Seal support assembly for turbine engine

A turbine engine is provided. The gas turbine engine defines a radial direction and includes: a rotor; the stator comprises a carrier; the sealing assembly is arranged between the rotor and the stator, the sealing assembly comprises a plurality of sealing sections, the plurality of sealing sections...

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Bibliographische Detailangaben
Hauptverfasser:	PATIL, PRADEESH, GANIGER RAVINDRA SHANKAR, JALAN, PRATIK, PORTHUN GRANT ROBERT, HARDIKAR NARENDRA ANAND, KANDUKURI, CHANDRASEKHAR, METRI, MARIKAGUN, YAMAS, DAVID, RAJU, GANGI NAGESWAR RAO, BIDKAR RAHUL ANIL, JOHNSON STEVEN DOUGLAS, GEORGI AJIT
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS 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 turbine engine is provided. The gas turbine engine defines a radial direction and includes: a rotor; the stator comprises a carrier; the sealing assembly is arranged between the rotor and the stator, the sealing assembly comprises a plurality of sealing sections, the plurality of sealing sections are provided with sealing sections, the sealing sections are provided with sealing surfaces, and the sealing surfaces and the rotor form a fluid bearing; and a seal support assembly including a pneumatic engagement assembly operable to bias the seal section in a radial direction during operation of the turbine engine. 提供了一种涡轮发动机。该燃气涡轮发动机限定径向方向，并且包括：转子；定子，定子包括载体；密封组件，密封组件设置在转子和定子之间，密封组件包括多个密封段，多个密封段具有密封段，密封段具有密封面，密封面被构造成与转子形成流体轴承；和密封支撑组件，密封支撑组件包括气动接合组件，气动接合组件能够操作，以在涡轮发动机的操作期间，使密封段沿径向方向偏置。