Passive venting technique for shallow cavities

Aeronautics and astronautics – Aircraft structure – Passenger or cargo loading or discharging

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2441181, 244130, B64C 700, B64D 102

Patent

active

050186884

ABSTRACT:
A device for reducing drag and store separation difficulties caused by shallow cavities on aircraft in supersonic flight consisting of a slab of porous material cut to fit precisely inside the cavity. This slab is mounted inside the cavity such that a plenum chamber is formed between the slab and the floor of the cavity. This device allows air to flow through the chamber opposite to the direction of flow outside the chamber. This results in reduced drag and improved store separation characteristics.

REFERENCES:
patent: 2791387 (1957-05-01), Weinberg
patent: 4522360 (1985-06-01), Barnwell et al.
patent: 4524670 (1985-06-01), Billard et al.
patent: 4703904 (1987-11-01), Haslund
patent: 4781342 (1988-11-01), Hardy et al.

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