Quick install insulation

Details Quick install insulation Quick install insulation

2005-05-03

2005-05-03

Swiatek, Robert P. (Department: 3643)

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

C052S506050, C052S404400

Reexamination Certificate

active

06886783

ABSTRACT:
A method for quick insulating the interior skin of an airplane. The system includes a new design for the insulating blanket with permeable and impermeable membranes and a blanket “clip” allowing for cable pass-through. The method stabilizes blanket construction method, minimizes moisture retention and promotes a design based provisioning strategy to accommodate system run access to the airplane skin through a simplified interface detail. Both the insulation blanket and the blanket clip attach to the aircraft frame via a “zip-lock” attachment system, which consists of vertical rails with receiving detail to receive the (blanket and clip) zip-lock strips, and a cap strip that covers (and secures) the zip-lock strips. The invention solves the moisture retention and installation time and the quantity of Mylar® used to encapsulate the fiberglass material.

REFERENCES:
patent: 3029910 (1962-04-01), Kirk et al.
patent: 5139839 (1992-08-01), Lim
patent: 5715638 (1998-02-01), Anderson, Sr.
patent: 6068907 (2000-05-01), Beauregard
patent: 6358591 (2002-03-01), Smith

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