초록 ▼

Thrust reverser inner wall structure comprising a thermally conductive nonmetallic carbon pitch fiber honeycomb core sandwiched between a top and bottom layer. The core is adhered by a reticulated layer of adhesive to a perforated carbon fiber top layer, and adhered to a base layer of nonmetallic, n

Thrust reverser inner wall structure comprising a thermally conductive nonmetallic carbon pitch fiber honeycomb core sandwiched between a top and bottom layer. The core is adhered by a reticulated layer of adhesive to a perforated carbon fiber top layer, and adhered to a base layer of nonmetallic, nonperforated carbon fiber reinforced fabric.

대표청구항 ▼

1. In an aircraft power plant, a method for conducting heat through a thrust reverser inner wall made from a honeycomb core sandwich panel, comprising the steps of:(a) conducting heat from a carbon-fiber reinforced resin composite face sheet of the inner wall to a carbon fiber honeycomb core, the co

1. In an aircraft power plant, a method for conducting heat through a thrust reverser inner wall made from a honeycomb core sandwich panel, comprising the steps of:(a) conducting heat from a carbon-fiber reinforced resin composite face sheet of the inner wall to a carbon fiber honeycomb core, the core having oriented carbon pitch fibers and a thermal conductivity of about 1.09-2.05W/m-.degree.K; and (b) conducting heat from the core to a perforated, fiber reinforced resin composite face sheet in contact with fan airflow for the aircraft power plant.