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1.发明公开Aircraft, particularly small aircraft, having a propulsion system including a plurality of pulse detonation engines (PDEs) 有权Flugzeug mit einem Antriebssystem bestehend aus mehreren pulsierten Detonationskraftmaschinen
公开(公告)号：EP1557356A1
公开(公告)日：2005-07-27
申请号：EP04425043.9
申请日：2004-01-26
发明人： Perlo, Piero , Golub, Victor , Kotelnikov, Andrei
摘要： A small aircraft is disclosed having a propulsion system including a plurality of Pulse Detonation Engines (PDEs). The engines are arranged within the wings (2a) of the aircraft. The discharge nozzles (8) of the detonation tubes (7) of the detonation engines are provided at different areas of the aircraft and are differently oriented, so as to provide extra manoeuvrability along the three directions. The arrangement of the detonation tubes (7) within the wings (2a) reduces drag and hence the fuel consumption.
摘要翻译： 公开了一种具有包括多个脉冲爆震引擎（PDE）的推进系统的小型飞机。 发动机布置在飞机的机翼（2a）内。 爆震发动机的引爆管（7）的排放喷嘴（8）设置在飞行器的不同区域，并且具有不同的定向，以便沿着三个方向提供额外的机动性。 在翼（2a）内的引爆管（7）的布置减少了阻力并因此降低了燃料消耗。
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2.发明公开
公开(公告)号：EP1548363A2
公开(公告)日：2005-06-29
申请号：EP04029268.2
申请日：2004-12-10
发明人： Perlo, Pietro , Innocenti, Gianfranco , Kotelnikov, Andrei , Li Pira, Nello , Brignone, Mauro , Lambertini, Vito
CPC分类号： F16C39/063 , F01D1/32 , F02C3/16 , F02C3/165 , F02K7/005 , F16C32/0427 , F16C32/0429 , F23C15/00 , F23R3/52 , F23R3/56 , H02K7/09 , H02K7/1823
摘要： The combustor (1) comprises a stationary structure (2), and at least one annular rotor supported rotatably about a shaft (4) by contactless suspension means (5-8). The rotor (3) comprises a first and a second main annular portions (3', 3'') which are interconnected by an intermediate annular portion (103) and in each of which there is defined a combustion chamber (20', 20'') that has a directed lateral opening (22, 24) for the ejection of the combustion gases. Each combustion chamber (20', 20'') has an injector (31', 31'') of fuel and oxidizer and an igniter (32', 32'') which extend through a circular opening (50) in the said intermediate annular portion (103) of the rotor (3). The injectors (31', 31'') and the associated igniters (32', 32'') extend through narrow circular slits (30', 30'') defined between each main annular portion (3', 3'') and the intermediate portion (103) of the rotor.
This intermediate portion (103) communicates with the region outside the rotor (3) through a circularly extending radial exhaust nozzle (60) of convergent-divergent type connected to the said circular opening (50) and having in cross section the shape of a De Laval nozzle.摘要翻译： 所述燃烧器（1）包括一个固定结构（2），和至少一个环形设计转子可转动地支承绕轴（4）通过非接触方式悬浮液（5-8）。 转子（3）包括一个第一和一个第二主环形图案部（3“ 3' ‘），其是通过在中间环状设计部（103）相互连接，并且在其中的每一个限定有燃烧室（20’，20” “）确实具有用于燃烧气体的喷射横向导向的开口（22，24）。 每个燃烧室（20“ 20' ‘）具有在所述中间燃料和氧化剂，并点火器（32”，32' “），它通过一个圆形开口（50）延伸的喷射器（31’，31‘’） 转子的环形设计部（103）（3）。 每个主环形图案部之间限定的喷射器（31 '31' '）和相关的点火器（32'，32 ''）通过窄的圆形槽延伸（30'，30' '）（3'，3 ''）和 转子的中间部分（103）。 此中间部分（103）与所述转子外侧的区域连通（3）通过在横截面中具有连接到所述圆形开口（50）会聚 - 发散型和的径向延伸的圆排气喷嘴（60）的 塑造德拉瓦尔喷嘴的。
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3.发明公开
公开(公告)号：EP1548363A3
公开(公告)日：2005-09-28
申请号：EP04029268.2
申请日：2004-12-10
发明人： Perlo, Pietro , Innocenti, Gianfranco , Kotelnikov, Andrei , Li Pira, Nello , Brignone, Mauro , Lambertini, Vito
CPC分类号： F16C39/063 , F01D1/32 , F02C3/16 , F02C3/165 , F02K7/005 , F16C32/0427 , F16C32/0429 , F23C15/00 , F23R3/52 , F23R3/56 , H02K7/09 , H02K7/1823
摘要： The combustor (1) comprises a stationary structure (2), and at least one annular rotor supported rotatably about a shaft (4) by contactless suspension means (5-8). The rotor (3) comprises a first and a second main annular portions (3', 3'') which are interconnected by an intermediate annular portion (103) and in each of which there is defined a combustion chamber (20', 20'') that has a directed lateral opening (22, 24) for the ejection of the combustion gases. Each combustion chamber (20', 20'') has an injector (31', 31'') of fuel and oxidizer and an igniter (32', 32'') which extend through a circular opening (50) in the said intermediate annular portion (103) of the rotor (3). The injectors (31', 31'') and the associated igniters (32', 32'') extend through narrow circular slits (30', 30'') defined between each main annular portion (3', 3'') and the intermediate portion (103) of the rotor.
This intermediate portion (103) communicates with the region outside the rotor (3) through a circularly extending radial exhaust nozzle (60) of convergent-divergent type connected to the said circular opening (50) and having in cross section the shape of a De Laval nozzle.-
4.发明授权
公开(公告)号：EP1557356B1
公开(公告)日：2005-12-14
申请号：EP04425043.9
申请日：2004-01-26
发明人： Perlo, Piero , Golub, Victor , Kotelnikov, Andrei
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