IP Library Granted Patent US 12,600,460
Granted Patent B2
US 12,600,460 · App. 19/183,289 · Granted Apr 14, 2026

Propeller

Inventors: Tatsuki Kitada (Neyagawa, JP); Mitsuru Kuwahata (Neyagawa, JP); Masahiro Ohno (Neyagawa, JP); Yasunori Kunisaki (Neyagawa, JP)
Assignee: EXEDY CORPORATION
B64C11/28B64C11/04B64C27/50B64U30/293
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,600,460
App. No.
19/183,289
Granted
Apr 14, 2026
Kind
B2
Abstract

A propeller designed to prevent unintentional folding of the blades includes a hub, a blade, a first engaging portion, and a second engaging portion. The blade is attached to the hub to be radially movable with respect thereto. The blade is attached to the hub to be pivotable with respect thereto. The first engaging portion is provided in the hub. The second engaging portion is provided in the blade. The second engaging portion is configured to be engaged with the first engaging portion to restrict the blade from pivoting with respect to the hub when the blade is moved radially outward. The second engaging portion is configured to be disengaged from the first engaging portion when the blade is moved radially inward.

Claims (36)

1 . A propeller, comprising:

a hub;

a blade attached to the hub to be pivotable and radially movable with respect thereto;

a first engaging portion provided in the hub; and

a second engaging portion provided in the blade, the second engaging portion configured to be engaged with the first engaging portion to restrict the blade from pivoting with respect to the hub when the blade is moved radially outward, when engaged with the first engaging portion, the second engaging portion configured to overlap the first engaging portion when viewed in an axial direction, the second engaging portion configured to be disengaged from the first engaging portion when the blade is moved radially inward, when disengaged with the first engaging portion, the second engaging portion configured not to overlap the first engaging portion when viewed in the axial direction.

2 . The propeller according to claim 1 , wherein the hub includes an upper hub portion disposed on an upper side of the blade.

3 . The propeller according to claim 2 , wherein the first engaging portion is provided in the upper hub portion.

4 . The propeller according to claim 2 , wherein the hub includes a lower hub portion disposed on a lower side of the blade.

5 . The propeller according to claim 1 , wherein

the first engaging portion is provided in the hub as one of a recess and a protrusion, and

the second engaging portion is provided in the blade as the other of the recess and the protrusion.

6 . The propeller according to claim 5 , wherein

the protrusion extends in the axial direction, and

the recess is recessed in the axial direction.

7 . The propeller according to claim 5 , wherein

the recess includes a pair of inner wall surfaces opposed to each other, and

the pair of inner wall surfaces slant to gradually separate from each other toward the protrusion.

8 . The propeller according to claim 7 , wherein

the protrusion extends in the axial direction, and

the recess is recessed in the axial direction.

9 . The propeller according to claim 5 , wherein

the recess includes a pair of inner wall surfaces opposed to each other, and

the pair of inner wall surfaces are substantially parallel.

10 . The propeller according to claim 1 , further comprising:

a pivot shaft axially extending from one of the hub and the blade, wherein

the other of the hub and the blade includes an elongated hole radially extending, the elongated hole guiding the pivot shaft such that the pivot shaft is made radially movable.

11 . The propeller according to claim 10 , wherein

the elongated hole is a slot.

12 . The propeller according to claim 10 , wherein

the pivot shaft axially extends from the hub, and

the blade includes the elongated hole.

13 . The propeller according to claim 12 , wherein

the elongated hole is a slot.

14 . A rotorcraft comprising:

the propeller recited in claim 1 ; and

a prime mover configured to rotate the propeller.

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE CITY PREVIOUSLY RECORDED AT REEL: 70883 FRAME: 547. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Apr 21, 2025
From: KITADA, TATSUKI; KUWAHATA, MITSURU; OHNO, MASAHIRO; KUNISAKI, YASUNORI
To: EXEDY CORPORATION
Reel/Frame 070896/0570 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 18, 2025
From: KITADA, TATSUKI; KUWAHATA, MITSURU; OHNO, MASAHIRO; KUNISAKI, YASUNORI
To: EXEDY CORPORATION
Reel/Frame 070883/0547 →
Priority Claims (1)
JP 2024-071322 · Apr 25, 2024 · national
Continuity (1)
Related Publication 20250333160A1 · Oct 30, 2025
References Cited (5)
US 4252504A · Covington · 1981 [cited by examiner]
US 10689103B2 · Holik · 2020 [cited by examiner]
US 11541996B2 · Kim · 2023 [cited by examiner]
JP 2023184048A · 2023 [cited by applicant]
WO WO2018172754A1 · 2018 [cited by examiner]