Fire resistant bearing compartment cover
AssigneeUnited Technologies Corporation
InventorsMartin J. Walsh, Karl J. Yaeger
Life of this patent
Estimating the term…
Abstract
A fire resistant bearing compartment cover (86) for a gas turbine engine features a fluid tight outer wall (106) comprised of an axially extending, radially converging support shell (90) and an axially extending piston ring carrier (92) joined to the support shell by a circumferentially continuous fluid tight joint (104). A heatshield (110) joined to the inner end of the support shell by another circumferentially continuous fluid tight joint (118) and slidably engaging the outer end of the support shell at an expansion joint (128) defines a stagnant air cavity (112). The arrangement reduces the likelihood that any oil leaking out of the bearing compartment will accumulate and be ignited by turbine cooling air (45) which leaks into the cavity.
Claims6
A fire resistant bearing cover for enclosing at least a portion of a bearing compartment in a gas turbine engine, including
- an axially extending support shell having a radially diverging outer end and a radially converging inner end,
- a seal carrier positioned radially inward of the support shell, the seal carrier having an inner face and an outer face, the bearing cover characterized by:
- a fluid tight interface joining the support shell and the seal carrier so that the support shell and seal carrier define a fluid tight outer wall;
- and
- a heatshield joined to the seal carrier by a fluid tight joint, the heatshield also being joined to the outer end of the support shell by an expansion joint to accommodate differential thermal response between the outer wall and the heatshield, the outer wall and the heatshield defining a stagnant insulating air cavity for thermally shielding the bearing compartment from the surrounding local environment.
Dependencies are inferred from the claim text.