A TURBOMACHINE COMPONENT WITH A STRESS RELIEF CAVITY

摘要

A turbomachine component (1) with a stress relief cavity is provided. The turbomachine component contains an airfoil (10) and a platform (20). The airfoil contains a trailing edge (14). The platform contains a trailing edge region, a seal strip slot (40) and a stress relief cavity (30). The trailing edge region supports at least a part of the trailing edge. The stress relief cavity extends inside the platform into the trailing edge region and is an extension of the seal strip slot.