公开(公告)号：US3883376A

公开(公告)日：1975-05-13

申请号：US35774873

申请日：1973-05-07

Applicant: US NAVY

Inventor： BILLIG FREDERICK S ,  PIRKLE JR JAMES C ,  GRENLESKI JR STEPHEN E

IPC: C10L1/00 ,  C10L1/30

CPC classification number: C10L1/301 ,  C10L1/00 ,  C10L1/30

Abstract: The invention relates to highly reactive fuel compositions primarily intended for supersonic combustion ramjet engines. In particular, the invention provides highly reactive fuel compositions capable of efficient oxidation and thrust production even within the low combustor residence time of a supersonic combustion ramjet engine. The fuel compositions comprise specific blends of a major fuel component and an additive which, on pyrophoric combustion thereof, produces sufficient heat energy to spontaneously ignite and burn the major fuel component at a substantially increased rate.

Abstract translation: 本发明涉及主要用于超音速燃烧冲压喷气发动机的高反应性燃料组合物。 特别地，本发明提供即使在超音速燃烧式冲压式喷气发动机的低燃烧器停留时间内能够有效氧化和推力生产的高反应性燃料组合物。 燃料组合物包括主要燃料组分和添加剂的特定混合物，其在其自燃燃烧时产生足够的热能以显着增加的速率自发点燃和燃烧主要燃料组分。