Jam-tolerant rotary control motor for hydraulic actuator valve

Patent metadata

Field	Value
Publication number	US-9783290-B2
Application number	US-201314038182-A
Country	US
Kind code	B2
Filing date	Sep 26, 2013
Priority date	Mar 14, 2013
Publication date	Oct 10, 2017
Grant date	Oct 10, 2017

Abstract

According to one embodiment, a linear control motor includes a first permanent magnet, a coil, a shaft, a first non-magnetic material, and a joint coupled between the shaft and a spool operable to convert rotations of the shaft into axial movements of the spool. The first non-magnetic material is disposed between at least one of the movable components and at least one of the static components and operable to prevent physical contact between at least one of the movable components and at least one of the static components.

First claim

What is claimed is:

1. A rotorcraft, comprising:
a body;
a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source;
a hub coupled to the drive shaft;
a rotor blade coupled to the hub;
a hydraulic actuator in mechanical communication with the rotor blade and operable to change a position of the rotor blade;
an actuator control valve system operable to regulate a flow of fluid to the hydraulic actuator, the actuator control valve system comprising a servo valve and a spool extending through the servo valve; and
a control motor in mechanical communication with the actuator control valve system, the control motor comprising:
a first permanent magnet operable to generate a first magnetic flux path;
a coil operable to selectively add magnetic flux to and subtract magnetic flux from the magnetic flux flowing in the first magnetic flux path, wherein one of the first permanent magnet and the coil is a movable component and the other one of the first permanent magnet and the coil is a static component, the movable component operable to rotate relative to the static component in response to variations in flux flowing in the first magnetic flux path;
a shaft coupled to the movable component such that the shaft is operable to rotate in response to variations in flux flowing in the first magnetic flux path;
a first non-magnetic material disposed between at least one of the movable components and at least one of the static components and operable to prevent physical contact between at least one of the movable components and at least one of the static components, wherein the first non-magnetic material is at least partially movable relative to both the movable component and the static component;

and
A joint coupled between the shaft and the spool and operable to convert rotations of the shaft into axial movements of the spool.

2. The rotorcraft of claim 1 , wherein a spring couples the first non-magnetic material to the movable component.

3. The rotorcraft of claim 1 , the joint comprising:
a pin comprising a detent portion;
a detent member adjacent to the pin and sized to fit at least partially within the detent portion;
a spring configured to apply a force against the detent member towards the pin, the detent member positioned between the spring and the pin; and
a substantially spherical member adjacent the pin and partially disposed within a recess of the spool, the substantially spherical member operable to reposition the pin such that the detent portion is positioned to at least partially receive the detent member.

4. The rotorcraft of claim 1 , the control motor further comprising:
a bearing separating the shaft from the static component; and
a break wire adjacent to the bearing, the break wire configured to sever in response to a failure of the bearing.

5. The rotorcraft of claim 1 , the control motor further comprising:
a metal tube positioned around the shaft;
a first electrical transmission line associated with the shaft;
a second electrical transmission line associated with the metal tube;
a bearing separating the metal tube from the static component; and
a jam member disposed between the bearing and the metal tube, the jam member configured to deform the metal tube in response to a failure of the bearing such the deformation closes an electrical circuit between the first electrical transmission line and the second electrical transmission line.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Covington Charles Eric
• Fenny Carlos A

Classifications

• B64C27/605

  including swash plate, spider or cam mechanisms · CPC title

• H02K7/003

  Couplings; Details of shafts (means for mounting rotors on shafts H02K1/28) · CPC title

• H01F7/122

  by permanent magnets {(H01F7/1615, H01F7/1646 take precedence)} · CPC title

• H01F7/066

  Electromagnets with movable winding · CPC title

• B64C27/64 Primary

  using fluid pressure, e.g. having fluid power amplification · CPC title