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公开(公告)号：US20110204187A1
公开(公告)日：2011-08-25
申请号：US13092940
申请日：2011-04-23
Applicant: Peter Spirov , Brad Pedersen
Inventor： Peter Spirov , Brad Pedersen
IPC: B64C13/20
CPC classification number: G05D1/0816 , B60V1/06 , B60V1/10 , B64C15/02 , B64C27/08 , B64C27/20 , B64C39/001 , B64C39/024 , B64C2201/042 , B64C2201/10 , B64C2201/108 , B64C2201/146 , B64D27/24 , G05D1/0016 , G05D1/0022 , G05D1/0858
Abstract: A homeostatic flying hovercraft preferably utilizes at least two pairs of counter-rotating ducted fans to generate lift like a hovercraft and utilizes a homeostatic hover control system to create a flying craft that is easily controlled. The homeostatic hover control system provides true homeostasis of the craft with a true fly-by-wire flight control and control-by-wire system control.
Abstract translation: 稳态飞行气垫船优选地使用至少两对反向旋转管道风扇来产生类似气垫船的升降机，并且利用稳态悬停控制系统来创建易于控制的飞行器。 稳态悬停控制系统通过真正的线控飞行控制和线控系统控制为飞行器提供真正的动态平衡。
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公开(公告)号：US20060144994A1
公开(公告)日：2006-07-06
申请号：US10526153
申请日：2003-09-02
Applicant: Peter Spirov , Brad Pedersen
Inventor： Peter Spirov , Brad Pedersen
IPC: B64C39/00
CPC classification number: G05D1/0816 , B60V1/06 , B60V1/10 , B64C15/02 , B64C27/08 , B64C27/20 , B64C39/001 , B64C39/024 , B64C2201/042 , B64C2201/10 , B64C2201/108 , B64C2201/146 , B64D27/24 , G05D1/0016 , G05D1/0022 , G05D1/0858
Abstract: A homeostatic flying hovercraft preferably utilizes at least two pairs of counter-rotating ducted fans to generate lift like a hovercraft and utilizes a homeostatic hover control system to create a flying craft that is easily controlled. The homeostatic hover control system provides true homeostasis of the craft with a true fly-by-wire flight control and control-by-wire system control.
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公开(公告)号：US11905000B2
公开(公告)日：2024-02-20
申请号：US16089643
申请日：2017-03-23
Applicant: NIKON CORPORATION
Inventor： Katsuki Ohata , Takanori Shioda , Marie Shimoyama , Toru Kijima , Shinichi Miyauchi , Sho Nakamura , Ryo Tsubata , Masaki Kaneko
CPC classification number: B64C13/18 , B64C13/20 , B64C39/024 , B64D47/08 , G05D1/00 , G05D1/0022 , G05D1/0033 , G05D1/101 , B64C2201/10 , B64C2201/20
Abstract: A flying device includes a flight unit; and a flight control unit that performs, in a case where a flight position by the flight unit is out of a predetermined range, a control that is different from a control in a case where the flight position is within the predetermined range.
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公开(公告)号：US20180321691A1
公开(公告)日：2018-11-08
申请号：US15906274
申请日：2018-02-27
Applicant: QFO Labs, Inc.
Inventor： Brad Pedersen , Peter Spirov
IPC: G05D1/08 , B60V1/06 , G05D1/00 , B64D27/24 , B60V1/10 , B64C15/02 , B64C27/08 , B64C39/02 , B64C39/00 , B64C27/20
CPC classification number: G05D1/0816 , B60V1/06 , B60V1/10 , B64C15/02 , B64C27/08 , B64C27/20 , B64C39/001 , B64C39/024 , B64C2201/042 , B64C2201/10 , B64C2201/108 , B64C2201/146 , B64D27/24 , G05D1/0016 , G05D1/0022 , G05D1/0858
Abstract: A homeostatic flying hovercraft preferably utilizes at least two pairs of counter-rotating ducted fans to generate lift like a hovercraft and utilizes a homeostatic hover control system to create a flying craft that is easily controlled. The homeostatic hover control system provides true homeostasis of the craft with a true fly-by-wire flight control and control-by-wire system control.
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公开(公告)号：US09950790B2
公开(公告)日：2018-04-24
申请号：US14198418
申请日：2014-03-05
Applicant: AeroVironment, Inc.
Inventor： Matthew Todd Keennon , Karl Robert Klingebiel , Alexander Andryukov , Bart Dean Hibbs , John Peter Zwaan
CPC classification number: B64C33/025 , B64C19/00 , B64C33/02 , B64C2201/025 , B64C2201/10 , B64C2201/146
Abstract: Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
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Patent Agency Ranking
公开(公告)号：US20180079504A9
公开(公告)日：2018-03-22
申请号：US14198418
申请日：2014-03-05
Applicant: AeroVironment, Inc.
Inventor： Matthew Todd Keennon , Karl Robert Klingebiel , Alexander Andryukov , Bart Dean Hibbs , John Peter Zwaan
CPC classification number: B64C33/025 , B64C19/00 , B64C33/02 , B64C2201/025 , B64C2201/10 , B64C2201/146
Abstract: Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
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公开(公告)号：US09904292B2
公开(公告)日：2018-02-27
申请号：US14791253
申请日：2015-07-03
Applicant: QFO Labs, Inc.
Inventor： Brad Pedersen , Peter Spirov
IPC: G05D1/08 , B60V1/06 , B60V1/10 , B64C27/20 , B64C39/00 , B64C39/02 , G05D1/00 , B64C15/02 , B64C27/08 , B64D27/24
CPC classification number: G05D1/0816 , B60V1/06 , B60V1/10 , B64C15/02 , B64C27/08 , B64C27/20 , B64C39/001 , B64C39/024 , B64C2201/042 , B64C2201/10 , B64C2201/108 , B64C2201/146 , B64D27/24 , G05D1/0016 , G05D1/0022 , G05D1/0858
Abstract: A homeostatic flying hovercraft preferably utilizes at least two pairs of counter-rotating ducted fans to generate lift like a hovercraft and utilizes a homeostatic hover control system to create a flying craft that is easily controlled. The homeostatic hover control system provides true homeostasis of the craft with a true fly-by-wire flight control and control-by-wire system control.
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公开(公告)号：US09688397B2
公开(公告)日：2017-06-27
申请号：US15204547
申请日：2016-07-07
Applicant: Frick A. Smith
Inventor： Frick A. Smith
IPC: B64D35/04 , B64D27/02 , B64C27/22 , B64C29/00 , B64C1/14 , B64C27/52 , B64C39/02 , B64D17/24 , B64D17/34 , B64D17/62 , B64D17/80 , B64D31/00 , B64C27/26 , B64C27/28 , B64C27/82 , B64D17/64
CPC classification number: B64C29/0033 , B64C1/1415 , B64C1/1476 , B64C27/22 , B64C27/26 , B64C27/28 , B64C27/52 , B64C27/82 , B64C29/00 , B64C29/0016 , B64C39/02 , B64C39/024 , B64C2201/04 , B64C2201/088 , B64C2201/10 , B64C2201/104 , B64C2201/108 , B64C2201/162 , B64D17/24 , B64D17/34 , B64D17/62 , B64D17/64 , B64D17/80 , B64D27/02 , B64D31/00 , B64D35/04
Abstract: An aircraft may have a fuselage, a left wing extending from the fuselage, a right wing extending from the fuselage, a tail section extending from a rear portion of the fuselage, and a first engine and a second engine operably connected by a common driveshaft, wherein the first and second engines are configured for freewheeling such that if one of the first and second engines loses power the other of the first and second engines continues to power the aircraft.
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公开(公告)号：US20160251760A1
公开(公告)日：2016-09-01
申请号：US14903898
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Glenn Levasseur , Joseph Parkos , Grant O. Cook , Charles R. Watson
CPC classification number: C25D5/56 , B05D5/00 , B05D7/02 , B22C7/023 , B22C9/043 , B22C9/10 , B28B1/24 , B28B7/342 , B28B11/04 , B28B11/243 , B32B3/263 , B32B7/12 , B32B15/04 , B32B15/08 , B32B15/20 , B32B37/12 , B32B37/1284 , B32B37/14 , B32B2255/10 , B32B2307/202 , B32B2307/554 , B32B2603/00 , B33Y10/00 , B33Y80/00 , B62D35/00 , B64C39/024 , B64C39/028 , B64C2201/10 , C04B35/76 , C04B35/806 , C09D5/26 , C23C14/20 , C23C16/06 , C23C18/1633 , C23C18/165 , C23C18/2013 , C23C18/22 , C23C18/31 , C23C26/00 , C23C28/02 , C25D3/02 , C25D3/38 , C25D3/46 , C25D5/48 , C25D9/04 , C25D11/20 , F01D5/00 , F01D5/147 , F01D5/187 , F01D5/284 , F01D5/288 , F01D9/02 , F01D9/041 , F01D11/08 , F01D25/005 , F04D29/023 , F04D29/324 , F04D29/542 , F05D2220/32 , F05D2230/10 , F05D2230/22 , F05D2230/30 , F05D2230/312 , F05D2230/314 , F05D2240/122 , F05D2240/304 , F05D2300/10 , F05D2300/11 , F05D2300/121 , F05D2300/132 , F05D2300/133 , F05D2300/1616 , F05D2300/171 , F05D2300/177 , F05D2300/20 , F05D2300/30 , F05D2300/44 , F05D2300/501 , F05D2300/603 , F05D2300/611 , F05D2300/614 , F42B10/02
Abstract: A vented plated polymer component is disclosed. The vented plated polymer component may comprise a polymer substrate, a metal plating deposited on a surface of the polymer substrate, and at least one vent formed through the metal plating. The at least one vent may extend from an outer surface of the metal plating to the surface of the polymer substrate, and it may be sized to allow an escape of a gas from the polymer substrate to an external environment surrounding the plated polymer component.
Abstract translation: 公开了一种通风的镀覆聚合物组分。 排气的镀覆聚合物组分可以包括聚合物基材，沉积在聚合物基材的表面上的金属电镀，以及通过金属镀层形成的至少一个通风口。 所述至少一个通气孔可以从金属镀层的外表面延伸到聚合物基底的表面，并且其尺寸可被设定为允许气体从聚合物基底逸出到围绕镀覆的聚合物组分的外部环境。
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公开(公告)号：US20140367509A1
公开(公告)日：2014-12-18
申请号：US14251850
申请日：2014-04-14
Applicant: Frick A. Smith
Inventor： Frick A. Smith
IPC: B64C27/22 , B64C29/00 , B64C27/52 , B64C39/02 , B64D17/34 , B64C1/14 , B64D17/80 , B64D17/62 , B64D17/24 , B64D27/02 , B64D31/00
CPC classification number: B64C29/0033 , B64C1/1415 , B64C1/1476 , B64C27/22 , B64C27/26 , B64C27/28 , B64C27/52 , B64C27/82 , B64C29/00 , B64C29/0016 , B64C39/02 , B64C39/024 , B64C2201/04 , B64C2201/088 , B64C2201/10 , B64C2201/104 , B64C2201/108 , B64C2201/162 , B64D17/24 , B64D17/34 , B64D17/62 , B64D17/64 , B64D17/80 , B64D27/02 , B64D31/00 , B64D35/04
Abstract: An aircraft may have a fuselage, a left wing extending from the fuselage, a right wing extending from the fuselage, a tail section extending from a rear portion of the fuselage, and a first engine and a second engine operably connected by a common driveshaft, wherein the first and second engines are configured for freewheeling such that if one of the first and second engines loses power the other of the first and second engines continues to power the aircraft.
Abstract translation: 飞机可以具有机身，从机身延伸的左翼，从机身延伸的右翼，从机身的后部延伸的尾部，以及通过共同的驱动轴可操作地连接的第一发动机和第二发动机， 其中所述第一和第二发动机被配置为自由转动，使得如果所述第一和第二发动机中的一个发动机失去动力，则所述第一和第二发动机中的另一个继续为所述飞行器供电。
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