Space Engine [UPDATED]
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Throughout the duration of the development of a hybrid DASS/turbojet engine at the University of Calgary, the engine has been evaluated both in the lab and in the wind tunnel. At the University of Calgary, they are currently working on a testbed for a hybrid DASS/turbojet engine that will be used to test the models developed at the ASD Lab. The hybrid engine is scheduled to be developed for the next phase of the hybrid hybrid engine development. They are also working on the development of a hybrid DASS/turbojet engine using a 4-shaft propulsion system.
The company also has an interest in developing a hybrid engine using a DASS engine and a conventional turbojet. The conventional turbojet would provide the thrust necessary to achieve the initial acceleration of the hybrid engine.
The DASS engine was designed by the company in collaboration with SaskPower and the University of Calgary's Advanced Engine Systems Design Laboratory (ASD Lab). The partners have done extensive work in the design of turbojet engines for ground-based applications and the hybrid version is believed to be the first of its kind. The ASD Lab's expertise in computational fluid dynamics and in particular computational thermodynamics is a key element to the development of a hybrid engine. One of the major benefits of a hybrid engine is the ability to carry auxiliary fuel for a certain period of time without any increase in specific thrust. This allows the use of advanced combustion modes that would otherwise be impractical without the use of auxiliary fuels. For example, in the case of a hybrid DASS/turbojet engine, auxiliary fuel can be used to pre-heat the incoming air to improve combustion and decrease unburned hydrocarbon emissions. This combustion mode is not possible in conventional turbofan engines because a conventional turbofan engine has to have stable and self-sustained combustion to produce thrust. If auxiliary fuel is allowed to burn in a conventional turbofan engine, there will be a significant increase in specific thrust and/or burning fuel may be a hazard to the engine and its components.
SES is looking at the possibility of adaptively designing a hybrid engine system that has the capability of switching between ramjet and ramjet and turbojet modes under a selection of flight conditions. The transition between modes would be seamless as the aerodynamics changes and no increase in specific thrust would be required.
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