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Axially-split radial turbines

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-005/04    F01D-005/06    F01D-005/08    F01D-005/14    F01D-005/18    F01D-005/28    F01D-005/30    B23P-015/00   
출원번호 US-0713220 (2015-05-15)
등록번호 US-9726022 (2017-08-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lorenz & Kopf, LLP
인용정보 피인용 횟수 : 0  인용 특허 : 67
초록

Embodiments of an axially-split radial turbine, as are embodiments of a method for manufacturing an axially-split radial turbine. In one embodiment, the method includes the steps of joining a forward bladed ring to a forward disk to produce a forward turbine rotor, fabricating an aft turbine rotor, and disposing the forward turbine rotor and the aft turbine rotor in an axially-abutting, rotationally-fixed relationship to produce the axially-split radial turbine.

대표
청구항
▼

1. An axially-split radial turbine, comprising: a forward turbine rotor, comprising: a forward bladed ring; anda forward disk joined to the forward bladed ring; andan aft turbine rotor;a plurality of hub flow paths extending from the forward turbine rotor to the aft turbine rotor, the plurality of hub low paths each comprising: a leading portion defined, at least in substantial part, by the forward disk; andan intermediate portion defined, at least in substantial part, by the forward bladed ring;wherein the forward turbine rotor and the aft turbine rotor...

이 특허에 인용된 특허 (67)

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