Connecting gas turbine engine annular members

A gas turbine engine assembly comprising:

• a rear turbine frame;
• a centerbody including a different material than the rear turbine frame;
• the centerbody connected to the rear turbine frame with a dual arm V bracket;
• the dual arm V bracket including a first arm and a second arm;
• the first arm and the second arm extending axially away from a bracket base;
• the bracket base attached to the rear turbine frame;
• and
• the first arm and the second arm attached to the centerbody.

An apparatus comprising:

• first annular member means;
• second annular member means of a different material than the first annular member means;
• the second annular member means connected to the first annular member means with dual arm V bracket means;
• the dual arm V bracket means including first arm means and second arm means;
• the first arm means and the second arm means extending axially away from bracket base means;
• the bracket base means attached to the first annular member means;
• and
• the first arm means and the second arm means attached to the second annular member means.