Propellant force generator

Patent metadata

Field	Value
Publication number	US-11718387-B2
Application number	US-202117606791-A
Country	US
Kind code	B2
Filing date	Mar 17, 2021
Priority date	Mar 17, 2020
Publication date	Aug 8, 2023
Grant date	Aug 8, 2023

Abstract

A propellant force generator is provided having the size in the axial direction of a rotational shaft of a motor reduced while making the pitch angles of rotational blades driven by the motor variable. The propellant force generator includes a propellant-force generating motor adapted to generate a propellant force for rotational blades, a pitch varying motor adapted to generate a rotational motion for changing pitch angles of the rotational blades, a rotation-linear motion converting unit adapted to convert the rotational motion generated by the pitch varying motor into a linear motion, and a linear motion-rotation converting unit adapted to convert the linear motions converted by the rotation-linear motion converting unit into rotational motions. At least a part of the linear motion-rotation converting unit is located within the propellant-force generating motor.

First claim

The invention claimed is:

1. A propellant force generator comprising:
a first motor adapted to generate a propellant force for rotational blades;
a second motor adapted to generate a rotational motion for changing pitch angles of the rotational blades;
a first converting unit adapted to convert the rotational motion generated by the second motor into a linear motion; and
a second converting unit adapted to convert the linear motion converted by the first converting unit into rotational motions, wherein the second converting unit comprises:
a linear mover comprising N surfaces corresponding to N rotational blades, N being a positive integer, the linear mover moving linearly in accordance with the linear motion converted by the first converting unit; and
N racks and N pinions corresponding to the N rotational blades,
wherein the N racks of the N racks and N pinions are supported by the N surfaces, respectively, and
the N pinions of the N racks and N pinions are supported on sides of support shafts for the N rotational blades, respectively.

2. A propellant force generator comprising:
a first motor adapted to generate a propellant force for rotational blades;
a second motor adapted to generate a rotational motion for changing pitch angles of the rotational blades;
a first converting unit adapted to convert the rotational motion generated by the second motor into a linear motion; and
a second converting unit adapted to convert the linear motion converted by the first converting unit into rotational motions,
wherein the first converting unit comprises a ball screw, and
wherein the first motor comprises a stator and a rotor, the ball screw comprising a ball screw shaft and a ball screw nut, the ball screw shaft being rotatably supported by a stationary member of the first motor, the ball screw nut being screwed to the ball screw shaft via balls and being guided to move linearly along the rotational axis.

3. The propellant force generator according to claim 2 , further comprising a linear motion transmission shaft adapted to transmit the linear motion converted by the first converting unit to the second converting unit, the linear motion transmission shaft being fixed to the ball screw nut of the ball screw, the linear motion transmission shaft comprising a surface adapted to restrict motion of the linear motion transmission shaft to a linear motion along a direction of the linear motion.

4. A propellant force generator comprising:
a first motor adapted to generate a propellant force for rotational blades;
a second motor adapted to generate a rotational motion for changing pitch angles of the rotational blades;
a first converting unit adapted to convert the rotational motion generated by the second motor into a linear motion; and
a second converting unit adapted to convert the linear motion converted by the first converting unit into rotational motions,
wherein the first motor comprises a stator and a rotor disposed inside the stator, and wherein at least a part of the first converting unit is located within the rotor of the first motor.

5. The propellant force generator according to claim 4 , wherein the rotor is fixed to a rotational shaft having a hollow section extending along an axial direction of the rotational shaft, and the part of the first converting unit that is located within the first motor is located within the hollow section.

6. The propellant force generator according to claim 5 , wherein the second motor is fixed to a part that is fixed to the stator.

7. The propellant force generator according to claim 4 , wherein the second motor is fixed to a part that is fixed to the stator.

Assignees

• Nsk Ltd

Inventors

• KUMAGAI Hiroyasu
• Gunji Daisuke

Classifications

• B64D27/34

  All-electric aircraft · CPC title

• B64C11/44 Primary

  electric · CPC title

• B64C27/605 Primary

  including swash plate, spider or cam mechanisms · CPC title

• B64U30/00

  Means for producing lift; Empennages; Arrangements thereof · CPC title

• Y02T50/40

  Weight reduction · CPC title