IP Library Granted Patent US 11,913,470
Granted Patent B2
US 11,913,470 · App. 16/754,064 · Granted Feb 27, 2024

Ducted fan, multicopter, vertical take-off and landing aircraft, CPU-cooling fan, and radiator-cooling fan

Inventor: Masashi Harada (Tokyo, JP)
Assignee: JAPAN AEROSPACE EXPLORATION AGENCY
F04D29/403B64C11/18B64C29/00F04D19/002F04D29/384
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Quick Facts
Patent No.
US 11,913,470
App. No.
16/754,064
Granted
Feb 27, 2024
Kind
B2
Abstract

[Object] To maximize static thrust of a ducted fan. [Solving Means] This ducted fan 1 includes a duct 10 , a fan 20 , a motor 30 , a housing 40 , and stators 50 . The fan 20 includes a hub 21 disposed concentric with the duct 10 and four blades 22 arranged at equal intervals on the outer circumference of the hub 21 . A chord length CL of the blade 22 gradually decreases toward a tip 22 A from the root. In contrast, the chord length CL of the blade 22 increases to the tip 21 B from a tip vicinity portion 22 B.

Claims (21)

1. A ducted fan, comprising:

a duct including a round-shaped lip; and

a propeller including a blade comprising a root and a tip opposite from the root, wherein the tip is adjacent to an inner wall of the duct, wherein a chord length of the blade gradually decreases from the root toward the tip until a tip vicinity portion and then increases from the tip vicinity portion to the tip such that: an axial velocity of flow in the duct increases from the root of the blade as it gets closer to the tip of the blade; and the axial velocity of flow is largest at the tip of the blade,

wherein a position of the tip vicinity portion at which the chord length increases is within a distance equivalent to 15% of a radius of the blade from the tip.

2. The ducted fan according to claim 1 , wherein

assuming that the chord length of the tip of the blade is denoted by CL A and the chord length of the tip vicinity portion of the blade is denoted by CLB B , the following expression is established

1.0×CL B <CL A ≤1.3×CL B .

3. The ducted fan according to claim 1 , wherein

a rate of gradual decrease of the chord length of the blade lowers toward the tip.

4. The ducted fan according to claim 1 , wherein

a ratio of a maximum chord length to a minimum chord length of the blade is 1.5 or more and 3.0 or less.

5. The ducted fan according to claim 1 , wherein

assuming that an inner diameter of the duct is denoted by R, the lip has a round shape having a radius of curvature r as follows

3/100× R≤r≤ 30/100× R.

6. The ducted fan according to claim 1 , wherein

the duct has a length longer than a length equivalent to 25% of the inner diameter of the duct.

7. The ducted fan according to claim 1 , wherein

the fan includes a hub that retains the blade, and

the hub has a diameter equivalent to 10% or more and 50% or less of the inner diameter of the duct.

8. The ducted fan according to claim 7 , wherein

the hub retains two to eight blades each being the blade.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 29, 2020
From: HARADA, MASASHI
To: JAPAN AEROSPACE EXPLORATION AGENCY
Reel/Frame 052520/0879 →
Priority Claims (1)
JP 2017-194779 · Oct 5, 2017 · national
Continuity (1)
Related Publication 20200325910A1 · Oct 15, 2020