Turbine engine tie rod systems
AssigneeRaytheon Technologies Corporation
InventorsNicholas W. Kantany, David T. Feindel, Nico M. Rappoli
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AssigneeRaytheon Technologies Corporation
InventorsNicholas W. Kantany, David T. Feindel, Nico M. Rappoli
Estimating the term…
A gas turbine engine turbine section has tie rod assemblies interconnecting an inner diameter structure and an outer casing. Each tie rod has: an inner diameter end; an outer diameter end; and an eyelet of an outer diameter spherical bearing formed at the outer diameter end. A first clevis carries a spherical ball of the bearing, a shank of said clevis extending to an outer diameter (OD) end. A tensioning bolt is mated to a threaded opening in said clevis OD end whereby tightening said bolt applies a tension to said rod. A radial span between a center of the outer diameter spherical bearing and an inner diameter surface of the outer casing is at least 50% greater than that between an outer diameter (OD) surface of the outer ring and the center.
A gas turbine engine turbine section comprising:
A gas turbine engine turbine section comprising:
A gas turbine engine turbine section comprising:
Dependencies are inferred from the claim text.