发明名称 Aircraft aircrew life support apparatus.
摘要 <p>A breathing demand regulator for use in aircrew life support apparatus has an aneroid capsule 56 coacting with a valve head 50 to restrict outflow from a breathing pressure control chamber 32. The aneroid capsule expands to move the valve head in the event of aircraft cabin altitude rising above a predetermined level due to loss of cabin pressure. An end face 53 of a valve stem 51 supporting the valve head senses inflation pressure of an aircrew G-suit by way of a passageway 59 for movement of the valve head in the presence of G-load. This arrangement provides for increased control pressure and, hence, increased breathing gas pressure in a regulator outlet 13, in meeting the higher of requirements for positive pressure breathing to protect an aircrew member exposed to both G-load and high aircraft ambient altitude (say above 12000 metres). The regulator is disclosed in combination with an anti-G valve arrangement 90, 100 and a G-suit inflation control valve arrangement 60, 61, and 120, 121 that provides the higher of G-suit inflation pressure requirement for protecting the aircrew member when exposed to high aircraft ambient altitude in the presence of G-load. &lt;IMAGE&gt;</p>
申请公布号 EP0448258(A1) 申请公布日期 1991.09.25
申请号 EP19910301937 申请日期 1991.03.08
申请人 NORMALAIR-GARRETT (HOLDINGS) LIMITED 发明人 FOOTE, JAMES CONWAY, 'SANDPIPERS';ROWLAND, PETER JOHN;HARRAL, MICHAEL WILLIAM
分类号 B64D10/00;A62B9/02 主分类号 B64D10/00
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