Space saver fitting for ejection seat catapult

Space saver fitting for ejection seat catapult

A fitting for use with an ejection seat system of an aircraft includes a fitting bar configured to extend across a top of a catapult of the ejection seat system and defining an angled slot configured to receive a portion of a gas port of the ejection seat system. The fitting further includes a first...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Cyle Teal, Kassidy L. Carson, Bradley Mastrolia
Format: Patent
Sprache:eng
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:A fitting for use with an ejection seat system of an aircraft includes a fitting bar configured to extend across a top of a catapult of the ejection seat system and defining an angled slot configured to receive a portion of a gas port of the ejection seat system. The fitting further includes a first leg and a second leg coupled to and extending away from the fitting bar and configured to be pivotally coupled to a smokestack structure of the ejection seat system.