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1.发明申请VARIABLE-SECTION NOZZLE, AND AIRCRAFT TURBOJET ENGINE NACELLE EQUIPPED WITH SUCH A NOZZLE 有权可变节喷嘴，以及装有喷嘴的飞机涡轮发动机公开(公告)号：US20150345423A1
公开(公告)日：2015-12-03
申请号：US14492274
申请日：2014-09-22
申请人： AIRCELLE
发明人： Hervé Hurlin , Hakim MAALIOUNE , Olivier KERBLER
CPC分类号： F01D17/141 , F01D17/20 , F01D17/22 , F01D17/24 , F02K1/06 , F02K1/08 , F02K1/085 , F02K1/09 , F02K1/10 , F02K1/11 , F02K1/12 , F02K1/1207 , F02K1/1215 , F02K1/1223 , F02K1/123 , F02K1/1238 , F02K1/1246 , F02K1/1253 , F02K1/1261 , F02K1/1269 , F02K1/1276 , F02K1/1284 , F02K1/1292 , F02K1/15 , F02K1/18 , F05D2260/407 , Y02T50/672
摘要： A variable-section nozzle for an aircraft nacelle includes a deformable portion of which is movable between a narrow section position and a wide section position. In particular, the variable-section nozzle includes piezoelectric actuators and a controller to control the piezoelectric actuators in order to displace the deformable portion between the narrow and wide section positions. The piezoelectric actuators can be disposed on at least one faces of the deformable portion or be disposed end-to-end to form actuating rods.
摘要翻译： 用于飞机机舱的可变截面喷嘴包括其可变形部分可在狭窄部分位置和宽部分位置之间移动。 特别地，可变截面喷嘴包括压电致动器和用于控制压电致动器的控制器，以便使狭窄部分和宽部分位置之间的可变形部分移位。 压电致动器可以设置在可变形部分的至少一个面上或者端对端设置以形成致动杆。
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公开(公告)号：US20170145955A1
公开(公告)日：2017-05-25
申请号：US14949315
申请日：2015-11-23
发明人： Von D. Baker
CPC分类号： F02K1/12 , B64D33/04 , F02K1/1276 , F02K3/077 , F05D2250/10 , F05D2250/13 , Y02T50/671
摘要： An exhaust system or nozzle for use in a gas turbine engine is disclosed herein. The exhaust system is adapted to adjust various streams of pressurized air produced by the gas turbine engine to control operation of the gas turbine engine.
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公开(公告)号：US3049875A
公开(公告)日：1962-08-21
申请号：US81121959
申请日：1959-05-05
申请人： UNITED AIRCRAFT CORP
发明人： HORGAN JOHN J
IPC分类号： F02K1/12
CPC分类号： F02K1/1207 , F02K1/1253 , F02K1/1261 , F02K1/1276 , F02K1/1284
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4.发明授权公开(公告)号：US09850776B2
公开(公告)日：2017-12-26
申请号：US14492274
申请日：2014-09-22
申请人： AIRCELLE
发明人： Hervé Hurlin , Hakim Maalioune , Olivier Kerbler
IPC分类号： F01D17/14 , F02K1/18 , F02K1/06 , F02K1/15 , F02K1/12 , F01D17/22 , F01D17/20 , F02K1/08 , F02K1/09 , F01D17/24 , F02K1/10 , F02K1/11
CPC分类号： F01D17/141 , F01D17/20 , F01D17/22 , F01D17/24 , F02K1/06 , F02K1/08 , F02K1/085 , F02K1/09 , F02K1/10 , F02K1/11 , F02K1/12 , F02K1/1207 , F02K1/1215 , F02K1/1223 , F02K1/123 , F02K1/1238 , F02K1/1246 , F02K1/1253 , F02K1/1261 , F02K1/1269 , F02K1/1276 , F02K1/1284 , F02K1/1292 , F02K1/15 , F02K1/18 , F05D2260/407 , Y02T50/672
摘要： A variable-section nozzle for an aircraft nacelle includes a deformable portion of which is movable between a narrow section position and a wide section position. In particular, the variable-section nozzle includes piezoelectric actuators and a controller to control the piezoelectric actuators in order to displace the deformable portion between the narrow and wide section positions. The piezoelectric actuators can be disposed on at least one faces of the deformable portion or be disposed end-to-end to form actuating rods.
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5.发明授权Longitudinally movable shroud and variable area exit nozzle for jet engine afterburner 失效用于喷气发动机后燃器的纵向移动护罩和可变区域出口喷嘴
公开(公告)号：US2840984A
公开(公告)日：1958-07-01
申请号：US30460052
申请日：1952-08-15
发明人： LAUCHER RICHARD G
IPC分类号： F02K1/12
CPC分类号： F02K1/1253 , F02K1/1207 , F02K1/1261 , F02K1/1276 , F02K1/1284
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