Hydraulic actuator with floating pistons

• US 7,882,778 B2
• Filed: 03/11/2008
• Issued: 02/08/2011
• Est. Priority Date: 03/11/2008
• Status: Active Grant

• Current Assignee: Woodward HRT Incorporated (Woodward Incorporated)
• Original Assignee: Woodward HRT Incorporated (Woodward Incorporated)
• Inventors: Fenny, Carlos A., Lauffer, John, Kinard, Marc W.
• Primary Examiner(s): Lazo; Thomas E
• Application Number:
  US12/045,924
• Publication Number:
  US 20090229694A1
• Time in Patent Office: 1,064 Days
• Field of Search: 915/08, 915/09, 915/10, 604/03, 604/05, 244/99.2, 244/99.4, 244/99.5, 244/99.6
• US Class Current: 91/509
• CPC Class Codes: F15B 2211/20576 with multiple pumps
• CPC Class Codes: F15B 2211/31535 having multiple pressure sources and a single output member
• CPC Class Codes: F15B 2211/324 manually, e.g. by using a lever or pedal
• CPC Class Codes: F15B 2211/7054 Having equal piston areas
• CPC Class Codes: F15B 2211/7055 having more than two chambers
• CPC Class Codes: F15B 2211/7056 Tandem cylinders
• CPC Class Codes: F15B 2211/7107 the output members being mechanically linked
• CPC Class Codes: F15B 2211/8757 using redundant components or assemblies
• CPC Class Codes: H03C 1/34 by means of light-sensitive element
• CPC Class Codes: H03C 7/00 Modulating electromagnetic waves devices or arrangements for the modulation of light G02F1/00
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y10T 137/86606 Common to plural valve motor chambers

Abstract

A hydraulic actuator is configured to provide redundant boost control to an aircraft within approximately the same space required by a single hydraulic cylinder. The hydraulic actuator includes a housing and a piston assembly disposed within the housing. The piston assembly includes a ram, a first piston secured to the ram, and second and third pistons disposed on the ram such that the second and third pistons are translatable relative to the longitudinal axis of the ram. The pistons form two hydraulically separate actuator cylinders within the space required by a single cylinder which results in a reduction in the weight and size of the hydraulic actuator.

Claims

1. A hydraulic actuator, comprising:

an elongate shaft;

a housing defining a housing chamber at least a portion of the elongate shaft disposed within the housing chamber, the housing configured to translate relative to the elongate shaft to control positioning of a variable-geometry element associated with an aircraft;

a first piston disposed on the elongate shaft within the housing chamber;

a second piston moveably disposed on the elongate shaft within the housing chamber;

a third piston moveably disposed on the elongate shaft within the housing chamber;

at least one of the second piston and the third piston being operable to translate along the elongated shaft between (i) a first position relative to the first piston when a fluid provided to the housing by a first pressurized fluid source has a pressure that is greater than a pressure of a fluid provided to the housing by a second pressurized fluid source and (ii) a second position relative to the first piston when the fluid provided to the housing by the first pressurized fluid source has a pressure that is less than the pressure of the fluid provided to the housing by the second pressurized fluid source;

the second piston is moveably disposed on the elongate shaft within the housing between the first piston and a first end wall of the housing; and

the third piston is moveably disposed on the elongate shaft within the housing between the first piston and a second end wall of the housing, the second end wall opposing the first end wall;

wherein a first actuator volume defined between the first piston and the second piston and between the first piston and the third piston is configured to fluidly communicate with the first pressure source;

wherein a second actuator volume defined between the second piston and the first end wall of the hydraulic cylinder and between the third piston and the second end wall of the of the hydraulic cylinder is configured to fluidly communicate with the second pressure source; and

wherein the elongate shaft defines a first channel configured to carry fluid between the first pressurized fluid source and a first chamber portion of the first actuator volume and defines a second channel configured to carry fluid between a second chamber portion of the first actuator volume and the first pressurized fluid source.

2. The hydraulic actuator of claim 1, comprising a first channel configured to carry fluid between the second pressurized fluid source and a third chamber portion of the second actuator volume and a second channel configured to carry fluid between the second pressurized fluid source and a fourth chamber portion of the second actuator volume.

3. The hydraulic actuator of claim 1, wherein the second piston comprises a seal disposed about an outer periphery of the second piston between the second piston and an inner wall of the housing.

4. The hydraulic actuator of claim 1, wherein the third piston comprises a seal disposed about an outer periphery of the third piston between the third piston and an inner wall of the housing.

5. A servovalve, comprising:

a first servovalve assembly having a first housing defining a first fluid pathway;

a second servovalve having a second housing defining a second fluid pathway; and

a hydraulic actuator in fluid communication with the first servovalve assembly and the second servovalve assembly, the hydraulic actuator having;

an elongate shaft;

a housing defining a housing chamber at least a portion of the elongate shaft disposed within the housing chamber, the housing configured to translate relative to the elongate shaft to control positioning of a variable-geometry element associated with an aircraft;

a first piston disposed on the elongate shaft within the housing chamber;

a second piston moveably disposed on the elongate shaft within the housing chamber; and

a third piston moveably disposed on the elongate shaft within the housing chamber;

at least one of the second piston and the third piston being operable to translate along the elongated shaft between (i) a first position relative to the first piston when a fluid provided to the housing by the first servovalve assembly has a pressure that is greater than a pressure of a fluid provided to the housing by the second servovalve assembly and (ii) a second position relative to the first piston when the fluid provided to the housing by the first servovalve assembly has a pressure that is less than the pressure of the fluid provided to the housing by the second servovalve assembly.

6. The servovalve of claim 5, wherein:

the second piston is moveably disposed on the elongate shaft within the housing between the first piston and a first end wall of the housing; and

a third piston moveably disposed on the elongate shaft within the housing between the first piston and a second end wall of the housing, the second end wall opposing the first end wall;

wherein a first actuator volume defined between the first piston and the second piston and between the first piston and the third piston is configured to fluidly communicate with the first servovalve assembly; and

wherein a second actuator volume defined between the second piston and the first end wall of the hydraulic cylinder and between the third piston and the second end wall of the of the hydraulic cylinder is configured to fluidly communicate with the second servovalve assembly.

7. The servovalve of claim 6, wherein the first servovalve assembly comprises a directional check valve disposed in fluid communication between the first actuator volume of the hydraulic actuator and a transmission line of a first pressurized fluid source, the directional check valve configured to be positioned between (i) a first position to allow the flow of fluid along the transmission line from the first pressurized fluid source to the first actuator volume of the hydraulic actuator and (ii) a second position that limits the flow of fluid from the first actuator volume of the hydraulic actuator to the first pressurized fluid source.

8. The servovalve of claim 7, wherein, the first actuator volume comprises a first chamber portion and a second chamber portion and wherein, when positioned in a second position, the directional check valve is configured to maintain a volume of fluid within at least one of the first chamber portion and the second chamber portion.

9. The servovalve of claim 6, wherein the second servovalve assembly comprises a directional check valve disposed in fluid communication between the second actuator volume of the hydraulic actuator and a transmission line of a second pressurized fluid source, the directional check valve configured to be positioned between (i) a first position to allow the flow of fluid along the transmission line from the second pressurized fluid source to the second actuator volume of the hydraulic actuator and (ii) a second position that limits the flow of fluid from the second actuator volume of the hydraulic actuator to the second pressurized fluid source.

10. The servovalve of claim 9, wherein, the second actuator volume comprises a third chamber portion and a fourth chamber portion and wherein, when positioned in a second position, the directional check valve is configured to maintain a volume of fluid within at least one of the third chamber portion and the fourth chamber portion.

11. The servovalve of claim 6, wherein the elongate shaft defines a first channel configured to carry fluid between the first servovalve assembly and a first chamber portion of the first actuator volume and defines a second channel configured to carry fluid between a second chamber portion of the first actuator volume and the first servovalve assembly.

12. The servovalve of claim 5, wherein the second piston comprises a seal disposed about an outer periphery of the second piston between the second piston and an inner wall of the housing.

13. The servovalve of claim 5, wherein the third piston comprises a seal disposed about an outer periphery of the third piston between the third piston and an inner wall of the housing.

14. A hydraulic actuator system, comprising:

a first pressurized fluid source;

a second pressurized fluid source;

a first servovalve assembly having a first housing defining a first fluid pathway, the first servovalve assembly in fluid communication with the first pressurized fluid source;

a second servovalve having a second housing defining a second fluid pathway the second servovalve assembly in fluid communication with the second pressurized fluid source; and

a hydraulic actuator in fluid communication with the first servovalve assembly and the second servovalve assembly, the hydraulic actuator having;

an elongate shaft;

a housing defining a housing chamber at least a portion of the elongate shaft disposed within the housing chamber, the housing configured to translate relative to the elongate shaft to control positioning of a variable-geometry element associated with an aircraft;

a first piston disposed on the elongate shaft within the housing chamber;

a second piston moveably disposed on the elongate shaft within the housing chamber; and

a third piston moveably disposed on the elongate shaft within the housing chamber;

at least one of the second piston and the third piston being operable to translate along the elongated shaft between (i) a first position relative to the first piston when a fluid provided to the housing by the first pressurized fluid source via the first servovalve assembly has a pressure that is greater than a pressure of a fluid provided by the second pressurized fluid source to the housing via the second servovalve assembly and (ii) a second position relative to the first piston when the fluid provided to the housing by the first pressurized fluid source via the first servovalve assembly has a pressure that is less than a pressure of the fluid provided by the second pressurized fluid source to the housing via the second servovalve assembly.

15. The hydraulic actuator system of claim 14, wherein:

the second piston is moveably disposed on the elongate shaft within the housing between the first piston and a first end wall of the housing; and

a third piston moveably disposed on the elongate shaft within the housing between the first piston and a second end wall of the housing, the second end wall opposing the first end wall;

wherein a first actuator volume defined between the first piston and the second piston and between the first piston and the third piston is configured to fluidly communicate with the first servovalve assembly; and

wherein a second actuator volume defined between the second piston and the first end wall of the hydraulic cylinder and between the third piston and the second end wall of the of the hydraulic cylinder is configured to fluidly communicate with the second servovalve assembly.

16. The hydraulic actuator system of claim 15, wherein the first servovalve assembly comprises a directional check valve disposed in fluid communication between the first actuator volume of the hydraulic actuator and a transmission line of a first pressurized fluid source, the directional check valve configured to be positioned between (i) a first position to allow the flow of fluid along the transmission line from the first pressurized fluid source to the first actuator volume of the hydraulic actuator and (ii) a second position that limits the flow of fluid from the first actuator volume of the hydraulic actuator to the first pressurized fluid source.

17. The hydraulic actuator system of claim 16, wherein, the first actuator volume comprises a first chamber portion and a second chamber portion and wherein, when positioned in a second position, the directional check valve is configured to maintain a volume of fluid within at least one of the first chamber portion and the second chamber portion.

18. The hydraulic actuator system of claim 15, wherein the second servovalve assembly comprises a directional check valve disposed in fluid communication between the second actuator volume of the hydraulic actuator and a transmission line of a second pressurized fluid source, the directional check valve configured to be positioned between (i) a first position to allow the flow of fluid along the transmission line from the second pressurized fluid source to the second actuator volume of the hydraulic actuator and (ii) a second position that limits the flow of fluid from the second actuator volume of the hydraulic actuator to the second pressurized fluid source.

19. The hydraulic actuator system of claim 18, wherein, the second actuator volume comprises a third chamber portion and a fourth chamber portion and wherein, when positioned in a second position, the directional check valve is configured to maintain a volume of fluid within at least one of the third chamber portion and the fourth chamber portion.