Swirling flows and swirler to enhance pulse detonation...

Power plants – Reaction motor – Intermittent combustion

Reexamination Certificate

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C060S039380, C060S039760

Reexamination Certificate

active

07614211

ABSTRACT:
A swirler having cross-sectional area comparable to the area of a detonation chamber is placed upstream of the detonation chamber to enhance the fuel-air mixing. The swirler has a first region and a second region, each of which induces swirl in the flow through the swirler. Each region induces a different direction of swirl in the flow. The residual net swirl present in the flow downstream of the swirler is controlled by the relative properties of each region of the swirler. The swirler also provides high optical blockage to inhibit the upstream propagation of flow due to the detonation shockwave.

REFERENCES:
patent: 3713588 (1973-01-01), Sharpe
patent: 5165241 (1992-11-01), Joshi et al.
patent: 5351477 (1994-10-01), Joshi et al.
patent: 5513489 (1996-05-01), Bussing
patent: 2002/0050139 (2002-05-01), Le Gal et al.
patent: 2005/0067506 (2005-03-01), Stotts et al.

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