Temperature normalized structure

Temperature normalized structure

Circulation of temperature controlled fluid through cavities in structure stiffening members (30) of hypersonic aerospace vehicles allows normalizing of destructive temperature gradients in such members and preserves stress residuals for functional requirements.

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Bibliographische Detailangaben
Hauptverfasser: PAXSON, PETER O, SHANKEN, MARTIN L, GUILLERMO, MAS, SHORTLAND, HARRY, JOHNSTON, DWAYNE C
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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Beschreibung
Zusammenfassung:Circulation of temperature controlled fluid through cavities in structure stiffening members (30) of hypersonic aerospace vehicles allows normalizing of destructive temperature gradients in such members and preserves stress residuals for functional requirements.