GB824620A - Control line regulator - Google Patents

Control line regulator

Info

Publication number
GB824620A
GB824620A GB40789/58A GB4078958A GB824620A GB 824620 A GB824620 A GB 824620A GB 40789/58 A GB40789/58 A GB 40789/58A GB 4078958 A GB4078958 A GB 4078958A GB 824620 A GB824620 A GB 824620A
Authority
GB
United Kingdom
Prior art keywords
yoke
bore
disc
jan
end portion
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
GB40789/58A
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.)
PACIFIC SCIENT AEROPRODUCTS
Pacific Scientific Co
Original Assignee
PACIFIC SCIENT AEROPRODUCTS
Pacific Scientific Aeroproducts
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 PACIFIC SCIENT AEROPRODUCTS, Pacific Scientific Aeroproducts filed Critical PACIFIC SCIENT AEROPRODUCTS
Publication of GB824620A publication Critical patent/GB824620A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C1/00—Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
    • F16C1/10—Means for transmitting linear movement in a flexible sheathing, e.g. "Bowden-mechanisms"
    • F16C1/22—Adjusting; Compensating length
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Oral & Maxillofacial Surgery (AREA)
  • Mechanical Engineering (AREA)
  • Flexible Shafts (AREA)
  • Devices For Conveying Motion By Means Of Endless Flexible Members (AREA)

Abstract

824,620. Tensioning wires. PACIFIC SCIENTIFIC AEROPRODUCTS. Jan. 25, 1957 [Jan. 30, 1956], No. 40789/58. Divided out of 821,468. Class 45. [Also in Groups XXX and XXXIII] A tension regulator for a dual control line transmission system e.g. for controlling an aircraft rudder &c., comprises an elongated body 111 having a bore 112 in the cylindrical shaped end portion, the opposite end portion of the body having a serrated bore extending transversely through the body and accommodating a controlled shaft 113 perpendicular to the axis of the body, a yoke 115 slidably mounted over the body with a pin 116 fixedly secured in the yoke extending through a longitudinal slot 117 in the body into the bore 112 to support a sliding collar disc 123 pressed there against by a pair of compression springs 118, 119 positioned between said disc and a fixed disc 121 and lock ring 122 in the upper end of the bore and a canting-type washer 124 inserted between the body 111 and the yoke 115. The springs 118, 119 expand and contract in use causing the yoke 115 to slide along the outer surface of the body 111 to maintain a desired rig loading in the control lines 127, 128, but when a working force is exerted on one of the lines the yoke 115 cants jamming the washer 124 against the body 111 and prevents the yoke sliding on the body, this latter rotating to transmit the control motion to the shaft 113.
GB40789/58A 1956-01-30 1957-01-25 Control line regulator Expired GB824620A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US824620XA 1956-01-30 1956-01-30

Publications (1)

Publication Number Publication Date
GB824620A true GB824620A (en) 1959-12-02

Family

ID=22171373

Family Applications (1)

Application Number Title Priority Date Filing Date
GB40789/58A Expired GB824620A (en) 1956-01-30 1957-01-25 Control line regulator

Country Status (1)

Country Link
GB (1) GB824620A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4584898A (en) * 1981-12-28 1986-04-29 Lockheed Corporation Spring-loaded push-pull cable assembly

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4584898A (en) * 1981-12-28 1986-04-29 Lockheed Corporation Spring-loaded push-pull cable assembly

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