专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US12030626B2 Vertical take-off and landing (VTOL) aircraft 有权
公开(公告)号：US12030626B2
公开(公告)日：2024-07-09
申请号：US17441007
申请日：2020-03-19
申请人： AMSL INNOVATIONS PTY LTD
发明人： Andrew Dudley Moore , John Wilson
IPC分类号： B64C29/00 , B64C9/18 , B64C9/24 , B64C13/28 , B64C13/50 , B64C35/00 , B64C39/06 , B64D27/24
CPC分类号： B64C29/0033 , B64C9/18 , B64C9/24 , B64C13/28 , B64C13/50 , B64C35/001 , B64C39/068 , B64D27/24 , B64C2211/00
摘要： A vertical take-off and landing (VTOL) aircraft (100) having: a wing structure having right and left side forward wings (20, 22); and right and left side rearward wings (30, 32), each of the right side wings (20, 30) being connected, and each of the left side wings (22, 32) being connected in a box wing configuration; wherein each wing (20, 22, 30, 32) has a fixed leading edge (100) and at least one moveable trailing control surface (110), further wherein each wing (20, 22, 30, 32) has at least one motor pod (195), the motor pod (195) being pivotally mounted to an underside of the fixed leading edge (100), and fixedly secured to the trailing control surface (110).

2. 发明授权

US11919652B2 Vertical take-off and landing aircraft with deployable rotors 有权
公开(公告)号：US11919652B2
公开(公告)日：2024-03-05
申请号：US18097497
申请日：2023-01-17
申请人： JOBY AERO, INC.
发明人： JoeBen Bevirt , Alex Stoll
IPC分类号： B64D27/24 , B64C11/28 , B64C29/00 , B64C39/06
CPC分类号： B64D27/24 , B64C11/28 , B64C29/0033 , B64C39/068 , Y02T50/60
摘要： An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle may have deployment mechanisms which deploy electric motor driven propellers from a forward facing to a vertical orientation. The deployment mechanisms deploy the rotor forward and up as they deploy from a forward flight configuration to a vertical thrust configuration.

3. 发明授权

US11780572B2 VTOL aircraft using fixed forward canted rotors to simulate rigid wing dynamics 有权
公开(公告)号：US11780572B2
公开(公告)日：2023-10-10
申请号：US17389131
申请日：2021-07-29
申请人： Joby Aero, Inc.
发明人： Gregor Veble Mikic , JoeBen Bevirt , Alex Stoll
IPC分类号： B64C27/26 , B64C3/32 , B64C27/22 , B64C29/00 , B64C3/10 , B64C27/08 , B64C27/52 , B64C39/06 , B64C27/82
CPC分类号： B64C27/26 , B64C3/10 , B64C3/32 , B64C27/08 , B64C27/22 , B64C27/52 , B64C29/0016 , B64C39/06 , B64C39/068 , B64C2027/8236
摘要： A method for the flying of a vertical take-off and landing aircraft which uses fixed rotors for both VTOL and forward flight operations. The rotors form a synthetic wing and are positioned to achieve a high span efficiency. The rotors are positioned to even out the lift across the span of the synthetic wing. The synthetic wing may also have narrow front and rear airfoils which may provide structural support as well as providing lift during forward flight, or may have a single center wing. The wing rotors are tilted forward and provide some forward propulsion during horizontal flight.

4. 发明授权

US11708158B2 Aircraft with right and left propulsion unit support beams extending between main and aft wings 有权
公开(公告)号：US11708158B2
公开(公告)日：2023-07-25
申请号：US16887071
申请日：2020-05-29
申请人： Volocopter GmbH
发明人： Sebastian Mores , Tobias Vermeulen , Ulrich Schaferlein
IPC分类号： B64C11/46 , B64C29/00 , B64C5/06 , B64C39/06 , B64C39/08 , B64D27/24
CPC分类号： B64C29/0025 , B64C5/06 , B64C11/46 , B64C39/068 , B64C39/08 , B64D27/24
摘要： A VTOL aircraft (1), including: a fuselage (2) for transporting passengers and/or load; a front wing (3) attached to the fuselage (2); an aft wing (4) attached to the fuselage (2), behind the front wing (3) in a direction of forward flight (FF); a right connecting beam (5a) and a left connecting beam (5b), which connecting beams (5a, 5b) structurally connect the front wing (3) and the aft wing (4), which connecting beams (5a, 5b) are spaced apart from the fuselage (2); and at least two propulsion units (6) on each one of the connecting beams (5a, 5b). The propulsion units (6) include at least one propeller (6b, 6b′) and at least one motor (6a) driving the propeller (6b, 6b′), preferably an electric motor, and are arranged with their respective propeller axis in an essentially vertical orientation (z).

5. 发明申请

US20180065722A1 TRACTION AIR DEVICE, AIR DEVICE FOR A WIND PLANT AND WIND PLANT FOR ELECTRIC POWER PRODUCTION, SHIP PROVIDED WITH A TRACTION AIR DEVICE 审中-公开
公开(公告)号：US20180065722A1
公开(公告)日：2018-03-08
申请号：US15558895
申请日：2016-03-17
申请人： SKYPULL SAGL
发明人： Aldo CATTANO
IPC分类号： B63H9/06 , B64C9/20 , B64C3/16 , F03D5/00 , B64C9/18 , F03D5/06 , F03D5/04
CPC分类号： B63H9/0685 , B63B2035/446 , B63H2009/0692 , B64C3/16 , B64C9/18 , B64C9/20 , B64C31/06 , B64C39/022 , B64C39/068 , F03D5/005 , F03D5/04 , F03D5/06 , F05B2240/917 , F05B2240/921 , F05B2240/931 , F05B2240/94 , F05B2250/12 , F05B2250/121 , Y02E10/70 , Y02E10/728
摘要： Traction air device with multiple wing contours for a wind power generation plant and wind power generation plant utilizing the air device.

6. 发明授权

US09567062B2 Box wing with angled gas turbine engine cores 有权
标题翻译：带有倾斜式燃气涡轮发动机内核的机翼
公开(公告)号：US09567062B2
公开(公告)日：2017-02-14
申请号：US14440895
申请日：2013-03-14
申请人： United Technologies Corporation
发明人： Jesse M. Chandler , Gabriel L. Suciu
IPC分类号： B64D27/14 , B64C39/06 , B64D33/04 , B64C3/14 , B64C39/12 , B64C39/10 , B64C5/06 , F02K1/56 , F02K1/78
CPC分类号： B64C3/14 , B64C5/06 , B64C39/068 , B64C39/10 , B64C39/12 , B64D27/14 , B64D33/04 , F02K1/56 , F02K1/78
摘要： An aircraft including a fuselage having a forward portion and an aft portion with a propulsion system mounted within the aft portion of the fuselage. A burst zone is defined that extends outward from the propulsion system. The aircraft includes a box wing extending from the aft portion of the fuselage to a forward portion of the fuselage that is disposed outside of the burst zone.
摘要翻译：一种飞机，包括具有前部和后部的机身，其具有安装在机身后部的推进系统。定义了从推进系统向外延伸的爆破区域。飞机包括从机身的后部延伸到设置在爆破区域外部的机身的前部的箱翼。

7. 发明授权

US09321526B2 Compound helicopter 有权
标题翻译：复合直升机
公开(公告)号：US09321526B2
公开(公告)日：2016-04-26
申请号：US13950570
申请日：2013-07-25
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GMBH
发明人： Axel Fink , Ambrosius Weiss , Andrew Winkworth
IPC分类号： B64C27/26 , B64C39/06
CPC分类号： B64C27/26 , B64C39/068
摘要： The invention relates to a compound helicopter comprising a fuselage, at least one engine and a main rotor driven by said at least one engine. At least one pair of fixed wings are mounted in an essentially horizontal plane on a left hand and a right hand side of the fuselage and horizontally oriented propulsion devices are mounted to each of the fixed wings, the fixed wings encompassing each a drive shaft from the at least one engine. Each fixed wing comprises a lower main wing and an upper secondary wing being connected to each other within an interconnection region. The propulsion devices include pusher propellers arranged at the interconnection region and the upper secondary wing houses the drive shaft from the at least one engine.
摘要翻译：本发明涉及复合直升机，其包括机身，至少一个发动机和由所述至少一个发动机驱动的主转子。至少一对固定翼安装在机身的左手和右手侧的基本水平的平面中，并且水平定向的推进装置安装到每个固定翼上，固定翼包括各自的驱动轴至少一台发动机。每个固定翼包括在主互连区域内彼此连接的下主翼和上副翼。推进装置包括布置在互连区域处的推进器螺旋桨，并且上部副翼翼从至少一个发动机容纳驱动轴。

8. 发明授权

US09308984B2 Flying device and a wing construction for the same 有权
标题翻译：飞行装置和翼结构相同
公开(公告)号：US09308984B2
公开(公告)日：2016-04-12
申请号：US14006754
申请日：2012-03-19
申请人： Aki Suokas
发明人： Aki Suokas
IPC分类号： B64C1/26 , B64C3/56 , B64C31/028 , B64C39/06
CPC分类号： B64C1/26 , B64C3/56 , B64C31/028 , B64C39/068
摘要： Flying device, in which there is a fuselage (2, 2′), wings (8, 9), which are connected to each other to form an essentially looped structure, elements (4, 5) for creating a flying force, and the desired elements (e.g., 7, 7′) for controlling the flying device (1). The wings (8, 9) of the flying device (1) form a unified totality detachable from the fuselage (2, 2′). A wing construction is also included.
摘要翻译：具有彼此连接以形成基本环形结构的机身（2,2'），机翼（8,9）的飞行装置，用于产生飞行力的元件（4,5），以及用于控制飞行装置（1）的所需元件（例如，7,7'）。飞行装置（1）的翼（8,9）形成从机身（2,2'）可拆卸的统一的总体。还包括机翼结构。

9. 发明申请

US20160031555A1 AERODYNAMICALLY EFFICIENT LIGHTWEIGHT VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH PIVOTING ROTORS AND STOWING ROTOR BLADES 审中-公开
公开(公告)号：US20160031555A1
公开(公告)日：2016-02-04
申请号：US14660771
申请日：2015-03-17
申请人： JOBY AVIATION, INC.
发明人： JOEBEN BEVIRT , ALEX STOLL
IPC分类号： B64C27/28 , B64C29/00
CPC分类号： B64C27/28 , B64C11/28 , B64C27/08 , B64C27/30 , B64C29/0008 , B64C29/0033 , B64C39/068
摘要： An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes.

10. 发明授权

US07100867B2 Lifting foil 有权
标题翻译：起重箔
公开(公告)号：US07100867B2
公开(公告)日：2006-09-05
申请号：US10774865
申请日：2004-02-09
申请人： Ronald G. Houck, II
发明人： Ronald G. Houck, II
IPC分类号： B64C39/08
CPC分类号： B64C39/068 , B63B1/248 , B64C3/16 , B64C39/066 , Y02T50/12
摘要： A lifting foil for an aircraft, a hydrofoil or the like having a pair of courses or wings. Vortex losses due to spanwise fluid flow are substantially reduced by joining the tips of the courses with flow guides configured for jointly terminating the undesired flows. Termination is effected by providing the flow guides with crossections cambered for reducing the dynamic pressure of fluid flowing in a spanwise direction across flow guide surfaces.
摘要翻译：用于具有一对路线或翼的飞机，水翼等的提升箔。通过将流程的末端连接到配置成共同终止不期望的流的流动引导件，由于翼展向流体流动引起的涡流损失大大降低。通过为流动引导器提供横截面来实现终止，所述横截面用于减小横跨流动导向表面沿翼展方向流动的流体的动态压力。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式