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.
A deployable air inlet duct having a scoop shape with an inlet opening for receiving air and an outlet opening for directing air to a jet engine, which comprises: a surface closure plate movable between a housed position within a vehicle skin surface and a deployed position substantially flush with said skin surface; an inner duct plate secured to the outer side of said surface closure plate and substantially parallel thereto; means for moving said surface closure plate from said housed position to said deployed position; an outer duct wall comprising two spaced sheets of flexible material; a plurality of drop threads extending between said spaced sheets; a flexible leading edge partially surrounding the inlet opening and secured to said outer duct wall and said inner duct plate; and means to admit gas under pressure between said sheets whereby said outer duct wall is inflated and a rigid duct between said inlet and outlet openings is formed.
Claim 2
Dependent Claim
157 words
A deployable air inlet duct having a scoop shape with an inlet opening for receiving air and an outlet opening for directing air to a jet engine, which comprises: a surface closure plate movable between a housed position within a vehicle skin surface and a deployed position substantially flush with said skin surface; an inner duct plate secured to the outer side of said surface closure plate and substantially parallel thereto; means for moving said surface closure plate from said housed position to said deployed position; an outer duct wall comprising two spaced sheets of flexible material; a plurality of drop threads extending between said spaced sheets; a flexible leading edge partially surrounding the inlet opening and secured to said outer duct wall and said inner duct plate; and means to admit gas under pressure between said sheets whereby said outer duct wall is inflated and a rigid duct between said inlet and outlet openings is formed.
Claim 3
Dependent Claim
25 words
The deployable air inlet duct according to claim 1 wherein a plow-shaped diverter is located between said surface closure plate and said inner duct plate.
Claim 4
Dependent Claim
53 words
The deployable air inlet duct according to claim 1 wherein said flexible leading edge comprises a silicone rubber body, at least one flexible metal cable within said body located substantially parallel to the air entrance edge of said leading edge, and at least one layer of polyester fiber fabric impregnated with silicone rubber.