Invention Grant
- Patent Title: Transition channel between two turbine stages
- Patent Title (中): 两台涡轮级之间的过渡通道
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Application No.: US11868189Application Date: 2007-10-05
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Publication No.: US08011879B2Publication Date: 2011-09-06
- Inventor: Jean-Michel Guimbard , Philippe Jean-Pierre Pabion , Eric Schwartz , Jean-Luc Soupizon
- Applicant: Jean-Michel Guimbard , Philippe Jean-Pierre Pabion , Eric Schwartz , Jean-Luc Soupizon
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0654139 20061006
- Main IPC: F01D5/08
- IPC: F01D5/08

Abstract:
A transition channel between a first turbine section and a second turbine section for a gas turbine engine is disclosed. The channel includes a first radially external annular wall including ring sector elements housed inside an annular ring and orifices for injecting a fluid into the channel in order to re-energize the boundary layer thereof, a second radially internal annular wall, and a fluid supply device arranged between the space outside the ring and the injection orifices.
Public/Granted literature
- US20080085182A1 TRANSITION CHANNEL BETWEEN TWO TURBINE STAGES Public/Granted day:2008-04-10
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