Propulsion device

Patent metadata

Field	Value
Publication number	US-11691743-B2
Application number	US-202217568106-A
Country	US
Kind code	B2
Filing date	Jan 4, 2022
Priority date	Jan 8, 2021
Publication date	Jul 4, 2023
Grant date	Jul 4, 2023

Abstract

A propulsion device includes: a duct in which a flow path extending in a direction of an axis; a fan which is provided with a) an outer peripheral ring formed in an annular shape surrounding the axis and installed to be relatively rotatable around the axis with respect to the duct, b) a plurality of fan blades arranged at intervals in a circumferential direction such that each blade is extended from the outer peripheral ring toward the inside of the flow path, and c) an inner peripheral ring formed in an annular shape being connected radially inner end portions of the plurality of fan blades and in which an air flow passage is formed so that air flows therethrough in the direction of the axis; and a motor which drives the fan to rotate around the axis.

First claim

What is claimed is:

1. A propulsion device comprising:
a duct in which a flow path extending in a direction of an axis is formed;
a fan which is provided with
a) an outer peripheral ring formed in an annular shape surrounding the axis and installed to be relatively rotatable around the axis with respect to the duct,
b) a plurality of fan blades arranged at intervals in a circumferential direction such that each blade is extended from the outer peripheral ring toward an inside of the flow path, and
c) an inner peripheral ring formed in an annular shape and to which inner end portions of the plurality of fan blades are connected, wherein an air flow passage is formed inside the inner peripheral ring so that air flows therethrough in the direction of the axis;
a motor which is configured to drive the fan to rotate around the axis; and
an outer bearing supporting the outer peripheral ring to be rotatable with respect to the duct,
wherein the outer bearing includes a housing which is provided on the duct and covering the outer peripheral ring, and a compressor which is allowed to introduce compressed air to the housing,
the motor includes a rotor core which is provided on an outer peripheral surface of the outer peripheral ring, and a stator core which is provided on the housing so as to face the rotor core,
the fan is rotatably supported by only the outer bearing, and
wherein an air bearing is formed between the outer peripheral ring and the housing as the outer bearing by introducing the compressed air from the compressor to a gap between the rotor core and the stator core inside the housing.

2. The propulsion device according to claim 1 ,
wherein the air flow passage has a circular cross-sectional shape when viewed from a first side in the direction of the axis.

3. The propulsion device according to claim 2 ,
wherein an inner diameter of the air flow passage is constant from the first side toward a second side in the direction of the axis.

Assignees

• Mitsubishi Heavy Ind Ltd

Inventors

• Karikomi Kai
• Morisaki Yuki
• Hosono Kazuki
• Iwatani Junji

Classifications

• B64D35/02

  specially adapted for specific power plants · CPC title

• B64D27/31

  within, or attached to, wings · CPC title

• B64D27/33

  Hybrid electric aircraft · CPC title

• B64C11/001 Primary

  Shrouded propellers · CPC title

• F04D25/06

  the pump being electrically driven (F04D25/08 takes precedence) · CPC title