being in fixed relation to each other and horlizontally diverging towards the ships tai 5. An airship comprising a hull; a power car suspended from said hull; and a propeller attached to said power car; the axis of said hull and the axis of said propeller being in fixed relation to each other and vertically diverging towards the ships tail.
6. An airship comprising a hull; a power car suspended from said hull; and a propeller attached to said power car; the axis of said hull and the axis of said propellerbeing. in fixed relation to each other and diverging, towards the ships tail. r
DR.\LUDWIG DURR.
US43833A 1924-07-31 1925-07-15 Airship Expired - Lifetime US1620449A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1620449X 1924-07-31

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US1620449A true US1620449A (en) 1927-03-08

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US43833A Expired - Lifetime US1620449A (en) 1924-07-31 1925-07-15 Airship

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070075184A1 (en) * 2005-10-05 2007-04-05 Marimon Thomas L Direct mounted propulsion for non-rigid airships

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070075184A1 (en) * 2005-10-05 2007-04-05 Marimon Thomas L Direct mounted propulsion for non-rigid airships
US7448572B2 (en) * 2005-10-05 2008-11-11 Lockheed Martin Corporation Direct mounted propulsion for non-rigid airships

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