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. <IMAGE>
申请公布号
EP0677439(A1)
申请公布日期
1995.10.18
申请号
EP19940102500
申请日期
1994.02.18
申请人
ROCKWELL INTERNATIONAL CORPORATION
发明人
SHORTLAND, HARRY;SHANKEN, MARTIN L.;PAXSON, PETER O.;JOHNSTON, DWAYNE C.;GUILLERMO, MAS