GB258918A - Dirigible flying machines - Google Patents

Dirigible flying machines

Info

Publication number
GB258918A
GB258918A GB1456225A GB1456225A GB258918A GB 258918 A GB258918 A GB 258918A GB 1456225 A GB1456225 A GB 1456225A GB 1456225 A GB1456225 A GB 1456225A GB 258918 A GB258918 A GB 258918A
Authority
GB
United Kingdom
Prior art keywords
framework
members
girders
frames
diagonal
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
GB1456225A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB1456225A priority Critical patent/GB258918A/en
Publication of GB258918A publication Critical patent/GB258918A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Bridges Or Land Bridges (AREA)

Abstract

258,918. Strauss, J. B. June 4, 1925. Airships; aerostats.-The aerostat framework of a rigid airship comprises two flat side frames united by top and .bottom cross members, the interior space being divided by diagonal bracing members into sections each adapted to contain a gas cell. In the construction shown in Figs. 2 and 4, the side frames 1, .2 are formed of longitudinal girders 9 and upright girders 6 braced by diagonal members 7, and are joined by horizontal members 3 provided with enlarged connecting ends. The diagonal bracing members 8 divide the interior into open sections. The top and bottom of the framework are connected by secondary frames 10 connected to the side frames 1, 2 and the horizontal members 3 and joined by longitudinal girders 11. Coffin-shaped gas cells fill the 'space between adjacent secondary frames 10 as well as the space between adjacent diagonal braces 8. According to a modifled construction, the main framework formed by the flat sides 2<b>, Fig. 5, and the horizontal members 3a, is of square cross-section, and secondary frames 10a are connected to all the sides to form a circular section. Square gas cells are located in the central portion of the framework and peripheral segmental gas cells occupy the spaces between the secondary frames 10a. All the girders comprising the framework are of triangular truss construction. Cars and cabins.-Cars 13a, Fig. 2, are suspended from supports 12a connected to the upright girders 6.
GB1456225A 1925-06-04 1925-06-04 Dirigible flying machines Expired GB258918A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1456225A GB258918A (en) 1925-06-04 1925-06-04 Dirigible flying machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1456225A GB258918A (en) 1925-06-04 1925-06-04 Dirigible flying machines

Publications (1)

Publication Number Publication Date
GB258918A true GB258918A (en) 1926-10-04

Family

ID=10043453

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1456225A Expired GB258918A (en) 1925-06-04 1925-06-04 Dirigible flying machines

Country Status (1)

Country Link
GB (1) GB258918A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2662995A1 (en) * 1990-06-12 1991-12-13 Zeppelin Luftschiffbau Dirigible with a skeleton consisting of triangular ribs and of longerons

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2662995A1 (en) * 1990-06-12 1991-12-13 Zeppelin Luftschiffbau Dirigible with a skeleton consisting of triangular ribs and of longerons

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