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 positio
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).
대표청구항▼
1. A pulse detonation engine operating with a detonating fuel-air mixture and comprising: at least one flame tube with a transversal bottom being mobile with respect to the transversal bottom so as to be able to occupy two limit positions, a first position corresponding to detonation phase of the de
1. A pulse detonation engine operating with a detonating fuel-air mixture and comprising: at least one flame tube with a transversal bottom being mobile with respect to the transversal bottom so as to be able to occupy two limit positions, a first position corresponding to detonation phase of the detonating fuel-air mixture in a combustion chamber of said at least one flame tube and a second position corresponding a supply phase of said combustion chamber;at least one intake port of the detonating mixture arranged in a side wall of said at least one flame tube; wherein: said pulse detonation engine comprises an external shell around said flame tube defining a peripheral ring space along the side wall of said flame tube allowing an air flux to flow from an air intake of said pulse detonation engine;fixed flowing guides are arranged in the peripheral ring space to define flowing channels; andat least one mobile block arranged in the peripheral ring space and connected to a mobile bottom, is provided for moving along the side wall of said at least one flame tube, said mobile block being able to obstruct, when said mobile bottom occupies the second position, at least one of said flowing channels so as to orient part of the air flow in the direction of said at least on intake port and release said at least one of said flowing channels when said mobile bottom is in the first position. 2. The pulse detonation engine according to claim 1: wherein said fixed flowing guides are arranged parallel to each other in a concentric way around the side wall of said at least one flame tube. 3. The pulse detonation engine according to claim 1, wherein said at least one mobile block sides laterally along the side wall of said flame tube. 4. The pulse detonation engine according to claim 1, wherein said at least one mobile block joins an external face of ends opposite two adjacent fixed flowing guide so to obstruct a flowing channel partially formed by the two adjacent fixed flowing guides, when said mobile bottom occupies the second position. 5. The pulse detonation engine according to claim 1, wherein; said mobile bottom, sliding between the first position and the second position, has a shape of a piston with a transversal wall facing said combustion chamber and with a side skirt cooperating with the side wall of said at least one flame tube; anda crown, comprising at least one detonating mixture supply opening arranged on a side wall of the crown, the crown being integral with the transversal wall of said piston and cooperating with the side wall of said at least one flame tube for obstructing at least partially said at least one intake port in the second position of said mobile bottom. 6. The pulse detonation engine according to claim 1, wherein: at least one first intake port, having a flowing hole with a fixed section, is obstructed in the first position of said mobile bottom and released in the second position of said bottom; andat least one second intake port, able to receive a mobile projection, and having a flowing hole with a variable section, said hole having a reduced section in the first position of said mobile bottom and an enlarged section in the second position of a id bottom. 7. The pulse detonation engine according to claim 6, comprising at least one pre-detonation tube arranged laterally relative to said combustion chamber, at least approximately along the combustion chamber, wherein: a mobile projection is engaged into said second intake port;said mobile projection joins the internal face of the ends of one of said fixed flowing guides, when said mobile bottom occupies the first position, so as to form a transversal passage putting in fluid communication said at least one pre-detonation tube and said combustion so as to allow transfer of explosion waves; andone of the ends of said transversal passage corresponds said flowing hole of said second intake port having a reduced section, when said mobile bottom occupies the first position, and the other end corresponds to the upstream hole, oriented to the air intake, of said pre-detonation tube. 8. The pulse detonation engine according to claim 1, comprising at let one pre-detonation tube arranged laterally relative to said combustion chamber, at least approximately along the combustion chamber. 9. The pulse detonation engine according to claim 1, comprising a plurality, at least two, of pre-detonation tubes in lateral positions diametrically opposed with respect to said combustion chamber. 10. The pulse detonation engine according to claim 1, wherein at least one of said fixed guides is shaped as a fork with teeth oriented to the air intake. 11. The pulse detonation engine according to claim 1, wherein return resilient means are provided in said flame tube for bringing back said mobile bottom from the first position to the second position. 12. The pulse detonation engine according to claim 11: wherein said return resilient means comprise at least one spring acting on the transversal wall of said bottom.
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이 특허에 인용된 특허 (3)
Louis G. Hunter, Jr. ; Kent W. Benner, Annular liquid fueled pulse detonation engine.
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