Finishing process for fabric covered air frame structure

Details Finishing process for fabric covered air frame structure Finishing process for fabric covered air frame structure

1973-10-25

1976-05-11

Husack, Ralph

Coating processes

With stretching or tensioning

244126, 244133, 427381, 427382, 427412, B05D 138, B64C 100

Patent

active

039565297

ABSTRACT:
A method of finishing cloth-covered aircraft wings and fuselage. The cloth, cotton or polyester cloth of the type made from monofilaments of the condensation product of ethylene glycol with terephthalic acid or dimethyl phthalate is, after application thereof onto the airframe, coated with a layer of latex and dried, then coated with a second, or intermediate, layer of different coating and dried, and then coated with a decorative coating material. The use of latex as a first coat on the cloth results in substantial savings in labor and time and results in a coated fabric of superior flexibility integrity and durability.

REFERENCES:
patent: 2167414 (1939-07-01), Billing
patent: 2336266 (1943-12-01), Lester
patent: 2356927 (1944-08-01), Grossman
patent: 2431745 (1947-12-01), Flanagan
patent: 2517852 (1950-08-01), Dreyling et al.
patent: 3067484 (1962-12-01), Rasero et al.
patent: 3140846 (1964-07-01), Lott
patent: R18355 (1932-02-01), Carson

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