| (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 |
| (22) |
Date of filing: 14.02.1990 |
|
|
| (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) |
|
| |
|
| (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.