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公开(公告)号：US20170029131A1
公开(公告)日：2017-02-02
申请号：US15220624
申请日：2016-07-27
Applicant: Airbus Defence and Space GmbH
Inventor： Jürgen Steinwandel , Ning Wang , Michael Judas , Jan Van Toor
CPC classification number: B64D35/08 , B64C29/0025 , B64C39/024 , B64C2201/042 , B64C2201/044 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/162 , B64D27/24 , B64D2027/026
Abstract: A vertical take-off aircraft with a propulsion drive for generating a driving force being effective in a horizontal direction and with a lift drive for generating a lifting force being effective in a vertical direction includes a motor for providing mechanical energy for the propulsion drive and a first generator for providing electrical energy for the lift drive. Moreover, the aircraft includes an exhaust gas turbocharger for the motor with a first turbine being driven by an exhaust gas flow of the motor, wherein the first turbine is configured to provide mechanical energy for the propulsion drive.
Abstract translation: 具有用于产生在水平方向上有效的驱动力的推进驱动器的垂直起飞飞机和用于产生在垂直方向上有效的提升力的提升驱动装置包括用于为推进驱动提供机械能的马达和 第一发电机，用于为升降机驱动提供电能。 此外，飞行器包括用于电动机的排气涡轮增压器，其中第一涡轮机由电动机的废气流驱动，其中第一涡轮机构造成为推进驱动提供机械能。
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公开(公告)号：US10435169B2
公开(公告)日：2019-10-08
申请号：US15220624
申请日：2016-07-27
Applicant: Airbus Defence and Space GmbH
Inventor： Jürgen Steinwandel , Ning Wang , Michael Judas , Jan Van Toor
Abstract: A vertical take-off aircraft with a propulsion drive for generating a driving force being effective in a horizontal direction and with a lift drive for generating a lifting force being effective in a vertical direction includes a motor for providing mechanical energy for the propulsion drive and a first generator for providing electrical energy for the lift drive. Moreover, the aircraft includes an exhaust gas turbocharger for the motor with a first turbine being driven by an exhaust gas flow of the motor, wherein the first turbine is configured to provide mechanical energy for the propulsion drive.
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公开(公告)号：US10131426B2
公开(公告)日：2018-11-20
申请号：US14915101
申请日：2014-08-29
Applicant: Airbus Defence and Space GmbH
Inventor： Michael Judas , Friederike Stratenberg , Jan Van Toor , Werner Scholz , Berthold Karrais , Wolfgang Stangl
IPC: B64C27/08 , B64C29/00 , B64C3/38 , B64C5/08 , B64C27/473 , B64C39/02 , B64C39/08 , B64D27/02 , B64D27/24
Abstract: The invention relates to an aircraft which can both take off and land vertically and can hover and also fly horizontally at a high cruising speed. The aircraft has a support structure, a wing structure, at least three and preferably at least four lifting rotors and at least one thrust drive. The wing structure is designed to generate a lifting force for the aircraft during horizontal motion. To achieve this the wing structure has at least one mainplane provided with a profile that generates dynamic lift. The wing structure is preferably designed as a tandem wing structure. Each of the lifting rotors is fixed to the support structure, has a propeller and is designed to generate a lifting force for the aircraft by means of a rotation of the propeller, said force acting in a vertical direction. The thrust drive is designed to generate a thrust force on the support structure, said force acting in a horizontal direction. The lifting rotors can have a simple construction, i.e. they can have a simple rigid propeller for example, and a vertical take-off or hovering of the aircraft can be controlled, in a similar manner to quadcopters, by a simple control of the speeds of the lifting rotors. High cruising speeds can be achieved as a result of the additional horizontally acting thrust drive.
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公开(公告)号：US10371066B2
公开(公告)日：2019-08-06
申请号：US15953209
申请日：2018-04-13
Applicant: Airbus Defence and Space GmbH
Inventor： Juergen Steinwandel , Florian Stagliano , Jan Van Toor
Abstract: An unmanned aircraft includes a propulsion system having a diesel or kerosene internal combustion engine and a charger device for engine charging. The propulsion system can be a hybrid propulsion system or a parallel hybrid propulsion system.
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