GB304889A - Improvements in or relating to lighter-than-air aircraft - Google Patents

Improvements in or relating to lighter-than-air aircraft

Info

Publication number
GB304889A
GB304889A GB3439727A GB3439727A GB304889A GB 304889 A GB304889 A GB 304889A GB 3439727 A GB3439727 A GB 3439727A GB 3439727 A GB3439727 A GB 3439727A GB 304889 A GB304889 A GB 304889A
Authority
GB
United Kingdom
Prior art keywords
propellers
airship
engines
tail
fins
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
GB3439727A
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.)
AIRSHIP GUARANTEE CO Ltd
Original Assignee
AIRSHIP GUARANTEE CO Ltd
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 AIRSHIP GUARANTEE CO Ltd filed Critical AIRSHIP GUARANTEE CO Ltd
Priority to GB3439727A priority Critical patent/GB304889A/en
Publication of GB304889A publication Critical patent/GB304889A/en
Expired legal-status Critical Current

Links

Classifications

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

Abstract

304,889. Airship Guarantee Co., Ltd., and Burney, C. D. Dec. 19, 1927. Propelling; steering and balancing. - An airship has its propelling machinery arranged close to the tail portion aft of the fins for driving propellers outside the envelope or in or close to one or more of the tail fins for driving propellers at the sides of the fins. One or more engines may be arranged within the tail compartment or the fin and drive propellers indirectly, or a separate engine may be direct-coupled to each propeller and mounted so that it can be swung inboard when required. Fig. 2 shows one of a series of engines 3 and propellers arranged in a ring about the tail of the airship. Each engine is mounted on a frame 4 normally connected to the axial girder of the airship but adapted to swing about pivots on the outer frame when it is required, to attend to the engine. The frames 4 may be constructed to rotate about their own axes so as to adjust the line of thrust of the propellers. Propellers 7 on opposite sides of a keel fin 2 also are shown driven through bevel gear and transverse shafts from engines 5 within the fin. Access to the engines from a passage 9 is obtained by ladders 8. The propellers are rotatable about the transverse shafts to vary their line of thrust, particularly for varying the trim of the airship at a mooring mast. Specifications 250,330 and 259,264 are referred to.
GB3439727A 1927-12-19 1927-12-19 Improvements in or relating to lighter-than-air aircraft Expired GB304889A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3439727A GB304889A (en) 1927-12-19 1927-12-19 Improvements in or relating to lighter-than-air aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3439727A GB304889A (en) 1927-12-19 1927-12-19 Improvements in or relating to lighter-than-air aircraft

Publications (1)

Publication Number Publication Date
GB304889A true GB304889A (en) 1929-01-31

Family

ID=10365133

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3439727A Expired GB304889A (en) 1927-12-19 1927-12-19 Improvements in or relating to lighter-than-air aircraft

Country Status (1)

Country Link
GB (1) GB304889A (en)

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