公开(公告)号：US20130319003A1

公开(公告)日：2013-12-05

申请号：US13483466

申请日：2012-05-30

Applicant: Jason Peel ,  Jack V. Vitale ,  Greg R. Giddings

Inventor： Jason Peel ,  Jack V. Vitale ,  Greg R. Giddings

IPC: B64D41/00

CPC classification number: B64D41/00 ,  B64D2041/002

Abstract: An auxiliary power unit has a gas turbine engine, a generator, and a gear box. A mount bracket is mechanically attached to the gear box. The bracket is for connecting to a plurality of struts. The struts are for connecting to an aircraft housing. A shield box is formed of a flame resistant rigid material. The shield box encloses the mount bracket to provide flame protection to the mechanical attachment.

Abstract translation: 辅助动力单元具有燃气涡轮发动机，发电机和齿轮箱。 安装支架机械地连接到齿轮箱。 支架用于连接多个支柱。 支柱用于连接飞机外壳。 屏蔽箱由耐火刚性材料形成。 屏蔽盒包围安装支架，为机械附件提供火焰保护。

公开(公告)号：US20130001009A1

公开(公告)日：2013-01-03

申请号：US13170600

申请日：2011-06-28

Applicant: Jay M. Francisco ,  Anthony C. Jones ,  Greg R. Giddings ,  Nagamany Thayalakhandan ,  Jason Peel

Inventor： Jay M. Francisco ,  Anthony C. Jones ,  Greg R. Giddings ,  Nagamany Thayalakhandan ,  Jason Peel

IPC: F01N13/08

CPC classification number: F02K1/46 ,  B64D33/06 ,  B64D2041/002 ,  F01N1/08 ,  F02K1/827 ,  F05D2220/50 ,  Y02T50/671

Abstract: An exhaust silencer assembly for use with an auxiliary power unit includes an eductor and a discharge pipe. The eductor is disposed downstream of the auxiliary power unit and has an entrance opening at a forward axial end thereof. The entrance opening is configured to receive exhaust airflow from the auxiliary power unit. The discharge pipe extends from the auxiliary power unit and communicates with the exhaust silencer assembly downstream of the entrance opening of the eductor.

Abstract translation: 与辅助动力单元一起使用的排气消音器组件包括喷射器和排出管。 喷射器设置在辅助动力单元的下游，并且在其前轴向端部具有入口。 入口开口构造成从辅助动力单元接收排气。 排放管从辅助动力单元延伸，并与喷射器入口的下游的排气消声器组件连通。

公开(公告)号：US20130320134A1

公开(公告)日：2013-12-05

申请号：US13484880

申请日：2012-05-31

Applicant: Melissa A. Bell ,  Michael J. Rollins ,  Jason Peel ,  Greg R. Giddings

Inventor： Melissa A. Bell ,  Michael J. Rollins ,  Jason Peel ,  Greg R. Giddings

IPC: B64D27/14

CPC classification number: B64D41/00 ,  B64D2041/002

Abstract: An auxiliary power unit is composed of a gas turbine engine, a gearbox, and a gearbox driven generator. A mount bracket is mechanically attached to the gearbox. The bracket is for connecting to an aircraft strut system. The aircraft strut system connects to the aircraft structure. The mount bracket has an upper mechanical attachment point and a lower mechanical attachment point to the gearbox. The gearbox includes an oil reservoir, and the lower attachment point is beneath the oil level within the oil reservoir such that said lower attachment point will be cooled by oil in the oil reservoir.

Abstract translation: 辅助动力单元由燃气涡轮发动机，变速箱和齿轮箱驱动的发电机组成。 安装支架机械地连接到齿轮箱。 支架用于连接飞机支柱系统。 飞机支柱系统连接到飞机结构。 安装支架具有上部机械连接点和到齿轮箱的下部机械连接点。 齿轮箱包括储油器，并且下附接点在储油器内的油位下方，使得所述下连接点将被油储存器中的油冷却。

公开(公告)号：US08556027B2

公开(公告)日：2013-10-15

申请号：US13170600

申请日：2011-06-28

Applicant: Jay M. Francisco ,  Anthony C. Jones ,  Greg R. Giddings ,  Nagamany Thayalakhandan ,  Jason Peel

Inventor： Jay M. Francisco ,  Anthony C. Jones ,  Greg R. Giddings ,  Nagamany Thayalakhandan ,  Jason Peel

IPC: F02K1/82 ,  F02K1/34 ,  F01N1/14 ,  F02K1/00 ,  F01N1/00

CPC classification number: F02K1/46 ,  B64D33/06 ,  B64D2041/002 ,  F01N1/08 ,  F02K1/827 ,  F05D2220/50 ,  Y02T50/671

Abstract: An exhaust silencer assembly for use with an auxiliary power unit includes an eductor and a discharge pipe. The eductor is disposed downstream of the auxiliary power unit and has an entrance opening at a forward axial end thereof. The entrance opening is configured to receive exhaust airflow from the auxiliary power unit. The discharge pipe extends from the auxiliary power unit and communicates with the exhaust silencer assembly downstream of the entrance opening of the eductor.

Abstract translation: 与辅助动力单元一起使用的排气消音器组件包括喷射器和排出管。 喷射器设置在辅助动力单元的下游，并且在其前轴向端部具有入口。 入口开口构造成从辅助动力单元接收排气。 排放管从辅助动力单元延伸，并与喷射器入口的下游的排气消声器组件连通。

公开(公告)号：US08864067B2

公开(公告)日：2014-10-21

申请号：US13484880

申请日：2012-05-31

Applicant: Melissa A. Bell ,  Michael J. Rollins ,  Jason Peel ,  Greg R. Giddings

Inventor： Melissa A. Bell ,  Michael J. Rollins ,  Jason Peel ,  Greg R. Giddings

IPC: B64D27/00 ,  B64D41/00

CPC classification number: B64D41/00 ,  B64D2041/002

Abstract: An auxiliary power unit is composed of a gas turbine engine, a gearbox, and a gearbox driven generator. A mount bracket is mechanically attached to the gearbox. The bracket is for connecting to an aircraft strut system. The aircraft strut system connects to the aircraft structure. The mount bracket has an upper mechanical attachment point and a lower mechanical attachment point to the gearbox. The gearbox includes an oil reservoir, and the lower attachment point is beneath the oil level within the oil reservoir such that said lower attachment point will be cooled by oil in the oil reservoir.

Abstract translation: 辅助动力单元由燃气涡轮发动机，变速箱和齿轮箱驱动的发电机组成。 安装支架机械地连接到齿轮箱。 支架用于连接飞机支柱系统。 飞机支柱系统连接到飞机结构。 安装支架具有上部机械连接点和到齿轮箱的下部机械连接点。 齿轮箱包括储油器，并且下附接点在储油器内的油位下方，使得所述下连接点将被油储存器中的油冷却。