公开(公告)号：US11661183B2

公开(公告)日：2023-05-30

申请号：US17203413

申请日：2021-03-16

Applicant: D. Anthony Windisch

Inventor： D. Anthony Windisch

IPC: F04D19/00 ,  B64C29/00 ,  B64C13/50 ,  F04D29/56

CPC classification number: B64C29/0066 ,  B64C13/503 ,  F04D19/007 ,  F04D29/563

Abstract: An aircraft having a frame assembly that supports a compressor having an outer shell that defines front and rear nozzle ports with rotatable nozzles for selectable vertical or horizontal thrust. The inner shell and the outer shell define an intake gap therebetween such as an annulus. A first fan unit within the inner shell and is configured to exhaust air through the front nozzle ports. A second fan unit within the outer shell intakes air through the intake gap and exhausts air through the rear nozzle ports. The fan units are preferably connected to one another via a drive shaft that is surrounded by a streamlining tube. The fan units each include a plurality of fans having stators therebetween. The stators have a plurality of stator arms with a wing structure pivotally attached to the trailing edge for angling air flow from a front to a rear fan.

公开(公告)号：US08960592B1

公开(公告)日：2015-02-24

申请号：US13553080

申请日：2012-07-19

Applicant: D. Anthony Windisch

Inventor： D. Anthony Windisch

IPC: B64C29/00 ,  B64D35/00 ,  B64D33/02

CPC classification number: A63H27/06 ,  A63H30/04 ,  B64C29/0025 ,  B64C2201/162 ,  B64C2203/00 ,  B64D35/00

Abstract: An aircraft, such as a radio controlled aircraft, capable of vertical take-off and landing. The aircraft has a compressor in a fuselage that contains an interconnected first and second fans driven by a motor. An intake provides air to the first fan, while a bypass duct directs airflow to the second fan. Air flow from the first fan to the second fan is controlled by a valve, which is operated in tandem with doors in the bypass duct. Nozzles direct air flow out of the compressor in a selected one of a vertical or non-vertical direction for conventional flight or for hover. Hover tubes are provided to adjust the aircraft in pitch, yaw and roll. The hover tubes operate simultaneously with conventional flight controls.

Abstract translation: 飞机，如无线电控制的飞机，能够垂直起飞和着陆。 飞机在机身中具有压缩机，其包含由电动机驱动的互连的第一和第二风扇。 进气口向第一风扇提供空气，而旁路管道将气流引导到第二风扇。 从第一风扇到第二风扇的气流由与旁通管道中的门串并联操作的阀来控制。 喷嘴直接以常规飞行或悬停的垂直或非垂直方向中的一个方式从压缩机流出。 提供悬停管，以调整俯仰，偏航和滚动的飞机。 悬停管与常规飞行控制同时操作。

公开(公告)号：US5666803A

公开(公告)日：1997-09-16

申请号：US514827

申请日：1995-08-14

Applicant: D. Anthony Windisch

Inventor： D. Anthony Windisch

IPC: B64C29/00 ,  F02B75/34 ,  F02K1/00 ,  F02K3/02 ,  F02K5/00

CPC classification number: F02K5/00 ,  B64C29/0066 ,  F02B75/34 ,  F02K1/004 ,  F02K3/025

Abstract: A vectored thrust compressor for use in remote controlled aircraft comprising a housing having a forwardly facing air intake is disclosed. Two pair of vectorable thrust nozzles connect to the housing and project from opposite sides of the housing. A first pair is disposed at the forward end of the housing and a second pair is located at the aft end. Each thrust nozzle is adjustable such that the thrust nozzles are rotatable simultaneously by remote control. A first ducted-fan is located in the forward end of the housing and is connected to a drive shaft. A portion of the air flow generated by the first ducted-fan is diverted through the forward pair of thrust nozzles. A second ducted-fan is situated in the aft end of the housing, forward of the second pair of thrust nozzles, and is also connected to the drive shaft. The drive shaft may be turned by a conventional engine.

Abstract translation: 公开了一种用于遥控飞行器的向心推力压缩机，其包括具有朝前的朝向进气口的壳体。 两对可向导的推力喷嘴连接到壳体并从壳体的相对侧突出。 第一对设置在壳体的前端，第二对位于后端。 每个推力喷嘴是可调节的，使得推力喷嘴可以通过遥控同时旋转。 第一导风扇位于壳体的前端，并与驱动轴连接。 由第一管道风扇产生的空气流的一部分通过前进的一对推力喷嘴转向。 第二导风扇位于壳体的后端部，位于第二对推力喷嘴的前方，并且还连接到驱动轴。 驱动轴可以由常规发动机转动。