초록 ▼

An aircraft anti-icing system includes a source of high temperature gas, a housing, at least one conduit to carry the high temperature gas from the source to the housing, the at least one conduit coupled to the housing and the source, at least one nozzle coupled to the at least one conduit, at least

An aircraft anti-icing system includes a source of high temperature gas, a housing, at least one conduit to carry the high temperature gas from the source to the housing, the at least one conduit coupled to the housing and the source, at least one nozzle coupled to the at least one conduit, at least one nozzle configured to impart a rotational motion to the high temperature gas before exhausting the high temperature gas into the housing, and a port for exhausting air from the housing.

대표청구항 ▼

What is claimed is: 1. An aircraft anti-icing system comprising:a source of high temperature gas;a housing;at least one conduit configured to carry the high temperature gas from the source to the housing;at least one nozzle coupled to said at least one conduit, said at least one nozzle configured to

What is claimed is: 1. An aircraft anti-icing system comprising:a source of high temperature gas;a housing;at least one conduit configured to carry the high temperature gas from the source to the housing;at least one nozzle coupled to said at least one conduit, said at least one nozzle configured to impart a rotational motion to the high temperature gas before exhausting the high temperature gas into the housing; anda port for exhausting air from the housing;wherein said at least one nozzle comprises a longitudinal axis and a plurality of tubes wrapped around the longitudinal axis of the at least one nozzle to form a helix; andwherein the housing comprises one of a nose cowl and a wing.