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GB536018A - Improvements in and relating to hydraulic power transmission systems - Google Patents

Improvements in and relating to hydraulic power transmission systems

Info

Publication number
GB536018A
GB536018A GB2689139A GB2689139A GB536018A GB 536018 A GB536018 A GB 536018A GB 2689139 A GB2689139 A GB 2689139A GB 2689139 A GB2689139 A GB 2689139A GB 536018 A GB536018 A GB 536018A
Authority
GB
United Kingdom
Prior art keywords
power transmission
hydraulic power
relating
valve
transmission systems
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
GB2689139A
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 GB2689139A priority Critical patent/GB536018A/en
Publication of GB536018A publication Critical patent/GB536018A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18—Operating mechanisms
    • B64C25/22—Operating mechanisms fluid

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

536,018. Hydraulic power transmission. NASH, A. G. FRAZER-. Sept. 29, 1939, No. 26891. [Class 69 (ii)] In a hydraulic power transmission system such as is used to actuate turrets, gun mountings &c. on aircraft and other vehicles, one relief valve 10 is arranged near the supply pump 1 between the supply line 2 and return line 3, and a second relief valve 9 is arranged near the control valve 4 of the turret 7, the valve 9 being arranged to open at a lower pressure than the valve 10.
GB2689139A 1939-09-29 1939-09-29 Improvements in and relating to hydraulic power transmission systems Expired GB536018A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2689139A GB536018A (en) 1939-09-29 1939-09-29 Improvements in and relating to hydraulic power transmission systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2689139A GB536018A (en) 1939-09-29 1939-09-29 Improvements in and relating to hydraulic power transmission systems

Publications (1)

Publication Number Publication Date
GB536018A true GB536018A (en) 1941-04-30

Family

ID=10250815

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2689139A Expired GB536018A (en) 1939-09-29 1939-09-29 Improvements in and relating to hydraulic power transmission systems

Country Status (1)

Country Link
GB (1) GB536018A (en)

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