Window cooling for high speed flight

Details Window cooling for high speed flight Window cooling for high speed flight

1990-04-27

1991-05-14

Barefoot, Galen

Aeronautics and astronautics

Aircraft structure

2441293, 244 1R, 350319, 350584, 165 44, 165169, B64C 138

Patent

active

050149326

ABSTRACT:
A buffering portion of boundary layer flow along a flight vehicle surface diverted into an internal cavity at a downstream edge of a surface mounted window isolating recirculating flow of the diverted fluid through the cavity while it is cooled therewithin. Outflow of the cooled buffering fluid from at an upstream edge of the window is conducted into the buffering portion of the boundary layer flow to cool the window and prevent damage thereof by aerodynamically generated heating of the surface under high velocity flight conditions.

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patent: 4172428 (1979-10-01), Pariset
patent: 4703904 (1987-11-01), Haslund
patent: 4858850 (1989-08-01), McNay
patent: 4863118 (1989-09-01), Stallings et al.
patent: 4896247 (1990-01-01), Cozel

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