GB119837A - Improvements in Airships. - Google Patents

Improvements in Airships.

Info

Publication number
GB119837A
GB119837A GB892218A GB892218A GB119837A GB 119837 A GB119837 A GB 119837A GB 892218 A GB892218 A GB 892218A GB 892218 A GB892218 A GB 892218A GB 119837 A GB119837 A GB 119837A
Authority
GB
United Kingdom
Prior art keywords
girder
aerostats
fitted
windows
rear end
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
GB892218A
Inventor
William Robert Douglas Shaw
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 GB892218A priority Critical patent/GB119837A/en
Publication of GB119837A publication Critical patent/GB119837A/en
Expired legal-status Critical Current

Links

Classifications

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

Abstract

119,837. Shaw, W. R. D. May 30, 1918. Aerial machines withaerostats; aerostats; cars and cabins planes, arrangement of.- An airship comprises a girder a, a' of T-form to which are attached aerostats b, c, d. The girder is covered with fabric and serves to carry passengers, guns, &c., being fitted with a look-out a<2>, doors a<4>, and windows or gun apertures in the sides of the horizontal portion a. The rear end of the horizontal portion a extends each side of the aerostat to form a tail-plane to which elevators h are attached, the upper surface of the tailplane being fitted with windows. The part a' of the girder forms a keel, to the rear end of which the rudder g is hinged. The aerostats may be detachably connected to the girder by means of rings and safety-hooks. Land wheels a<3> are fitted as shown. Propelling.-Motors k are arranged at opposite sides of the girder portion a for driving propellers m.
GB892218A 1918-05-30 1918-05-30 Improvements in Airships. Expired GB119837A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB892218A GB119837A (en) 1918-05-30 1918-05-30 Improvements in Airships.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB892218A GB119837A (en) 1918-05-30 1918-05-30 Improvements in Airships.

Publications (1)

Publication Number Publication Date
GB119837A true GB119837A (en) 1918-10-17

Family

ID=32407959

Family Applications (1)

Application Number Title Priority Date Filing Date
GB892218A Expired GB119837A (en) 1918-05-30 1918-05-30 Improvements in Airships.

Country Status (1)

Country Link
GB (1) GB119837A (en)

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