A turbine engine comprising a housing in which a rotor (14) is rotatably mounted, the housing is of a split casing construction including a centre casing sandwiched between a pair of outer casings, namely an inlet outer casing and an outlet casing. The rotor (14) is shaped circular in profile and includes three working surfaces generally defined by a peripheral surface (32) and a pair of opposing side surfaces (34, 36) respectively. The peripheral surface (32) of the rotor (14) which acts as a first stage of the turbine engine includes a plurality of circumferentially spaced and generally axially directed ribs in the form of a series of arcuate flutes such as (38). The rotor (14) also includes a plurality of angularly spaced and radially extending rotor blades (40) which in transverse cross-section are aerofoil shaped with at least a portion of the concave or generally flat and convex surfaces of each of the blades (40) defining two further working surfaces of the rotor (14).
申请公布号
WO0223013(A1)
申请公布日期
2002.03.21
申请号
WO2001AU00617
申请日期
2001.05.24
申请人
ECO-TURBO PTY LTD;CHOY, DOMINIC, KIN, LEUNG;DAEVYS, STUART;KHOSHKBIJARY, AMIR, SAID
发明人
CHOY, DOMINIC, KIN, LEUNG;DAEVYS, STUART;KHOSHKBIJARY, AMIR, SAID