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

Claim 0:
1. A structure for a gas turbine engine, comprising:
an engine case including a base, a mounting boss and a first support element, the base extending axially along and circumferentially about an axial centerline of the engine case, the mounting boss projecting radially out from the base, the first support element projecting radially out from the base and laterally out from the mounting boss, and the first support element comprising a peripheral boss;
an engine pylon mounted to the mounting boss by a plurality of bolts, each of the bolts projecting radially through a mount of the engine pylon and into a respective bolt aperture in the mounting boss; and
an engine line coupled to the peripheral boss.