Metal working – Method of mechanical manufacture – Utilizing transitory attached element or associated separate...
Patent
1978-07-05
1980-01-29
Combs, E. M.
Metal working
Method of mechanical manufacture
Utilizing transitory attached element or associated separate...
B64D 3302
Patent
active
041853733
ABSTRACT:
An air inlet duct for a jet propulsion missile or other vehicle which is movable between a housed, pre-launch position and an extended or deployed flight position. A method of manufacturing the duct is also disclosed. The duct system includes a flexible leading edge attached to a double-wall inflatable duct body. Drop threads extend between the duct body walls to hold an exact desired contour when the duct is inflated. A pivotable plate moves the inflatable duct between a housed, deflated, position and an inflated flight position. Manufacture of the inflatable duct is basically accomplished by preparing a foamed plastic form in the desired duct wall shape, covering the form with fabric, stitching through the foam and fabric, coating the fabric with a flexible sealing compound, dissolving away the foamed plastic and attaching the resulting inflatable duct to other missile components.
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Holland Charles L.
Nicoloff George B.
Combs E. M.
Duncan John R.
General Dynamics Corporation
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