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In-Flight Refuelling Probe Selector Valve

In-Flight Refuelling Probe Selector Valve
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In-Flight Refuelling Probe Selector Valve

Product catalog summary
Technical Overview: The document details the specifications of a multi-way hydraulic directional control valve designed by FIMAC S.p.A. for in-flight refuelling applications. The valve features a rip-stop, failure-tolerant aluminum alloy manifold design with four spool and sleeve selectors, electrically actuated by five solenoid pilot valves.
Specifications:
  • Selector for Door Operation: Four ways, two positions, ball retained.
  • Selector for Probe Operation: Four ways, three positions, spring centered.
  • Selector Shut-off: For actuation logic consensus.
  • Dump Valve Selector: For emergency deployment, with separation between two independent hydraulic systems.
  • Operating Temperature: -40°C to +97°C.
  • Operating Fluid: MIL-H-5606.
  • Operating Pressure: 4000 psi (270 bar).
  • Unit Weight: 3.15 kg.
  • Application: Employed on the Eurofighter Typhoon.
Contact Information: FIMAC S.p.A., Via Piemonte, 19, 20030 SENAGO (Milano), Italy. Tel: +39 0299010754, Fax: +39 0299010759, Email: [email protected], Website: www.fimac.aero.
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Catalog excerpts

In-Flight Refuelling Probe Selector Valve-1

Hydraulic & Pneumatic Equipment Multi-way hydraulic directional control valve. Rip-stop, failure tolerant aluminum alloy manifold design, featuring four spool and sleeve selectors. Electrical actuation of the Selectors by means of five Solenoid Pilot Valves. • Selector for the Door operation (four ways, two positions, ball retained). • Selector for the Probe operation (four ways, three positions, spring centered). • Selector Shut-off for the actuation logic consensus. • Dump Valve Selector, for emergency deployment, with separation between two independent hydraulic systems.

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