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公开(公告)号：US10429160B2
公开(公告)日：2019-10-01
申请号：US15785906
申请日：2017-10-17
Applicant: THE BOEING COMPANY
Inventor： Todd W. Erickson , Sina Golshany , Shelly A. Songstad , Adriana W. Blom , Jacqueline A. Artis , Christopher R. Holtorf , Natalie Daughtry
Abstract: An artillery shell is fired out of a gun towards a fire. A trigger releases a fire-retarding material from the artillery shell to retard the fire.
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公开(公告)号：US09828084B2
公开(公告)日：2017-11-28
申请号：US14705863
申请日：2015-05-06
Applicant: The Boeing Company
Inventor： Sina Sam Golshany , Todd W. Erickson , Paul R. Tretow , David M. Huntly
CPC classification number: B64C5/02 , B64C1/26 , F16F15/002 , F16F15/022 , F16F2228/066 , F16F2230/18
Abstract: Systems and methods provide for the mitigation of vibrational forces acting on a horizontal stabilizer of an aircraft. According to one aspect, a damper is coupled to a front portion of a horizontal stabilizer to dampen vibrations in a first degree of freedom, with another damper coupled to a mounting point of the horizontal stabilizer to dampen vibrations in a second degree of freedom. The dampers may be passive, operating independently to mitigate vibrational forces, or active, applying a mitigating force to the horizontal stabilizer based on real-time or estimated vibration states.
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公开(公告)号：US20160144967A1
公开(公告)日：2016-05-26
申请号：US14555340
申请日：2014-11-26
Applicant: The Boeing Company
Inventor： Sina Golshany , Todd W. Erickson , Christopher R. Holtorf , Derek R. Alderks
CPC classification number: B64D27/18 , B64C3/32 , B64C11/001 , B64D29/02 , Y02T50/66
Abstract: A propulsion system for a transport aircraft employs a gas turbine core coupled to a wing. A ducted fan is coupled to the core gas turbine extending downstream from and integrated in a trailing edge of the airplane wing.
Abstract translation: 用于运输飞机的推进系统采用联接到机翼的燃气涡轮机芯。 管道风扇连接到从飞机机翼的后缘下游并集成在飞机机翼后缘的核心燃气涡轮机。
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公开(公告)号：US10955227B2
公开(公告)日：2021-03-23
申请号：US16559247
申请日：2019-09-03
Applicant: THE BOEING COMPANY
Inventor： Todd W. Erickson , Sina Golshany , Shelly A. Songstad , Adriana W. Blom , Jacqueline A. Artis , Christopher R. Holtorf , Natalie Daughtry
Abstract: An artillery shell is fired out of a gun towards a fire. A trigger releases a fire-retarding material from the artillery shell to retard the fire.
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公开(公告)号：US09950800B2
公开(公告)日：2018-04-24
申请号：US14555340
申请日：2014-11-26
Applicant: The Boeing Company
Inventor： Sina Golshany , Todd W. Erickson , Christopher R. Holtorf , Derek R. Alderks
CPC classification number: B64D27/18 , B64C3/32 , B64C11/001 , B64D29/02 , Y02T50/66
Abstract: A propulsion system for a transport aircraft employs a gas turbine core coupled to a wing. A ducted fan is coupled to the core gas turbine extending downstream from and integrated in a trailing edge of the airplane wing.
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Patent Agency Ranking
公开(公告)号：US09835093B2
公开(公告)日：2017-12-05
申请号：US14032163
申请日：2013-09-19
Applicant: The Boeing Company
Inventor： Sina S. Golshany , David Miles Huntly , Adriana W. Blom , Todd W. Erickson , Paul R. Tretow
IPC: F02C7/36 , F02C6/20 , B64C27/12 , B64D35/04 , F02C3/36 , B64D35/06 , B64C27/10 , B64C11/46 , F02C3/067
CPC classification number: F02C7/36 , B64C11/46 , B64C27/10 , B64C27/12 , B64D35/04 , B64D35/06 , F02C3/067 , F02C3/36 , F02C6/206 , F05D2220/325
Abstract: In one aspect a propulsion system comprises an engine and a drive assembly coupled to the engine, comprising a first driveshaft rotatable in a first direction about a first axis, a first fan coupled to the first driveshaft to rotate in the first direction, and a clutch assembly to selectively disengage the first fan from the first driveshaft. Other aspects may be described.
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公开(公告)号：US20160216091A1
公开(公告)日：2016-07-28
申请号：US14180307
申请日：2014-02-13
Applicant: The Boeing Company
Inventor： Todd W. Erickson , Sina Golshany , Shelly A. Songstad , Adriana W. Blom , Jacqueline A. Artis , Christopher R. Holtorf , Natalie Daughtry
CPC classification number: F42B12/50 , A62C3/0228 , A62C3/025 , F42C19/0838
Abstract: An artillery shell is fired out of a gun towards a fire. A trigger releases a fire-retarding material from the artillery shell to retard the fire.
Abstract translation: 炮弹从炮火中射出一个炮弹。 触发器从炮弹释放阻燃材料以阻止火灾。
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公开(公告)号：US10018058B2
公开(公告)日：2018-07-10
申请号：US14798788
申请日：2015-07-14
Applicant: The Boeing Company
Inventor： Sina Golshany , Todd W. Erickson
Abstract: A propulsion unit having reduced noise employs a rotor having a plurality of variable pitch blades. A tensioning joint mechanism is carried within each blade and a tension element is engaged by the tension joint mechanism. The tension element is configured to maintain tension between the blades in the rotor and the tensioning joint mechanism adapted to allow variation of pitch of the blades without altering tension in the tension element.
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公开(公告)号：US20180118364A1
公开(公告)日：2018-05-03
申请号：US15343116
申请日：2016-11-03
Applicant: THE BOEING COMPANY
Inventor： Sina S. Golshany , Todd W. Erickson , Derek R. Alderks
CPC classification number: B64D35/08 , B64D27/02 , B64D27/16 , B64D27/24 , B64D31/06 , B64D2027/026 , F02C6/06 , F02C7/36 , F05D2220/323 , F05D2220/70 , F05D2260/4023
Abstract: An aircraft propulsion system includes a fan, a primary powerplant, an augmenting powerplant and a controller. The primary powerplant is coupled to the fan and configured to rotate the fan during a first flight stage and during a second flight stage. The augmenting powerplant is coupleable with the fan. The controller is configured to cause the augmenting powerplant to drive the fan during the first flight stage, and to cause the augmenting powerplant to cease driving the fan based on an indication of a transition from the first flight stage to the second flight stage.
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公开(公告)号：US09816791B2
公开(公告)日：2017-11-14
申请号：US14180307
申请日：2014-02-13
Applicant: The Boeing Company
Inventor： Todd W. Erickson , Sina Golshany , Shelly A. Songstad , Adriana W. Blom , Jacqueline A. Artis , Christopher R. Holtorf , Natalie Daughtry
CPC classification number: F42B12/50 , A62C3/0228 , A62C3/025 , F42C19/0838
Abstract: An artillery shell is fired out of a gun towards a fire. A trigger releases a fire-retarding material from the artillery shell to retard the fire.
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