发明名称 HYPERVELOCITY WIND TUNNEL WITH BALLISTIC PISTON
摘要 A hypervelocity wind tunnel comprising compression tube (10) lengthened to increase piston speed and working pressure, a diaphragm (33), a shock tube (31), a high pressure reservoir supplying compressed air that propels a piston (21) along the compression tube (10) and an inlet valve (44) through which working gas can enter into the shock tube (31) via an isolating plenum (42). Stress wave dampers (49, 50, 51, 52) connected by a yoke (48) to either the compression tube (10) or the shock tube (31) enable the wind tunnel to withstand the higher working pressure. A cyclonic diaphragm seat (40) ensures that diaphragm fragments are carried towards the shock tube wall. The piston (21) may be loaded via a breech mechanism (20) locked by a locking ring (25). Compressed air may be injected into a space (23) to initially drive the piston (21) along the compression tube (10) until the high pressure reservoir is connected via ports (13, 22) to the space (23) behind the piston (21).
申请公布号 WO8902071(A1) 申请公布日期 1989.03.09
申请号 WO1988AU00330 申请日期 1988.08.26
申请人 UNIVERSITY OF QUEENSLAND 发明人 STALKER, RAYMOND, JOHN
分类号 G10K15/04;(IPC1-7):G01M9/00 主分类号 G10K15/04
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