公开(公告)号：US08341934B2

公开(公告)日：2013-01-01

申请号：US12280693

申请日：2006-12-07

申请人： John S. Chapkovich, III ,  Henry E. Voegeli ,  Nathan C. Blair ,  Jeffrey A. Math

发明人： John S. Chapkovich, III ,  Henry E. Voegeli ,  Nathan C. Blair ,  Jeffrey A. Math

IPC分类号： F02K1/38

CPC分类号： F02K1/825 ,  Y02T50/671

摘要： An InfraRed Suppression System (IRSS) includes a double-walled exhaust duct and double walled septum. The double walled structure provides a flow path for secondary (non-exhaust gas) cooling air flow to slots along the surfaces exposed to exhaust gases. Exhaust gas flow past these slots draws cooling air across the duct and septum surfaces. This flow cools the surfaces close to the slots and mixes with exhaust gasses downstream to cool the exhaust plume. The septum in the shape of a helix rotating 360° fully blocks line-of-sight to the turbine exit from the aft of the aircraft. The exhaust duct is intended to be shrouded by an aerodynamic fairing which provides an aerodynamic contour which minimizes aerodynamic impact on the aircraft.

摘要翻译： 红外线抑制系统（IRSS）包括双壁排气管和双壁隔膜。 双壁结构为沿着暴露于废气的表面的狭缝提供了二次（非排气）冷却空气流向槽的流动路径。 通过这些槽的排气流过管道和隔膜表面的冷却空气。 该流冷却靠近槽的表面，并与下游的废气混合以冷却排气羽流。 以360°旋转的螺旋形状的隔膜完全阻挡了从飞机后部离开涡轮机的视线。 排气管旨在被空气动力整流罩罩住，其提供空气动力学轮廓，其最小化对飞行器的空气动力学冲击。

公开(公告)号：US20090025362A1

公开(公告)日：2009-01-29

申请号：US12280693

申请日：2006-12-07

申请人： John S. Chapkovich ,  Henry E. Voegeli ,  Nathan C. Blair ,  Jeffrey A. Math

发明人： John S. Chapkovich ,  Henry E. Voegeli ,  Nathan C. Blair ,  Jeffrey A. Math

IPC分类号： B64D33/04 ,  F02K1/00 ,  F02K1/82 ,  F02C7/18

CPC分类号： F02K1/825 ,  Y02T50/671

摘要： An InfraRed Suppression System (IRSS) includes a double-walled exhaust duct and double walled septum. The double walled structure provides a flow path for secondary (non-exhaust gas) cooling air flow to slots along the surfaces exposed to exhaust gases. Exhaust gas flow past these slots draws cooling air across the duct and septum surfaces. This flow cools the surfaces close to the slots and mixes with exhaust gasses downstream to cool the exhaust plume. The septum in the shape of a helix rotating fully blocks line-of-sight to the turbine exit from the aft of the aircraft. The exhaust duct is intended to be shrouded by an aerodynamic fairing which provides an aerodynamic contour which minimizes aerodynamic impact on the aircraft.

摘要翻译： 红外线抑制系统（IRSS）包括双壁排气管和双壁隔膜。 双壁结构为沿着暴露于废气的表面的狭缝提供了二次（非排气）冷却空气流向槽的流动路径。 通过这些槽的排气流过管道和隔膜表面的冷却空气。 该流冷却靠近槽的表面，并与下游的废气混合以冷却排气羽流。 旋转螺旋形状的隔膜完全阻挡了飞机离开飞机尾部的视线。 排气管旨在被空气动力整流罩罩住，其提供空气动力学轮廓，其最小化对飞行器的空气动力学冲击。

公开(公告)号：US4473641A

公开(公告)日：1984-09-25

申请号：US68616

申请日：1979-08-22

申请人： Henry E. Voegeli

发明人： Henry E. Voegeli

IPC分类号： A23K1/00 ,  C12N1/20 ,  C12N1/26 ,  C12P21/00

CPC分类号： C12N1/26 ,  A23K10/12 ,  C12N1/20 ,  Y10S435/804 ,  Y10S435/874

摘要： Protein is produced by bacterial degradation of rubber in a nutrient-containing, preferably sterile environment. The resultant protein is particularly useful as an animal feed.

摘要翻译： 蛋白质通过含营养物质，优选无菌环境中的橡胶的细菌降解产生。 所得蛋白质作为动物饲料特别有用。