|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 10|
Gas turbine engine systems involving hydrostatic face seals are provided. In this regard, representative compressor assembly for a gas turbine engine includes a compressor having a hydrostatic seal formed by a seal face and a seal runner.
The invention claimed is: 1. A hydrostatic seal assembly for a compressor of a gas turbine engine comprising: a carrier having orifices that extend therethrough to supply a high-pressure airflow along a metal seal face; a mounting bracket that positions the seal face within the gas turbine engine so as to maintain a pressure differential within the gas turbine engine during operation of the engine; a compressor component disposed at an outer diameter of the compressor and having a metal seal runner integral thereto, the seal runner interfacing with the ...