F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 5/10 (2006.01) F02C 5/02 (2006.01) F02C 9/26 (2006.01) F23R 7/00 (2006.01)
Patent
CA 2696290
An engine (100) contains at least one pulse detonation combustor (103) having a combustion chamber (106) and an exit nozzle (107) coupled to and downstream of the combustion chamber (107). During operation of the at least one pulse detonation combustor (103) a detonation occurs within the combustion chamber (107) and at least one of a fuel fill fraction and purge fraction of the at least one pulse detonation combustor (103) are utilized to offset a temperature peak of said detonation from a pressure peak of said detonation. The fuel fill fraction is defined as 1 - purge fraction, and the purge fraction is the ratio of the purge time of the at least one pulse detonation combustor (103) to a sum of the purge time of the at least one pulse detonation combustor (103) and a fuel fill time of the at least one pulse detonation combustor.
Joshi Narendra Digamber
Tangirala Venkat Eswarlu
Company General Electric
Craig Wilson And Company
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