STRUCTURAL PANEL WITH INTEGRATED COUPLER

An assembly (58) is provided for an aircraft propulsion system (20). This assembly includes a cowl door (64) movable between a closed position and an open position. The cowl door (64) includes a structural panel (72) and a mount (74). The structural panel (72) includes an inner skin (78), an outer s...

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Bibliographische Detailangaben
Hauptverfasser:	SHANER, Kristopher B, LUNDIN, Joseph R, SOMMER, Thomas
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An assembly (58) is provided for an aircraft propulsion system (20). This assembly includes a cowl door (64) movable between a closed position and an open position. The cowl door (64) includes a structural panel (72) and a mount (74). The structural panel (72) includes an inner skin (78), an outer skin (80) and a cellular core (82,84). The cellular core (82,84) is connected to and arranged between the inner skin (78) and the outer skin (80). The mount (74) includes a base (102) and a coupler (104). The base (102) is connected to and arranged between the inner skin (78) and the outer skin (80). The coupler (104) projects out from the base (102).