公开(公告)号：US20140295747A1

公开(公告)日：2014-10-02

申请号：US14231993

申请日：2014-04-01

申请人： Airbus Operations GmbH

发明人： Martin Schmid ,  Christian Bartels ,  Frank Klimpel ,  Klaus Vehlhaber

IPC分类号： B64D13/00

CPC分类号： B64D13/00 ,  B64D2013/0611 ,  B64D2013/0618 ,  B64D2241/00 ,  Y02T50/56

摘要： An aircraft ram air channel assembly having: a first ram air inlet with a deflector protruding from the aircraft outer skin, the deflector guiding an air flow into a first ram air inlet channel; a second ram air inlet having a cross-sectional area flush with the outer skin, the second inlet being coupled to a second ram air inlet channel and arranged proximate to the first inlet upstream of the first inlet; and a flap pivotable about an axis between first and second operating positions. The axis is upstream of the first and second inlets and extends perpendicular to the air flow. The flap in its first position projects into the second inlet channel to control air flow through the second inlet into the second inlet channel, and in its second position projects into the air flow to prevent foreign objects from entering the first and second inlets.

摘要翻译： 一种飞机冲压空气通道组件，其具有：具有从飞行器外皮突出的偏转器的第一冲压空气入口，所述偏转器将空气流引导到第一冲压空气入口通道中; 第二冲压空气入口，其具有与外表面齐平的横截面面积，第二入口联接到第二冲压空气入口通道并且布置成靠近第一入口上游的第一入口; 以及围绕第一和第二操作位置之间的轴线枢转的挡板。 轴线位于第一和第二入口的上游，并垂直于空气流延伸。 在其第一位置的翼片进入第二入口通道以控制通过第二入口的空气流入第二入口通道，并且在其第二位置突出到空气流中以防止异物进入第一入口和第二入口。

公开(公告)号：US20190023404A1

公开(公告)日：2019-01-24

申请号：US16049012

申请日：2018-07-30

申请人： Airbus Operations GmbH

发明人： Martin Schmid ,  Christian Bartels ,  Frank Klimpel ,  Klaus Vehlhaber

IPC分类号： B64D13/00

摘要： An aircraft ram air channel assembly having: a first ram air inlet with a deflector protruding from the aircraft outer skin, the deflector guiding an air flow into a first ram air inlet channel; a second ram air inlet having a cross-sectional area flush with the outer skin, the second inlet being coupled to a second ram air inlet channel and arranged proximate to the first inlet upstream of the first inlet; and a flap pivotable about an axis between first and second operating positions. The axis is upstream of the first and second inlets and extends perpendicular to the air flow. The flap in its first position projects into the second inlet channel to control air flow through the second inlet into the second inlet channel, and in its second position projects into the air flow to prevent foreign objects from entering the first and second inlets.

公开(公告)号：US10035601B2

公开(公告)日：2018-07-31

申请号：US14231993

申请日：2014-04-01

申请人： Airbus Operations GmbH

发明人： Martin Schmid ,  Christian Bartels ,  Frank Klimpel ,  Klaus Vehlhaber

IPC分类号： B64D13/00 ,  B64D13/06

CPC分类号： B64D13/00 ,  B64D2013/0611 ,  B64D2013/0618 ,  B64D2241/00 ,  Y02T50/56

摘要： An aircraft ram air channel assembly having: a first ram air inlet with a deflector protruding from the aircraft outer skin, the deflector guiding an air flow into a first ram air inlet channel; a second ram air inlet having a cross-sectional area flush with the outer skin, the second inlet being coupled to a second ram air inlet channel and arranged proximate to the first inlet upstream of the first inlet; and a flap pivotable about an axis between first and second operating positions. The axis is upstream of the first and second inlets and extends perpendicular to the air flow. The flap in its first position projects into the second inlet channel to control air flow through the second inlet into the second inlet channel, and in its second position projects into the air flow to prevent foreign objects from entering the first and second inlets.

公开(公告)号：US10196148B1

公开(公告)日：2019-02-05

申请号：US16049012

申请日：2018-07-30

申请人： Airbus Operations GmbH

发明人： Martin Schmid ,  Christian Bartels ,  Frank Klimpel ,  Klaus Vehlhaber

IPC分类号： B64D13/00 ,  B64D13/06

摘要： An aircraft ram air channel assembly having: a first ram air inlet with a deflector protruding from the aircraft outer skin, the deflector guiding an air flow into a first ram air inlet channel; a second ram air inlet having a cross-sectional area flush with the outer skin, the second inlet being coupled to a second ram air inlet channel and arranged proximate to the first inlet upstream of the first inlet; and a flap pivotable about an axis between first and second operating positions. The axis is upstream of the first and second inlets and extends perpendicular to the air flow. The flap in its first position projects into the second inlet channel to control air flow through the second inlet into the second inlet channel, and in its second position projects into the air flow to prevent foreign objects from entering the first and second inlets.