GB539028A - Improvements in hydraulic systems for aircraft - Google Patents

Improvements in hydraulic systems for aircraft

Info

Publication number
GB539028A
GB539028A GB318340A GB318340A GB539028A GB 539028 A GB539028 A GB 539028A GB 318340 A GB318340 A GB 318340A GB 318340 A GB318340 A GB 318340A GB 539028 A GB539028 A GB 539028A
Authority
GB
United Kingdom
Prior art keywords
aircraft
hydraulic systems
reservoir
pump
pipe
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
GB318340A
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.)
AIRCRAFT HYDRAULIC APPLIANCES
Original Assignee
AIRCRAFT HYDRAULIC APPLIANCES
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 AIRCRAFT HYDRAULIC APPLIANCES filed Critical AIRCRAFT HYDRAULIC APPLIANCES
Priority to GB318340A priority Critical patent/GB539028A/en
Publication of GB539028A publication Critical patent/GB539028A/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)
  • External Artificial Organs (AREA)

Abstract

539,028. Pump reservoirs and air vessels. AIRCRAFT HYDRAULIC APPLIANCES, Ltd., and WYLIE, H. N. Feb. 20, 1940, No. 3183. [Class 102 (i)] In aircraft hydraulic systems, a sealed air vessel maintains pressure in a liquid reservoir which supplies a pump through a pipe. The pipe connection between the air vessel and the reservoir may be bent to form a trap ; the pump suction pipe may draw from near the centre of the reservoir.
GB318340A 1940-02-20 1940-02-20 Improvements in hydraulic systems for aircraft Expired GB539028A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB318340A GB539028A (en) 1940-02-20 1940-02-20 Improvements in hydraulic systems for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB318340A GB539028A (en) 1940-02-20 1940-02-20 Improvements in hydraulic systems for aircraft

Publications (1)

Publication Number Publication Date
GB539028A true GB539028A (en) 1941-08-26

Family

ID=9753492

Family Applications (1)

Application Number Title Priority Date Filing Date
GB318340A Expired GB539028A (en) 1940-02-20 1940-02-20 Improvements in hydraulic systems for aircraft

Country Status (1)

Country Link
GB (1) GB539028A (en)

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