Haubenringverriegelungsanordnung
Anmelder: Rohr, Inc. 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4331998
- Aktenzeichen
- EP23194953
- Anmeldetag
- 1. September 2023
- Veröffentlichung
- 10. April 2024
- Rechtsraum
- EP
- IPC
- B64D29/06B64D29/08
Abstract
A nacelle (22) for a gas turbine engine (20) includes a fixed nacelle portion (48), a cowl panel (52), and a latch assembly. The fixed nacelle portion (48) extends circumferentially about an axial centerline. The cowl panel (52) is axially adjacent the fixed nacelle portion (48). The cowl panel (52) is moveable relative to the fixed nacelle portion (48) between an open position and a closed position. The latch assembly includes a first latch portion and a second latch portion. The first latch portion is mounted to the cowl panel (52). The first latch portion includes a pin configured for translation along a pin axis between an extended pin position and a retracted pin position. The second latch portion is mounted to the fixed nacelle portion (48). The second latch portion includes a pin guide. The pin guide is configured to receive and engage the pin with the pin in the extended position and the cowl panel (52) in the closed position.
Anmelder
- Firma
- Rohr, Inc.
- Land
- 🇺🇸 USA
US-amerikanisches Unternehmen, das Triebwerksverkleidungen und weitere Strukturkomponenten für Flugzeugtriebwerke entwickelt und herstellt.
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