Bolted joint for rotor disks and method of reducing thermal gradients therein
AssigneeGeneral Electric Company
InventorsJason Francis Pepi, Brian Edward Dix, Tyler Frederick Hooper
Life of this patent
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AssigneeGeneral Electric Company
InventorsJason Francis Pepi, Brian Edward Dix, Tyler Frederick Hooper
Estimating the term…
Bolt hole stress in rotor disks having bolted joints is reduced by passing relatively hot secondary flow path air (such as compressor discharge air) through each bolt hole to heat the disk from inside the bolt hole. In doing so, the temperature distribution in the area of the bolt hole is made more uniform and the stress is dramatically reduced. The bolted joint includes a bolt hole formed in a first rotor disk and a bolt disposed in the bolt hole such that a channel is defined between the bolt and the bolt hole. A first nut or abutment is attached to a first end of the bolt, and a second nut or abutment is attached to a second end of the bolt. A first passage associated with the first abutment provides fluid communication with the channel, and a second passage associated with the second abutment provides fluid communication with the channel, thereby allowing the relatively hot fluid to pass through the channel during engine operation.
A bolted joint for connecting first and second components, said bolted joint comprising:
In a gas turbine engine comprising a first rotor disk, a second rotor disk, a first cavity adjacent to said first rotor disk, and a second cavity adjacent to said second rotor disk, a bolted joint for connecting said first and second rotor disks, said bolted joint comprising:
In a gas turbine engine having a bolted joint for connecting a first rotor disk and a second rotor disk wherein said bolted joint includes a bolt disposed in a bolt hole formed in said first rotor disk, a method of reducing thermal gradients in said first rotor disk comprising:
Dependencies are inferred from the claim text.