Split vane flow blocker
View Patent ↗A gas path flow blocker comprising a plurality of vanes each comprising a forward portion and an aft portion defining a plurality of gas paths, a forward ring comprising a central axis about which is circumferentially disposed the plurality of forward portions, and an aft ring disposed about the central axis about which is circumferentially disposed the plurality of aft portions wherein the forward ring and the aft ring are moveable with respect to each other to at least partially block the flow of a gas through the gas paths.
1. A gas path flow blocker assembly for use in a gas turbine engine having a gas flowpath between an outer duct and an inner support structure comprising:
a plurality of vanes located in said gas flowpath between said outer duct and said inner support structure of said gas turbine engine, each of said vanes having an airfoil shape and comprising a forward portion and an aft portion defining a plurality of gas paths;
said flowpath being a secondary flowpath;
a forward ring comprising a central axis about which is circumferentially disposed said plurality of forward portions; and
an aft ring disposed about said central axis about which is circumferentially disposed said plurality of aft portions, wherein said forward ring and said aft ring are moveable with respect to each other to at least partially block the flow of a gas through said gas paths.
2. The flow blocker assembly of claim 1 , wherein each of said plurality of forward portions has a trailing edge of a width w and each of said aft portions has a leading edge of said width w.
3. The flow blocker assembly of claim 2 , wherein each of said plurality of vanes is separated from each adjoining one of said plurality of vanes by a width d.
4. The flow blocker assembly of claim 3 , wherein said width d is approximately equal to said width w.
5. The flow blocker assembly of claim 1 , wherein said forward ring is rotatable about said central axis.
6. The flow blocker assembly of claim 2 , wherein said forward ring may be positioned such that each of said plurality of trailing edges is aligned with one of said plurality of leading edges.
7. The flow blocker assembly of claim 2 , wherein each of said plurality of trailing edges and each of said plurality of leading edges are aligned normal to said central axis.
8. A method of controlling gas flow through a secondary gas flowpath of a gas turbine engine located between an outer duct and an inner support structure of said gas turbine engine comprising the steps of:
providing a plurality of vanes positioned in said secondary gas flowpath between said outer duct and said inner support structure, each of said vanes having an airfoil shape and comprising a forward portion and an aft portion defining a plurality of gas paths;
providing a forward ring comprising a central axis about which is circumferentially disposed said plurality of forward portions;
providing an aft ring disposed about said central axis about which is circumferentially disposed said plurality of aft portions; and
rotating at least one of said rings about said central axis to at least partially block the flow of a gas through said gas paths.
9. The method of claim 8 wherein said rotating said at least one ring comprises rotating said forward ring such that each of said plurality of forward portions is aligned with one of said plurality of aft portions to form an airfoil.
10. The method of claim 8 wherein said rotating said at least one ring comprises rotating said forward ring such that each of said plurality of forward portions is not in alignment with any one of said plurality of aft portions.
11. The method of claim 8 wherein said providing said plurality of vanes comprises the steps of:
providing a plurality of forward portions each having a trailing edge of a width w;
providing a plurality of aft portions each having a leading edge of said width w;
separating each of said plurality of vanes from each adjoining one of said plurality of vanes by a width d whereby said width w is approximately equal to said width d.