GB875291A - Improvements in the control of aircraft - Google Patents

Improvements in the control of aircraft

Info

Publication number
GB875291A
GB875291A GB31875/58A GB3187558A GB875291A GB 875291 A GB875291 A GB 875291A GB 31875/58 A GB31875/58 A GB 31875/58A GB 3187558 A GB3187558 A GB 3187558A GB 875291 A GB875291 A GB 875291A
Authority
GB
United Kingdom
Prior art keywords
attached
aircraft
cables
rods
rod
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
GB31875/58A
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 GB31875/58A priority Critical patent/GB875291A/en
Publication of GB875291A publication Critical patent/GB875291A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)

Abstract

875,291. Controlling aircraft. EVANS, D. J. Sept. 22, 1959 [Oct. 6, 1958], No. 31875/58. Class 4. An aircraft comprises a rudder 16 on a vertical shaft 18 having an integral transverse lever 20, the ends of which are attached to rods, cables, or the like 36, 38 also attached to transversely pivoted levers 30 (one shown in Fig. 4) each working in an aperture 22 in the cockpit floor and coupled by pin and slot means 66, 68 to a rod 56 terminating in a pedal 60. Each rod is: attached to a piston 70 in a double acting centering spring box 48. The two rods or cables 36, 38 need not be crossed.
GB31875/58A 1958-10-06 1958-10-06 Improvements in the control of aircraft Expired GB875291A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB31875/58A GB875291A (en) 1958-10-06 1958-10-06 Improvements in the control of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB31875/58A GB875291A (en) 1958-10-06 1958-10-06 Improvements in the control of aircraft

Publications (1)

Publication Number Publication Date
GB875291A true GB875291A (en) 1961-08-16

Family

ID=10329703

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31875/58A Expired GB875291A (en) 1958-10-06 1958-10-06 Improvements in the control of aircraft

Country Status (1)

Country Link
GB (1) GB875291A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1048563A3 (en) * 1999-04-30 2001-04-11 Lord Corporation Self-centering bearing for aircraft control surfaces
WO2003064884A1 (en) 2002-01-28 2003-08-07 Barnes Group Inc. Compression spring rod

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1048563A3 (en) * 1999-04-30 2001-04-11 Lord Corporation Self-centering bearing for aircraft control surfaces
WO2003064884A1 (en) 2002-01-28 2003-08-07 Barnes Group Inc. Compression spring rod
EP1470345A1 (en) * 2002-01-28 2004-10-27 Barnes Group Inc. Compression spring rod
EP1470345A4 (en) * 2002-01-28 2007-03-14 Barnes Group Inc Compression spring rod
US7467787B2 (en) 2002-01-28 2008-12-23 Barnes Group Inc. Compression spring rod

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