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公开(公告)号：US10648426B2
公开(公告)日：2020-05-12
申请号：US14995396
申请日：2016-01-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Danis Burton Smith , Mark Knowles , Shawn Alstad , Robert Romano , John Taylor Pearson , Morris Anderson , David Robinson
Abstract: A thrust reverser system comprising a single row vane assembly is provided. The provided thrust reverser system is capable of meeting performance requirements for turbine engines with reduced weight and cost.
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2.发明申请SYSTEM AND METHOD FOR REDUCING IDLE THRUST IN A TRANSLATING COWL THRUST REVERSER 审中-公开用于减少翻转轮反转器中的空闲扭矩的系统和方法公开(公告)号：US20170074211A1
公开(公告)日：2017-03-16
申请号：US14850348
申请日：2015-09-10
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Danis Burton Smith , Shawn Alstad , Robert Romano , Mark Knowles , David Robinson
CPC classification number: F02K1/605 , F02K1/09 , F02K1/60 , F02K1/70 , F02K1/72 , F02K1/763 , F02K1/766 , F05D2260/50 , F05D2260/52 , F05D2260/56
Abstract: A system and method for reducing idle thrust in a translating cowl reverser system is provided. The provided system and method provide a partial deployment, or thrust reverser system intermediate position for a translating cowl thrust reverser system.
Abstract translation: 提供了一种用于减小翻转整流罩逆变器系统中的空转推力的系统和方法。 所提供的系统和方法提供了用于平移整流罩推力反向器系统的部分部署或推力反向器系统中间位置。
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Patent Agency Ranking
公开(公告)号：US10451002B2
公开(公告)日：2019-10-22
申请号：US15004020
申请日：2016-01-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Danis Burton Smith , Mark Knowles , Robert Romano , Shawn Alstad , David Robinson
Abstract: A thrust reverser system for a turbine engine includes a support structure, a transcowl, a door, and an anti-rotation structure. The transcowl is mounted on the support structure and has an inner surface. The transcowl is axially translatable, relative to the support structure, between first and second positions. The door is pivotally coupled to the turbine engine, and has a forward edge and an aft edge. The door is rotatable between stowed and deployed positions when the transcowl translates between the first and second positions, respectively. The anti-rotation structure extends from the transcowl and is disposed adjacent to the aft edge of the door when the transcowl is in the first position and the door is in the stowed position. The anti-rotation structure is configured such that door rotation out of the stowed position only occurs subsequent to or concurrently with translation of the transcowl out of the first position.
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公开(公告)号：US10344709B2
公开(公告)日：2019-07-09
申请号：US14850348
申请日：2015-09-10
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Danis Burton Smith , Shawn Alstad , Robert Romano , Mark Knowles , David Robinson
Abstract: A system and method for reducing idle thrust in a translating cowl reverser system is provided. The provided system and method provide a partial deployment, or thrust reverser system intermediate position for a translating cowl thrust reverser system.
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公开(公告)号：US20170211510A1
公开(公告)日：2017-07-27
申请号：US15004020
申请日：2016-01-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Danis Burton Smith , Mark Knowles , Robert Romano , Shawn Alstad , David Robinson
CPC classification number: F02K1/625 , F01D25/24 , F01D25/28 , F02K1/62 , F02K1/68 , F02K1/70 , F02K1/72 , F02K1/766 , F05D2220/32 , F05D2260/30
Abstract: A thrust reverser system for a turbine engine includes a support structure, a transcowl, a door, and an anti-rotation structure. The transcowl is mounted on the support structure and has an inner surface. The transcowl is axially translatable, relative to the support structure, between first and second positions. The door is pivotally coupled to the turbine engine, and has a forward edge and an aft edge. The door is rotatable between stowed and deployed positions when the transcowl translates between the first and second positions, respectively. The anti-rotation structure extends from the transcowl and is disposed adjacent to the aft edge of the door when the transcowl is in the first position and the door is in the stowed position. The anti-rotation structure is configured such that door rotation out of the stowed position only occurs subsequent to or concurrently with translation of the transcowl out of the first position.
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公开(公告)号：US20170204809A1
公开(公告)日：2017-07-20
申请号：US14995396
申请日：2016-01-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Danis Burton Smith , Mark Knowles , Shawn Alstad , Robert Romano , John Taylor Pearson , Morris Anderson , David Robinson
CPC classification number: F02K1/625 , F01D9/041 , F01D25/24 , F01D25/28 , F02K1/605 , F02K1/72 , F05D2220/32 , F05D2240/129
Abstract: A thrust reverser system comprising a single row vane assembly is provided. The provided thrust reverser system is capable of meeting performance requirements for turbine engines with reduced weight and cost.
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7.发明申请公开(公告)号：US20160305370A1
公开(公告)日：2016-10-20
申请号：US14688779
申请日：2015-04-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Danis Burton Smith , Mark Knowles , Robert Romano , Shawn Alstad , David Robinson , Israel Picazo
CPC classification number: F02K1/605 , F02K1/72 , Y02T50/671
Abstract: A thrust reverser system capable of providing high efficiency within a tightly constrained nacelle is provided. The thrust reverser system provides a displaceable internal door pivotally mounted within a transcowl. The displaceable internal door is rotatable about a pivot axis that is positioned aft of a front edge of the transcowl when the transcowl is in a deployed position.
Abstract translation: 提供了能够在紧密限制的机舱内提供高效率的推力反向器系统。 推力反向器系统提供可枢转地安装在转子内的可移动内门。 可移动的内部门可以围绕枢转轴线旋转，当枢轴转动器处于展开位置时，该枢转轴线定位在转子的前边缘的后方。
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