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公开(公告)号：US4662658A
公开(公告)日：1987-05-05
申请号：US616624
申请日：1984-06-04
申请人： Joseph Holowach , James A. Crowley
发明人： Joseph Holowach , James A. Crowley
CPC分类号： F02K1/386 , F02K1/80 , Y02T50/671 , Y10S285/917
摘要： Seal means for reducing the gas flow through the space between the opposing ends of first and second concentric axially disposed cylinders is disclosed. The seal means includes a presizeable annular leaf seal concentrically mateable with the first cylinder. In addition, the seal means includes securing means for securing the left seal to the second cylinder. In a specific embodiment, the seal means provides an effective seal between a turbine rear frame and mixer liner.
摘要翻译： 公开了用于减少通过第一和第二同心轴向设置的气缸的相对端之间的空间的气流的密封装置。 密封装置包括与第一气缸同心地配合的可预定的环形叶片密封件。 此外，密封装置包括用于将左密封件固定到第二气缸的固定装置。 在具体实施例中，密封装置在涡轮机后框架和混合器衬套之间提供有效的密封。
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公开(公告)号：US4813608A
公开(公告)日：1989-03-21
申请号：US939999
申请日：1986-12-10
申请人： Joseph Holowach , George D. Lee
发明人： Joseph Holowach , George D. Lee
CPC分类号： F02K1/805 , F16J15/025 , F16J15/164
摘要： A bimetallic leaf seal 40 for forming an air seal between adjacent structures (38, 42). The bimetallic seal 40 comprises two metallic layers 46, 48 having different coefficients of thermal expansion. The seal moves in a preferred direction upon the application of heat to form an air seal upon the application of heat.
摘要翻译： 用于在相邻结构（38,42）之间形成空气密封的双金属叶片密封件40。 双金属密封件40包括具有不同热膨胀系数的两个金属层46,48。 在施加热量时，密封件沿优选方向移动，以在施加热量时形成空气密封。
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公开(公告)号：US4106587A
公开(公告)日：1978-08-15
申请号：US702115
申请日：1976-07-02
申请人： Dudley O. Nash , Joseph Holowach
发明人： Dudley O. Nash , Joseph Holowach
CPC分类号： G10K11/172 , F02K1/827
摘要： Sound-suppressing structure comprising stacked acoustic panels wherein the inner high frequency panel is mounted for thermal expansion with respect to the outer low frequency panel. Slip joints eliminate the potential for thermal stresses, and a thermal expansion gap between the panels provides for additional relative thermal growth while reducing heat convection into the low frequency panel.
摘要翻译： 声压抑制结构包括堆叠的声学面板，其中内部高频面板被安装用于相对于外部低频面板的热膨胀。 滑动接头消除了热应力的可能性，并且面板之间的热膨胀间隙提供额外的相对热增长，同时减少进入低频面板的热对流。
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4.发明授权公开(公告)号：US06857600B1
公开(公告)日：2005-02-22
申请号：US10133077
申请日：2002-04-26
CPC分类号： F02K1/822 , F02K1/12 , F02K1/1207 , Y02T50/671 , Y02T50/675
摘要： A two dimensional gas turbine engine exhaust nozzle includes transversely spaced apart upper and lower convergent and divergent flaps and extending longitudinally in a downstream direction and between two widthwise spaced apart sidewalls. The divergent flaps have inwardly facing upper and lower flap surfaces defining together with the sidewalls at least a part of an exhaust stream flowpath therebetween. The upper and lower flap surfaces have respective upper and lower apexes wherein the upper apex is axially spaced apart and aft of the lower apex. The upper divergent flap has an expansion ramp diverging away from the nozzle axis. The ramp extends aftwardly from the upper apex and aftwardly of a trailing edge of the lower divergent flap. The upper and lower divergent flaps are operably movable to block a line of sight along the nozzle axis through an exit of the nozzle during engine operation.
摘要翻译： 二维燃气涡轮发动机排气喷嘴包括横向间隔开的上部和下部会聚和发散的翼片，并且在下游方向上和两个宽度方向间隔开的侧壁之间纵向延伸。 发散的翼片具有向内的上和下翼片表面，其与侧壁一起限定其间的排气流流路的至少一部分。 上和下翼片表面具有相应的上顶点和下顶点，其中上顶点轴向间隔开并且下顶点的后部。 上发散片具有从喷嘴轴线分叉的膨胀斜面。 斜坡从上顶点向后延伸，并从下发散瓣的后缘向后延伸。 在发动机运行期间，上部和下部发散翼片可操作地移动以阻挡沿着喷嘴轴线的视线通过喷嘴的出口。
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公开(公告)号：US5690280A
公开(公告)日：1997-11-25
申请号：US571793
申请日：1990-08-24
CPC分类号： F02K1/006 , F02K1/12 , Y02T50/671
摘要： A short take off and vertical landing (STOVL) nozzle for a jet aircraft provides thrust reversing and thrust vectoring functions using two pairs of flaps. Each flap is independently actuated and controlled to allow for numerous exhaust gas exit configurations. A two dimensional or rectangular center plug extends across the nozzle throat region to allow one pair of flaps to selectively engage the plug for STOVL operation.
摘要翻译： 用于喷气式飞机的短起飞和垂直着陆（STOVL）喷嘴使用两对襟翼提供推力反向和推力矢量功能。 每个挡板被独立地致动和控制，以允许许多废气排出构造。 二维或矩形中心塞延伸穿过喷嘴喉部区域，以允许一对翼片选择性地接合插头用于STOVL操作。
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