| CPC F01D 25/24 (2013.01) [F01D 11/003 (2013.01); F01D 25/16 (2013.01); F05D 2220/32 (2013.01); F05D 2230/70 (2013.01); F05D 2240/50 (2013.01); F05D 2240/55 (2013.01)] | 20 Claims |

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1. A compression tool for a seal assembly of a gas turbine engine, comprising:
a cover configured to be installed to a seal assembly, the seal assembly including:
a seal carrier;
a seal element installed to the seal carrier, the seal element configured as a ring, and extending in a first axial direction from the seal carrier; and
one or more biasing elements extending from the seal carrier in a second axial direction and configured to axially bias a position of the seal element toward the first axial direction;
the cover including:
a cover body; and
a cover flange including a flange groove configured to cover the seal element of the seal assembly and to urge the seal carrier in the second axial direction.
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