Pratt-whitney Canada Corp

Pierre Huppe

Benjamin James Renaud

Richard Robert Kudrna

A fireproof assembly for an aircraft engine, comprises a fireproof housing having an internal volume and an opening. A fireproof internal shield is located within the fireproof housing. The internal shield divides the volume into a first sub-volume and a second sub-volume, the first sub-volume configured for receiving a component of the aircraft engine. A non-fireproof component seals the opening of the fireproof housing. Fireproof fasteners are used to support internal shield inside the housing.

Fireproof assembly

A gasket providing electrical conductivity between components is disclosed. The gasket comprises a body having a fastener hole extending therethrough and an electrically conductive insert lining at least part of the fastener hole in the body. The insert has a first contact face disposed for electrically contacting a first component and a second contact face disposed for electrically contacting a second component. The first contact face is in electrical communication with the second contact face.

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Lemoyne, Canada

Pierre Huppe