GB622971A - Aircraft control cable - Google Patents

Aircraft control cable

Info

Publication number
GB622971A
GB622971A GB2755/47A GB275547A GB622971A GB 622971 A GB622971 A GB 622971A GB 2755/47 A GB2755/47 A GB 2755/47A GB 275547 A GB275547 A GB 275547A GB 622971 A GB622971 A GB 622971A
Authority
GB
United Kingdom
Prior art keywords
per cent
control cable
aircraft control
max
manganese
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
GB2755/47A
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.)
American Steel and Wire Company of New Jersey
Original Assignee
American Steel and Wire Company of New Jersey
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 American Steel and Wire Company of New Jersey filed Critical American Steel and Wire Company of New Jersey
Publication of GB622971A publication Critical patent/GB622971A/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
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms

Abstract

An aircraft control cable having substantially the following composition: carbon 0.50-0.60 per cent; manganese 4.50-5.50 per cent; phosphorus 0.030 max; sulphur 0.030 max; silicon 0.500 max; nickel 11.00-13.00; chromium 3.00-4.00; iron balance is employed with an aircraft structure having substantially the following composition: copper 4.4 per cent; magnesium 1.5 per cent; manganese 0.06 per cent; aluminium balance.
GB2755/47A 1946-09-06 1947-01-29 Aircraft control cable Expired GB622971A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US622971XA 1946-09-06 1946-09-06

Publications (1)

Publication Number Publication Date
GB622971A true GB622971A (en) 1949-05-10

Family

ID=22041559

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2755/47A Expired GB622971A (en) 1946-09-06 1947-01-29 Aircraft control cable

Country Status (1)

Country Link
GB (1) GB622971A (en)

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