(19)
(11) EP 0 383 573 A3

(12) EUROPEAN PATENT APPLICATION

(88) Date of publication A3:
08.07.1992 Bulletin 1992/28

(43) Date of publication A2:
22.08.1990 Bulletin 1990/34

(21) Application number: 90301568.3

(22) Date of filing: 14.02.1990
(51) International Patent Classification (IPC)5A62B 7/14, A62B 9/02
(84) Designated Contracting States:
DE ES FR GB IT

(30) Priority: 15.02.1989 GB 8903433

(71) Applicant: NORMALAIR-GARRETT (HOLDINGS) LIMITED
Yeovil Somerset, BA20 2YB (GB)

(72) Inventors:
  • Tucker, Paul Ashton
    Yeovil, Somerset BA20 2PB (GB)
  • Marsh, Roger Malcolm
    Sherborne, Dorset (GB)

(74) Representative: Jack, Bruce James et al
FORRESTER & BOEHMERT Franz-Joseph-Strasse 38
D-80801 München
D-80801 München (DE)


(56) References cited: : 
   
       


    (54) Aircraft aircrew auxiliary oxygen bottle


    (57) An auxiliary oxygen bottle (11) for an aircraft aircrew breathing system is provided with an operating head (12) having a selector valve (51) for connecting either an oxygen enriched breathable gas inlet passage (54) or an auxiliary oxygen inlet passage (15) to an outlet passage (55) which is adapted for connection to an aircrew breathing demand regulator. A lever assembly (70) is automatically actuated following aircraft cabin decompression for control of a servo-pressure controlled diaphragm valve (40) to effect movement of the selector valve (51) to a position in which auxiliary oxygen is delivered to the outlet passage (55). The lever assembly (70) may be manually operated by an aircrew member for selection of auxiliary oxygen or oxygen-enriched breathable gas but re-selection of oxygen-enriched breathable gas is inhibited following cabin decompression if the aircraft is operating above a predetermined altitude.





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