Patent ID: 11859506
Assignee: PRATT & WHITNEY CANADA CORP.
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  B | IPC B  F

Claim 19:
20. A structure for a gas turbine engine, comprising:
an engine case including a base, a mounting boss, a first support element and a second support element axially spaced from the first support element by a gap;
the base extending axially along and circumferentially about an axial centerline;
the mounting boss projecting radially out from the base, the mounting boss extending axially between a first side surface and a second side surface, and the mounting boss extending laterally to a lateral side surface;
the first support element comprising a peripheral boss, the peripheral boss projecting radially out from the base, laterally out from the mounting boss and axially to the first side surface; and
the second support element comprising a rib, the rib projecting radially out from the base, laterally out from the mounting boss and axially to the second side surface;
wherein the lateral side surface projects radially out from the base, and wherein the lateral side surface extends axially from the first support element to the second support element.