Ducted fan device and aircraft

Patent metadata

Field	Value
Publication number	US-12312077-B2
Application number	US-202218289177-A
Country	US
Kind code	B2
Filing date	Feb 14, 2022
Priority date	May 12, 2021
Publication date	May 27, 2025
Grant date	May 27, 2025

Abstract

A ducted fan device includes: a plurality of fan devices each having a fan configured to be rotated about a first axis to generate an airflow and a cylindrical smaller duct surrounding the fan about the first axis and extending in a first axis direction; and a cylindrical larger duct extending in a second axis direction parallel to the first axis. Each of the fan devices is arranged on an inner side of the larger duct when viewed in the second axis direction. At least a part of the smaller duct is arranged outside the larger duct on an upstream side in a flow direction of an airflow when viewed in a direction orthogonal to the second axis.

First claim

The invention claimed is:

1. A ducted fan device comprising:
fan devices each comprising:
a fan that rotates about a first axis and generates an airflow; and
a cylindrical smaller duct surrounding the fan about the first axis and extending in a first axis direction; and

a cylindrical larger duct extending in a second axis direction parallel to the first axis, wherein
each of the fan devices is disposed inside the larger duct when viewed in the second axis direction,
at least a part of the smaller duct is disposed outside the larger duct and upstream of the larger duct in a flow direction of the airflow when viewed in a direction orthogonal to the second axis direction, and
in the flow direction, a downstream end face of the smaller duct of each of the fan devices is disposed upstream with respect to an upstream end face of the larger duct.

2. The ducted fan device according to claim 1 , wherein a distance along the second axis direction between the downstream end face of the smaller duct of each of the fan devices and the upstream end face of the larger duct is greater than or equal to 0 H and less than or equal to 0.5 H, where H is a dimension of the smaller duct along the first axis.

3. A ducted fan device comprising:
fan devices each comprising:
a fan that rotates about a first axis and generates an airflow; and
a cylindrical smaller duct surrounding the fan about the first axis and extending in a first axis direction; and

a cylindrical larger duct extending in a second axis direction parallel to the first axis, wherein
each of the fan devices is disposed inside the larger duct when viewed in the second axis direction,
at least a part of the smaller duct is disposed outside the larger duct and upstream of the larger duct in a flow direction of the airflow when viewed in a direction orthogonal to the second axis direction,
in the flow direction, a downstream end face of the smaller duct of each of the fan devices is disposed downstream with respect to an upstream end face of the larger duct, and
in the flow direction, an upstream end face of the smaller duct of each of the fan devices is disposed upstream with respect to the upstream end face of the larger duct, and
a distance along the second axis direction between the downstream end face of the smaller duct of each of the fan devices and the upstream end face of the larger duct is greater than 0 H and less than or equal to 0.5 H, where H is a dimension of the smaller duct along the first axis.

4. The ducted fan device according to claim 1 , wherein the fan devices are disposed at equal angular intervals in a circumferential direction around an axis of the larger duct.

5. The ducted fan device according to claim 4 , wherein a length between the smaller duct of one of the fan devices and the smaller duct of an adjacent one of the fan devices in the circumferential direction is greater than or equal to 0.5 D and less than or equal to 1.5 D, where D is a diameter of the smaller duct.

6. The ducted fan device according to claim 1 , wherein each of the fan devices is driven separately by a corresponding electric motor.

7. An aircraft comprising the ducted fan device according to claim 1 .

8. The ducted fan device according to claim 3 , wherein the fan devices are disposed at equal angular intervals in a circumferential direction around an axis of the larger duct.

9. The ducted fan device according to claim 8 , wherein a length between the smaller duct of one of the fan devices and the smaller duct of an adjacent one of the fan devices in the circumferential direction is greater than or equal to 0.5 D and less than or equal to 1.5 D, where D is a diameter of the smaller duct.

10. The ducted fan device according to claim 3 , wherein each of the fan devices is driven separately by a corresponding electric motor.

11. An aircraft comprising the ducted fan device according to claim 3 .

Assignees

• Mitsubishi Heavy Ind Ltd

Inventors

• Morisaki Yuki
• Oda Masayuki
• Saiki Yasuhiro

Classifications

• B64C11/001

  Shrouded propellers · CPC title

• B64C29/00

  Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft (rotorcraft B64C27/00) · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• B64C29/0091 Primary

  Accessories not provided for elsewhere · CPC title

• B64D27/30 Primary

  Aircraft characterised by electric power plants · CPC title