Propulsor brake lock

Patent metadata

Field	Value
Publication number	US-12258140-B2
Application number	US-202318310679-A
Country	US
Kind code	B2
Filing date	May 2, 2023
Priority date	Feb 21, 2023
Publication date	Mar 25, 2025
Grant date	Mar 25, 2025

Abstract

A propulsor brake lock system includes an aircraft propulsor, a reduction gear assembly, a brake shaft, and a brake assembly. The aircraft propulsor includes a propeller having a propeller input shaft coupled thereto. The reduction gear assembly includes at least an input gear and an output gear. The input gear and output gear are both rotatable with the propeller input shaft. The brake shaft is coupled to, and is rotatable with, the output gear. The brake assembly is coupled to the brake shaft and is moveable between a disengaged position, in which the brake shaft may rotate whenever the output gear rotates, and an engaged position, in which the brake shaft is prevented from rotating, thereby preventing rotation of the output gear, the input gear, and the propeller input shaft.

First claim

What is claimed is:

1. A propulsor brake lock system, comprising:
an aircraft propulsor including a propeller having a propeller input shaft coupled thereto;
a reduction gear assembly including at least an input gear and an output gear, the input gear and output gear rotatable with the propeller input shaft;
a brake shaft coupled to, and rotatable with, the output gear; and
a brake assembly coupled to the brake shaft, the brake assembly moveable between a disengaged position, in which the brake shaft may rotate whenever the output gear rotates, and an engaged position, in which the brake shaft is prevented from rotating, thereby preventing rotation of the output gear, the input gear, and the propeller input shaft,
wherein:
the brake assembly is a bi-stable brake assembly that is adapted to receive an electrical pulse and is configured such that: (i) when the brake assembly is in the disengaged position, upon receipt of the electrical pulse, the brake assembly moves from the disengaged position to the engaged position, and (ii) when the brake assembly is in the engaged position, upon receipt of the electrical pulse, the brake assembly moves from the engaged position to the disengaged position,
the bi-stable brake assembly is a dual-channel brake, and
each channel is adapted to selectively receive the electrical pulse.

2. The system of claim 1 , further comprising:
an electric motor coupled to the propeller input shaft and configured to selectively supply torque thereto;
a motor control in operable communication with the electric motor and configured to selectively energize, and thereby control the torque supplied by, the electric motor.

3. The system of claim 2 , wherein the motor control is in operable communication with the brake assembly and is further configured to selectively command the brake assembly to move between the disengaged position and the engaged position.

4. The system of claim 3 , further comprising:
a propeller position sensor configured to sense a rotational position of the propeller and supply a propeller position sensor signal indicative thereof,
wherein the motor control is coupled to receive a brake command and the propeller position sensor signal and is further configured:
to process the propeller position signal to determine when the propeller is in a predetermined rotational position, and
upon receipt of the brake command, to command the brake assembly to move to the engaged position only when the propeller is in the predetermined position.

5. The system of claim 1 , further comprising:
a first electric motor coupled to the propeller input shaft and configured to selectively supply torque thereto;
a second electric motor coupled to the propeller input shaft and configured to selectively supply torque thereto;
a dual-channel motor control including a first channel and a second channel, the first channel in operable communication with the first electric motor, the second channel in operable communication with the second electric motor, the dual-channel motor control configured such that:
only one of the first channel or the second channel is active,
when the first channel is active, the first channel is operable to selectively energize, and thereby control the torque supplied by, the first electric motor, and
when the second channel is active, the second channel is operable to selectively energize, and thereby control the torque supplied by, the second electric motor.

6. The system of claim 5 , wherein the dual-channel motor control is in operable communication with the brake assembly and is further configured to selectively command the brake assembly to move between the disengaged position and the engaged position.

7. The system of claim 6 , further comprising:
a first propeller position sensor configured to sense a rotational position of the propeller and supply a first propeller position sensor signal indicative thereof;
a second propeller position sensor configured to sense the rotational position of the propeller and supply a second propeller position sensor signal indicative thereof,
wherein:
the first channel is coupled to receive a brake command and the first propeller position sensor signal and the second channel is coupled to receive the brake command and the second propeller position sensor signal,
when the first channel is active, the first channel is further configured to:
process the first propeller position signal to determine when the propeller is in a predetermined rotational position, and
upon receipt of the brake command, to command the brake assembly to move to the engaged position only when the propeller is in the predetermined position; and
when the second channel is active, the second channel is further configured to:
process the second propeller position signal to determine when the propeller is in the predetermined rotational position, and
upon receipt of the brake command, to command the brake assembly to move to the engaged position only when the propeller is in the predetermined position.

8. The system of claim 1 , wherein the propellor input shaft includes a spline gear that meshes with the input gear.

9. A propulsor brake lock system, comprising:
an aircraft propulsor including a propeller having a propeller input shaft coupled thereto;
a propeller position sensor configured to sense a rotational position of the propeller and supply a propeller position sensor signal indicative thereof;
a reduction gear assembly including at least an input gear and an output gear, the input gear and output gear rotatable with the propeller input shaft;
an electric motor coupled to the propeller input shaft and configured to selectively supply torque thereto;
a brake shaft coupled to, and rotatable with, the output gear;
a brake assembly coupled to the brake shaft, the brake assembly moveable between a disengaged position, in which the brake shaft may rotate whenever the output gear rotates, and an engaged position, in which the brake shaft is prevented from rotating, thereby preventing rotation of the output gear, the input gear, and the propeller input shaft;
a motor control in operable communication with the electric motor and with the brake assembly and coupled to receive a brake command and the propeller position signal, the motor control configured to:
(i) selectively energize, and thereby control the torque supplied by, the electric motor,
selectively command the brake assembly to move between the disengaged position and the engaged position,
(ii) process the propeller position signal to determine when the propeller is in a predetermined rotational position, and
(ii) upon receipt of the brake command, to command the brake assembly to move to the engaged position only when the propeller is in the predetermined position.

10. The system of claim 9 , wherein the brake assembly is a bi-stable brake assembly that is adapted to receive an electrical pulse and is configured such that:
when the brake assembly is in the disengaged position, upon receipt of the electrical pulse, the brake assembly moves from the disengaged position to the engaged position, and
when the brake assembly is in the engaged position, upon receipt of the electrical pulse, the brake assembly moves from the engaged position to the disengaged position.

11. The system of claim 10 , wherein:
the bi-stable brake assembly is a dual-channel brake; and
each channel is adapted to selectively receive the electrical pulse.

12. The system of claim 9 , wherein the propellor input shaft includes a spline gear that meshes with the input gear.

13. A propulsor brake lock system, comprising:
an aircra

Assignees

• Honeywell Int Inc

Inventors

• Vaughan Ronald
• Quitmeyer James N
• Canepa Everett

Classifications

• B64D35/08

  characterised by the transmission being driven by a plurality of power plants (for hybrid-electric power plants B64D35/022) · CPC title

• B64D27/30

  Aircraft characterised by electric power plants · CPC title

• B64C11/002

  Braking propellers, e.g. for measuring the power output of an engine · CPC title

• B64D31/14

  Transmitting means between initiating means and power plants · CPC title

• B64U2101/61

  for transporting passengers · CPC title