摘要:
The invention relates to a pulse detonation engine operating with an air-fuel mixture. According to the invention, the engine (1) includes at least two predetonation tubes (4, 5) which operate under conditions close to thermal cutoff conditions and the shock waves from which are focused in the combustion chamber (19).
摘要:
An engine including a means for supplying fuel to the combustion chamber of the fire tube, that includes a variable-volume transfer chamber for receiving fuel, a fuel transfer means from the tank of the engine towards the transfer chamber, and injection means for injecting fuel into the combustion chamber from the transfer chamber. The engine further includes an elastic return at least partially defined by the fuel contained in the transfer chamber.
摘要:
According to the invention, the said engine (I), which comprises at least one flame tube (2) with a mobile transverse end wall (18), comprises an external envelope (3) around the said flame tube (2), which defines a peripheral annular space (4) in which fixed flow guides (11, 12, 13, 14) are positioned, these flow guides forming flow channels (10) for the air, and at least one mobile plug (25), connected to the said mobile end wall (18), to close off and open one of the flow channels (10).
摘要:
According to the invention, the engine (I) includes a means for supplying fuel to the combustion chamber (7) of the fire tube (2), that comprises a variable-volume transfer chamber (9) for receiving fuel, a fuel transfer means (10) from the tank (4) of the engine (I) towards the transfer chamber (9), and injection means (11) for injecting fuel into the combustion chamber (7) from the transfer chamber (9). The engine further includes an elastic return means at least partially defined by the fuel contained in the transfer chamber (9).
摘要:
According to the invention, the said engine (I), which comprises at least one flame tube (2) with a mobile transverse end wall (18), comprises an external envelope (3) around the said flame tube (2), which defines a peripheral annular space (4) in which fixed flow guides (11, 12, 13, 14) are positioned, these flow guides forming flow channels (10) for the air, and at least one mobile plug (25), connected to the said mobile end wall (18), to close off and open one of the flow channels (10).
摘要:
The invention relates to a pulse detonation engine operating with an air-fuel mixture. According to the invention, the engine (1) includes at least two predetonation tubes (4, 5) which operate under conditions close to thermal cutoff conditions and the shock waves from which are focused in the combustion chamber (19).
摘要:
To generate an unpolluted high enthalpy air blast of several seconds duration a mass of feed air intended to constitute the high enthalpy air blast is preheated to a given temperature and stored at a given pressure in an elongate confinement tunnel with thermally insulative walls. A downstream orifice of the tunnel is kept closed and a blast of high-pressure air is applied to the upstream end of the mass of feed air to compress it quasi adiabatically to obtain a feed air temperature of at least 1,800K. The downstream orifice is opened and application of the high-pressure air blast is continued whereby the mass of feed air is expelled through the downstream orifice in the form of a feed blast, the temperature of which remains constant for several seconds.