Cooling pipe line for an engine

Details Cooling pipe line for an engine Cooling pipe line for an engine

1988-03-10

1990-06-19

Bryant, III, James E.

Pipes and tubular conduits

Distinct layers

With intermediate insulation layer

138138, 138140, 138143, 138DIG2, 138DIG10, F16L 914

Patent

active

049344129

ABSTRACT:
In a pipe line for an engine, in particular a cooling line in aircraft construction, the walls of the pipe line are composed of a load-bearing inner layer (2) of fibre reinforced, curable synthetic resin and of a heat insulating outer layer (3) of fibre reinforced curable synthetic resin, bonded to the inner layer (2). For the production of the two layers (2, 3) a removable core (1) is used, for example composed of a low melting metal alloy.

REFERENCES:
patent: 3044499 (1962-07-01), Frerich
patent: 3053715 (1962-09-01), Labino
patent: 3554237 (1971-01-01), Pelley et al.
patent: 3614967 (1971-10-01), Royston
patent: 3886024 (1975-05-01), Chase
patent: 3901281 (1975-08-01), Morrisey
patent: 3963547 (1976-06-01), Kaneko et al.
patent: 4208373 (1980-06-01), Matovich
patent: 4310585 (1982-01-01), Shannon
patent: 4442585 (1984-04-01), McGehee et al.
patent: 4516608 (1985-05-01), Titus et al.
patent: 4673002 (1987-06-01), Scanlon et al.

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