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Power Plants > Reaction Motor (e.g., Motive Fluid Generator And Reaction Nozzle, Etc.) > Interrelated Reaction Motors Interrelated Reaction MotorsInterrelated Reaction Motors patent applications listed are from June 2005 to current and include Date, Patent Application Number, Patent Title, Patent Abstract summary and are linked to the corresponding patent application page.05/31/07 - 20070119149 - Hyperjet The present invention provides a hypersonic jet engine able to start in air-breathing mode, on its own, from zero speed without a compressor. The hypersonic jet engine, known herein as the hyperjet is also able to fly an aircraft at and faster than Mach 6 without using the scramjet method ... 02/08/07 - 20070028594 - Scramjet arrangement for hypersonic aircraft Hypersonic aircraft having a lateral arrangement of turbojet and SCRAMjet engines are disclosed. The SCRAMjet engines may be positioned laterally outboard of the turbojet engines. In one embodiment, the turbojet inlet and outlet openings may be covered during use of the SCRAMjets in order to provide compression and expansion ramps ... 08/24/06 - 20060185346 - Turbofan arrangement A bypass turbofan engine comprises a first propulsion system and a second propulsion system. The first propulsion system comprises a first fan rotor, a core engine, a first low pressure turbine and a first fan shaft drivingly connecting the first turbine and the first fan rotor. The second propulsion system ... 12/29/05 - 20050284129 - Hybrid propulsion system Whilst commercial jet aircraft are capable of transporting large pay load economically, the same is not true for rockets. To solve this problem, a hybrid propulsion system is proposed for use in Horizontal Take-Off and Land (HOTOL) craft. The purpose is to maximized the use of ambient oxygen and minimize ... 09/29/05 - 20050210863 - Methods and apparatus for operating gas turbine engines A gas turbine engine assembly includes at least one propelling gas turbine engine and an auxiliary engine used for generating power. The propelling gas turbine engine includes a fan assembly and a core engine downstream from said fan assembly. The core engine includes a compressor, a high pressure turbine, a ... 09/29/05 - 20050210862 - Quantum jet turbine propulsion system A quantum jet turbine propulsion system includes a plurality of jet turbine engines housed within an airtight common exhaust system. The individual jet turbine engines receive propulsion from fuel and air sources remote from the engines, preferably provided by fuel and air pumps and air compressors. The jet turbine propulsion ... ### FreshPatents.com Support |