(19)
(11)EP 2 233 808 A3

(12)EUROPEAN PATENT APPLICATION

(88)Date of publication A3:
06.12.2017 Bulletin 2017/49

(43)Date of publication A2:
29.09.2010 Bulletin 2010/39

(21)Application number: 10157727.8

(22)Date of filing:  25.03.2010
(51)International Patent Classification (IPC): 
F16K 31/122(2006.01)
F15B 13/02(2006.01)
B64C 13/42(2006.01)
(84)Designated Contracting States:
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR
Designated Extension States:
AL BA ME RS

(30)Priority: 26.03.2009 JP 2009076471

(71)Applicant: Nabtesco Corporation
Tokyo 105-0022 (JP)

(72)Inventors:
  • Yoshioka, Teruhiko
    Fuwa-gun, Gifu 503-2124 (JP)
  • Niwa, Hideki
    Fuwa-gun, Gifu 503-2124 (JP)

(74)Representative: Intès, Didier Gérard André et al
Cabinet Beau de Loménie 158 rue de l'Université
75340 Paris Cedex 07
75340 Paris Cedex 07 (FR)

  


(54)Multifunction relief valve and airplane emergency hydraulic power source unit having the same


(57) A multifunction relief valve 1 includes: a relief chamber 2 having an introduction port 7 and a relief port 8 for introducing and relieving pressure fluid; a back pressure chamber 3 formed on one end side of the relief chamber 2; a piston 4 which is movably provided in the back pressure chamber 3 and divides the back pressure chamber 3 into a first back pressure chamber 3a and a second back pressure chamber 3b; a first spring 5 which is provided in the first back pressure chamber 3a and exerts a biasing force in a direction in which the relief port 8 is closed; a second spring 6 which is provided in the second back pressure chamber 3b and biases the piston 4 in the direction in which the relief port 8 is closed; and a pilot pressure supply port 9 formed in the first back pressure chamber 3a. The pressure fluid introduced into the first back pressure chamber 3a via the pilot pressure supply port 9 changes the relief pressure.







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