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公开(公告)号：US09540114B2
公开(公告)日：2017-01-10
申请号：US14771431
申请日：2014-03-03
Applicant: United Technologies Corporation
Inventor： Eric Andrew Nager , James C. Napier , Farooq Rehman , Anthony C. Jones
CPC classification number: B64D33/06 , B64D41/00 , B64D2041/002 , F01D25/30 , F02C7/24 , F02C7/32 , F05D2220/50 , F05D2260/96 , Y02T50/44
Abstract: An exhaust system for an APU in a gas turbine engine aircraft having a tail cone in which exhaust noise is reduced. An APU exhaust liner is attached to the APU and extending to an oval cutout at the tail cone The liner has a first constant cross section from the APU to a point proximate the tail cone, and a second, increasing cross section from the point proximate the tail cone to the liner cutout. The liner is turned toward the side of the tail. The liner cutout is further enlarged with at least one larger cutout.
Abstract translation: 一种用于燃气涡轮发动机飞行器中的APU的排气系统，其具有减少排气噪声的尾锥。 APU排气衬套连接到APU并延伸到尾锥处的椭圆形切口。衬套具有从APU到靠近尾锥的点的第一恒定横截面，以及从接近尾部的点增加的第二截面 尾锥到衬里切口。 衬里转向尾部侧面。 衬套切口进一步放大至少一个更大的切口。
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Patent Agency Ranking
公开(公告)号：US09469412B2
公开(公告)日：2016-10-18
申请号：US14439356
申请日：2013-10-28
Applicant: United Technologies Corporation
Inventor： Eric Andrew Nager , David Lau
CPC classification number: B64D41/00 , B64D2041/002
Abstract: An auxiliary power unit mounting system according to an exemplary aspect of the present disclosure includes, among other things, a plurality of linkages to support an auxiliary power unit, and a redundant mount to selectively support said auxiliary power unit.
Abstract translation: 根据本公开的示例性方面的辅助动力装置安装系统尤其包括用于支撑辅助动力单元的多个联动装置以及用于选择性地支撑所述辅助动力装置的冗余支架。
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公开(公告)号：US20160244178A1
公开(公告)日：2016-08-25
申请号：US15026555
申请日：2014-08-29
Applicant: United Technologies Corporation
Inventor： Brett Colin Bonner , Eric Andrew Nager
CPC classification number: B64D33/04 , B64D41/00 , B64D2041/002 , F01D25/28 , F01D25/30 , F02C7/20 , F02K1/04 , F05D2220/50 , F05D2230/60 , F05D2230/644 , F05D2250/241 , F05D2250/711 , F05D2250/712 , F05D2260/30
Abstract: An exhaust system for an aircraft includes an exhaust duct configured to be inserted within a plurality of leaf springs of an aircraft. The exhaust duct is configured to be in fluid communication with the auxiliary power unit for conveying exhaust from the auxiliary power unit to an exhaust exit, the exhaust duct including at least one exhaust bracket for movably mounting the exhaust duct to an airframe. An alignment system is configured to be operatively connected to the exhaust duct.
Abstract translation: 用于飞行器的排气系统包括被配置为插入飞行器的多个板簧内的排气管道。 排气管被构造成与辅助动力单元流体连通，用于将排气从辅助动力单元输送到排气出口，排气管道包括至少一个排气支架，用于将排气管可移动地安装到机身上。 对准系统被配置为可操作地连接到排气管。
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公开(公告)号：US10246198B2
公开(公告)日：2019-04-02
申请号：US15026555
申请日：2014-08-29
Applicant: United Technologies Corporation
Inventor： Brett Colin Bonner , Eric Andrew Nager
Abstract: An exhaust system for an aircraft includes an exhaust duct configured to be inserted within a plurality of leaf springs of an aircraft. The exhaust duct is configured to be in fluid communication with the auxiliary power unit for conveying exhaust from the auxiliary power unit to an exhaust exit, the exhaust duct including at least one exhaust bracket for movably mounting the exhaust duct to an airframe. An alignment system is configured to be operatively connected to the exhaust duct.
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公开(公告)号：US20160001890A1
公开(公告)日：2016-01-07
申请号：US14771431
申请日：2014-03-03
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Eric Andrew Nager , James C. Napier , Farooq Rehman , Anthony C. Jones
CPC classification number: B64D33/06 , B64D41/00 , B64D2041/002 , F01D25/30 , F02C7/24 , F02C7/32 , F05D2220/50 , F05D2260/96 , Y02T50/44
Abstract: An exhaust system for an APU in a gas turbine engine aircraft having a tail cone in which exhaust noise is reduced. An APU exhaust liner is attached to the APU and extending to an oval cutout at the tail cone The liner has a first constant cross section from the APU to a point proximate the tail cone, and a second, increasing cross section from the point proximate the tail cone to the liner cutout. The liner is turned toward the side of the tail. The liner cutout is further enlarged with at least one larger cutout.
Abstract translation: 一种用于燃气涡轮发动机飞行器中的APU的排气系统，其具有减少排气噪声的尾锥。 APU排气衬套连接到APU并延伸到尾锥处的椭圆形切口。衬套具有从APU到靠近尾锥的点的第一恒定横截面，以及从接近尾部点的第二个增加的横截面 尾锥到衬里切口。 衬里转向尾部侧面。 衬套切口进一步放大至少一个更大的切口。
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公开(公告)号：US20150298815A1
公开(公告)日：2015-10-22
申请号：US14439356
申请日：2013-10-28
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Eric Andrew Nager , David Lau
IPC: B64D41/00
CPC classification number: B64D41/00 , B64D2041/002
Abstract: An auxiliary power unit mounting system according to an exemplary aspect of the present disclosure includes, among other things, a plurality of linkages to support an auxiliary power unit, and a redundant mount to selectively support said auxiliary power unit.
Abstract translation: 根据本公开的示例性方面的辅助动力装置安装系统尤其包括用于支撑辅助动力单元的多个联动装置以及用于选择性地支撑所述辅助动力装置的冗余支架。
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