GB119974A - Improvements in or relating to the Tail Fins of Aeroplanes or other Aircraft. - Google Patents

Improvements in or relating to the Tail Fins of Aeroplanes or other Aircraft.

Info

Publication number
GB119974A
GB119974A GB1373/18A GB137318A GB119974A GB 119974 A GB119974 A GB 119974A GB 1373/18 A GB1373/18 A GB 1373/18A GB 137318 A GB137318 A GB 137318A GB 119974 A GB119974 A GB 119974A
Authority
GB
United Kingdom
Prior art keywords
spar
aeroplanes
aircraft
fin
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
GB1373/18A
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.)
HARRIS BOOTH
Blackburn Aeroplane and Motor Co Ltd
Original Assignee
HARRIS BOOTH
Blackburn Aeroplane and Motor 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 HARRIS BOOTH, Blackburn Aeroplane and Motor Co Ltd filed Critical HARRIS BOOTH
Priority to GB1373/18A priority Critical patent/GB119974A/en
Publication of GB119974A publication Critical patent/GB119974A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Abstract

119,974. Blackburn Aeroplane & Motor Co., and Booth, H. Jan. 24, 1918. Planes, arrangement and construction of.-Tail fins for aeroplanes and other aircraft are constructed with two vertical spars extending into the fuselage, either the front or rear spar being laterally flexible and the other spar rigid so that the effectiveness of the fin shall be respectively increased or diminished with increase of speed. Fig. 1 shows a fin 2 having a flexible rear spar 5 and rigid front spar 4 extending into the fuselage. A rudder 3 is pivoted to the rear edge of the fin.
GB1373/18A 1918-01-24 1918-01-24 Improvements in or relating to the Tail Fins of Aeroplanes or other Aircraft. Expired GB119974A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1373/18A GB119974A (en) 1918-01-24 1918-01-24 Improvements in or relating to the Tail Fins of Aeroplanes or other Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1373/18A GB119974A (en) 1918-01-24 1918-01-24 Improvements in or relating to the Tail Fins of Aeroplanes or other Aircraft.

Publications (1)

Publication Number Publication Date
GB119974A true GB119974A (en) 1918-10-24

Family

ID=32407403

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1373/18A Expired GB119974A (en) 1918-01-24 1918-01-24 Improvements in or relating to the Tail Fins of Aeroplanes or other Aircraft.

Country Status (1)

Country Link
GB (1) GB119974A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009016094A2 (en) 2007-07-27 2009-02-05 Airbus España S.L. Aircraft tail assembly

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009016094A2 (en) 2007-07-27 2009-02-05 Airbus España S.L. Aircraft tail assembly
WO2009016094A3 (en) * 2007-07-27 2009-03-19 Airbus Espana Sl Aircraft tail assembly
ES2335840A1 (en) * 2007-07-27 2010-04-05 Airbus España, S.L. Aircraft tail assembly

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