초록 ▼

A regenerator assembly for a gas turbine engine has a hot side seal assembly formed in part by a cast metal engine block having a seal recess formed therein that is configured to supportingly receive ceramic support blocks including an inboard face thereon having a regenerator seal face bonded there

A regenerator assembly for a gas turbine engine has a hot side seal assembly formed in part by a cast metal engine block having a seal recess formed therein that is configured to supportingly receive ceramic support blocks including an inboard face thereon having a regenerator seal face bonded thereto. A pressurized leaf seal is interposed between the ceramic support block and the cast metal engine block to bias the seal wear face into sealing engagement with a hot side surface of a rotary regenerator matrix.

대표청구항 ▼

In a gas turbine engine regenerator system of the type including a regenerator disc disposed on a block portion of said engine for rotation about a spindle means and intercepting a pressurized compressor discharge passage and a power turbine exhaust passage, said compressor discharge and turbine exh

In a gas turbine engine regenerator system of the type including a regenerator disc disposed on a block portion of said engine for rotation about a spindle means and intercepting a pressurized compressor discharge passage and a power turbine exhaust passage, said compressor discharge and turbine exhaust passages being separated by an engine block cross arm, and inboard and outboard rim seal means between said disc and said engine block, an improved cross arm seal arrangement comprising, means on said engine block cross arm defining a groove flanked on opposite sides by a pair of flat surfaces, a ceramic seal means having a pair of flanges engaging respective ones of said flat surfaces to support said seal means on said engine block and a base disposed in said groove, said seal means engaging said disc and defining thereat a cross arm seal, leaf spring seal means disposed in said groove between said block cross arm and said ceramic seal means for completing separation between said compressor discharge passage and said turbine exhaust passage at said cross arm, first auxiliary passage means for directing pressurized cold air from a high pressure zone on one side of said disc to said groove through said spindle means thereby to pressure bias said leaf spring seal means into engagement on one of said ceramic seal means and said block cross arm, and second auxiliary passage means for directing said pressurized cold air from said groove to a lower high pressure zone on the other side of said disc thereby to permit flow-through of high pressure cooling air for cooling said spindle means and said leaf spring seal means.