US Patent 10233763 Seal assembly for turbine engine component

A seal assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a housing, a seal carrier secured to the housing and configured to be selectively biased from the housing, and a wedge seal secured to the seal carrier and configured to abut against at least two sealing surfaces. A method of sealing between adjacent components of a gas turbine engine is also disclosed.