Aeroplane equipped with an internal escape hatch incorporating a pressure regulating system
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United States of America Patent
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Jan 10, 2017
Grant Date -
Dec 31, 2015
app pub date -
Jun 25, 2015
filing date -
Jun 27, 2014
priority date (Note) -
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status (Latency Note)
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Abstract
An aeroplane includes an external skin and an internal bulkhead delimiting a cabin, and an escape opening passing through the external skin and the internal bulkhead. The escape opening is closed off by an external escape hatch disposed flush with the external skin. The aeroplane also includes an internal escape hatch that closes off the escape opening disposed flush with the internal bulkhead, and pressure regulating means capable of automatically triggering an opening of the internal escape hatch or a part of the internal escape hatch when a pressure differential on both sides of the internal escape hatch exceeds a determined value.
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