초록 ▼

A gas turbine engine inertial inlet particle separator having anti-icing. The separator has inner and outer walls defining a main inlet channel and splitter walls dividing the main channel into inner and outer branches. At least one of the walls has a surface portion subject to icing and a partition

A gas turbine engine inertial inlet particle separator having anti-icing. The separator has inner and outer walls defining a main inlet channel and splitter walls dividing the main channel into inner and outer branches. At least one of the walls has a surface portion subject to icing and a partition on the separator is closely disposed behind the one wall to define therewith a narrow annular tunnel. An inlet passage ducts hot compressed air from the engine to one end of the narrow tunnel and a discharge passage ducts the hot compressed air from the other end of the tunnel to a discharge, the flow area of the tunnel being less than the flow area of at least one of the discarge and inlet passages so that the tunnel defines a high velocity, enhanced heat transfer segment of a heating air channel consisting of the tunnel and the inlet and discharge passages. Heat conducting bridges extend across the tunnel to further enhance heat transfer to the icing surface portion.

대표청구항 ▼

On a gas turbine engine having a source of hot compressed air and an annular compressor entry, an inlet particle separator comprising: an annular inner wall, an annular outer wall around said inner wall and cooperating therewith in defining a main inlet channel having an inlet at one end, a splitter

On a gas turbine engine having a source of hot compressed air and an annular compressor entry, an inlet particle separator comprising: an annular inner wall, an annular outer wall around said inner wall and cooperating therewith in defining a main inlet channel having an inlet at one end, a splitter in said main channel having a first wall facing said annular outer wall and defining therewith an annular outer branch between said main inlet channel and a scroll chamber of said separator and a second wall facing said annular inner wall and defining therewith an annular inner branch between said main inlet channel and said compressor entry and a nose connecting said inner and said outer walls, means defining a surface portion on one of said inner and said outer walls and said first and said second walls generally frontally exposed to an airstream in a corresponding one of said main inlet channel and said inner and said outer branches, a partition on said separator cooperating with said one of said inner and said outer walls and said first and said second walls in defining an annular tunnel behind said surface portion, means defining a heating air inlet passage connecting an upstream end of said annular tunnel to said source of hot compressed air, means defining a heating air discharge passage connecting a downstream end of said annular tunnel to a discharge so that a heating air channel is defined between said inlet and said discharge for flow of hot compressed air from said source, one of said heating air inlet and said heating air discharge passages having a flow area exceeding the flow area of said annular tunnel so that said annular tunnel defines a high velocity segment of said heating air channel and said one of said heating air inlet and said heating air discharge passages defines a low velocity segment of said heating air channel, and means defining a heat conducting bridge across said annular tunnel between said partition and said one of said inner and said outer walls and said first and said second walls.