Deckbandsystem mit Zweistufiger Feder und Rückhaltesystem für Gasturbinenmotordeckband
Anmelder: Honeywell International Inc. 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4793466
- Anmeldetag
- 20. Januar 2026
- Veröffentlichung
- 19. August 2026
- Rechtsraum
- EP
- IPC
- F01D11/18, F01D25/24
Abstract
SHROUD SYSTEM WITH TWO-STAGE SPRING AND RETAINER SYSTEM FOR GAS TURBINE ENGINE SHROUD A shroud system (150) for a gas turbine engine. The shroud system includes a support structure (204) defining two stages. One shroud is disposed at one stage and another shroud is disposed at the other stage. A retention and positioning assembly (222) is disposed on the support structure and positions and holds both shrouds relative to the support structure. A load transfer pin (232, 234) is located radially outward from each of the shrouds. A spring (230) is coupled to the support structure and engages both load transfer pins. The spring applies forces on the load transfer pins toward their respective shroud. A retainer is coupled with the support structure and extends over both stages.
Anmelder
- Firma
- Honeywell International Inc.
- Land
- 🇺🇸 USA
US-amerikanischer Mischkonzern mit Schwerpunkten in Luft- und Raumfahrttechnik, Automatisierungslösungen, Gebäudetechnik sowie Spezialchemikalien und -materialien für Industrie- und Verteidigungskunden.
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