System for protecting a rotatable shaft of a motor from excessive bending moments

Patent metadata

Field	Value
Publication number	US-11618549-B2
Application number	US-201916682965-A
Country	US
Kind code	B2
Filing date	Nov 13, 2019
Priority date	Aug 19, 2011
Publication date	Apr 4, 2023
Grant date	Apr 4, 2023

Abstract

A motor assembly that includes a motor having a motor casing, a rotatable shaft extending from said motor casing to a shaft length and a hub coupled to said rotatable shaft, the hub having a circumferential skid surface disposed immediately proximal to the motor casing and having a channel configured to seat a propeller, when a propeller is present, wherein a bending moment applied to the shaft through the hub results in the circumferential skid surface contacting said motor casing.

First claim

What is claimed is:

1. A method comprising:
applying a bending moment to a rotatable shaft extending from a motor, wherein the motor is attached to a first structure;
bending the rotatable shaft by the applied bending moment such that at least a portion of a surface of a second structure contacts at least a portion of the first structure, wherein the surface of the second structure is disposed adjacent to and apart from at least a portion of the first structure; and
applying a bending moment to a propeller coupled to the rotatable shaft, wherein the bending moment applied to the propeller is transmitted to the rotatable shaft.

2. The method of claim 1 further comprising:
receiving and seating the propeller by the second structure, wherein the second structure is a hub.

3. The method of claim 1 further comprising:
receiving the rotatable shaft by a cavity of the second structure, wherein the second structure is a hub which further comprises the cavity, and wherein the rotatable shaft has a threaded distal portion configured to threadably receive a spinner nut to hold the propeller to the hub.

4. The method of claim 2 , wherein the hub has a channel which is contoured to approximate a bottom surface of an airfoil.

5. The method of claim 1 further comprising:
receiving the rotatable shaft by a shaft cavity, wherein the shaft cavity extends approximately to a shaft length so that a circumferential skid surface is disposed immediately proximal to the first structure, and wherein the first structure is a motor casing.

6. The method of claim 1 , wherein the surface is at least one of: annular and non-annular.

7. The method of claim 1 further comprising:
transferring a load between at least the portion of the surface of the second structure and at least the portion of the first structure during contact.

8. The method of claim 1 , wherein the surface comprises opposing radial hub wings.

9. The method of claim 1 , wherein the first structure is a motor casing and the second structure is a hub, wherein the surface is a circumferential skid surface which is spaced apart from the motor casing by a gap distance, and wherein the gap distance enables the contact of the circumferential skid surface onto the motor casing prior to reaching a load limit of the rotatable shaft.

10. A method comprising:
applying a bending moment to a rotatable shaft extending past a skid face of a motor, wherein the motor is attached to a fixed structure; and
bending the rotatable shaft by the applied bending moment such that a skid surface of a rotatable structure contacts the skid face, wherein the skid surface of the rotatable structure is disposed adjacent to the skid face during at least a portion of a rotation of the rotatable shaft, and wherein the skid surface is defined by opposing radial hub wings.

11. The method of claim 10 , wherein the skid surface is annular.

12. The method of claim 10 , wherein the skid surface is spaced apart from the skid face by a gap distance, and wherein the gap distance enables the contact of the skid surface onto the skid face prior to reaching a load limit of the rotatable shaft.

13. The method of claim 10 further comprising:
limiting bending of the rotatable shaft by reinforcing contact between the rotatable structure and the fixed structure attached to the motor.

14. A method comprising:
applying a bending moment to a rotatable shaft, wherein a rotatable hub is coupled to the rotatable shaft, and wherein the rotatable hub has a skid surface;
bending the rotatable shaft by the applied bending moment such that the skid surface of the rotatable hub contacts a skid face of a motor for providing reinforcing contact, wherein the skid face of the motor is spaced immediately apart from an in complementary opposition to the skid surface of the rotatable hub; and
seating a propeller onto the rotatable shaft by a channel, wherein the channel for seating is configured so that a bending moment applied to the propeller is transmitted to the rotatable hub through the rotatable shaft and results in the skid surface contacting the skid face for providing reinforcing contact.

15. The method of claim 14 , wherein the skid surface is at least one of:
annular and non-annular.

16. The method of claim 15 , wherein the skid surface is defined by opposing radial hub wings.

17. The method of claim 14 , wherein the skid surface is spaced apart from the skid face by a gap distance, and wherein the gap distance enables the contact of the skid surface onto the skid face prior to reaching a load limit of the rotatable shaft.

Assignees

• Aerovironment Inc

Inventors

• Ghapgharan Emil
• Dalan Lane
• Belik Pavel
• Fisher Christopher Eugene
• Gunder Austin Craig

Classifications

• B64U50/19

  using electrically powered motors · CPC title

• H02K7/14

  Structural association with mechanical loads, e.g. with hand-held machine tools or fans (with fan or impeller for cooling the machine H02K9/06) · CPC title

• B64C11/02 Primary

  Hub construction · CPC title

• A63H27/02

  Model aircraft · CPC title

• F01D5/3007

  of axial insertion type · CPC title