TRANSITION SYSTEM SIDE SEAL FOR GAS TURBINE ENGINES

TRANSITION SYSTEM SIDE SEAL FOR GAS TURBINE ENGINES

A gas turbine engine has a transition duct assembly. Between two adjacent transition ducts (20) there is a transition side groove (23) that is formed by transition side rails (22). In this transitionside groove (23) is inserted a side seal (30a-30e) that engages transition side grooves (23) that are...

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Bibliographische Detailangaben
1. Verfasser: SCHIAVO ANTHONY L
Format: Patent
Sprache:chi ; eng
Schlagworte:
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Beschreibung
Zusammenfassung:A gas turbine engine has a transition duct assembly. Between two adjacent transition ducts (20) there is a transition side groove (23) that is formed by transition side rails (22). In this transitionside groove (23) is inserted a side seal (30a-30e) that engages transition side grooves (23) that are formed in the transition side rails (22). 燃气涡轮发动机具有过渡管道组件。在两个相邻的过渡管道（20）之间存在过渡件侧槽（23），该过渡件侧槽（23）由过渡件侧轨（22）形成。在该过渡件侧槽（23）中插入侧密封件（30a-30e），该侧密封件（30a-30e）接合形成在过渡件侧轨（22）中的过渡件侧槽（23）。