GB390432A - Improvements in or relating to aircraft - Google Patents

Improvements in or relating to aircraft

Info

Publication number
GB390432A
GB390432A GB27559/32A GB2755932A GB390432A GB 390432 A GB390432 A GB 390432A GB 27559/32 A GB27559/32 A GB 27559/32A GB 2755932 A GB2755932 A GB 2755932A GB 390432 A GB390432 A GB 390432A
Authority
GB
United Kingdom
Prior art keywords
elevator
hinged
aircraft
tail plane
auxiliary
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
GB27559/32A
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.)
CHARLES VINCENT LEO FOLEY
Original Assignee
CHARLES VINCENT LEO FOLEY
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 CHARLES VINCENT LEO FOLEY filed Critical CHARLES VINCENT LEO FOLEY
Priority to GB27559/32A priority Critical patent/GB390432A/en
Publication of GB390432A publication Critical patent/GB390432A/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

390,432. Controlling aircraft. FOLEY, C. V. L., Oakfield, Sligo, Irish Free State. Oct. 4, 1932, No. 27559. [Class 4.] Aircraft are provided with an auxiliary elevator for use in emergency and/or as a tailtrimming device which auxiliary elevator is mounted immediately in front of the normal elevator of the craft in a cut-away portion of the fixed tail plane to which the latter is also hinged. As shown, the auxiliary elevator 1 is hinged to a spar 11 of the tail plane 4 and the elevator 2 is hinged to a spar 2b disposed at the trailing edge of the tail plane and bounding a space 3 in which rocks the elevator 1. Elevator 1 is independently operated by hand or foot control provided with means for locking it in any adjusted position.
GB27559/32A 1932-10-04 1932-10-04 Improvements in or relating to aircraft Expired GB390432A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB27559/32A GB390432A (en) 1932-10-04 1932-10-04 Improvements in or relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB27559/32A GB390432A (en) 1932-10-04 1932-10-04 Improvements in or relating to aircraft

Publications (1)

Publication Number Publication Date
GB390432A true GB390432A (en) 1933-04-06

Family

ID=10261580

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27559/32A Expired GB390432A (en) 1932-10-04 1932-10-04 Improvements in or relating to aircraft

Country Status (1)

Country Link
GB (1) GB390432A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2439304A (en) * 1943-02-01 1948-04-06 William H Jackson Aeroplane empennage
US3041014A (en) * 1957-05-13 1962-06-26 Gerin Jacques Jean-Marie Jules High lift, highly extensible device for aircraft wings

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2439304A (en) * 1943-02-01 1948-04-06 William H Jackson Aeroplane empennage
US3041014A (en) * 1957-05-13 1962-06-26 Gerin Jacques Jean-Marie Jules High lift, highly extensible device for aircraft wings

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