Servo valve

Patent metadata

Field	Value
Publication number	US-9702478-B2
Application number	US-201313766080-A
Country	US
Kind code	B2
Filing date	Feb 13, 2013
Priority date	Feb 14, 2012
Publication date	Jul 11, 2017
Grant date	Jul 11, 2017

Abstract

The invention relates to a servo valve, in particular a two-stage or multistage electrohydraulic servo valve, having a first stage which works as a pilot stage, and a second stage which works as a power stage, wherein the second stage has a valve block and a control slide valve sleeve arranged therein and having a jacket surface ( 18 ), wherein the jacket surface and/or another region of the control slide valve sleeve is preferably provided with at least one flow passage for transferring control flow and/or volume flow, and wherein a control slide valve is movably arranged in the control slide valve sleeve, wherein at least one of the flow passages is formed by a groove which is arranged in the surface of the control slide valve sleeve and which does not extend sectionally or overall in the peripheral direction of the control slide valve sleeve.

First claim

The invention claimed is:

1. A servo valve, having
a first stage which works as a pilot stage, and
a second stage which works as a power stage, wherein
the second stage has a valve block ( 14 ) and a control slide valve sleeve ( 16 ) arranged in the valve block ( 14 ) and having a jacket surface ( 18 ),
the control slide valve sleeve ( 16 ) has a main longitudinal axis and, including the jacket surface ( 18 ), is provided with a plurality of flow passages ( 20 , 20 ′, 20 ″) arranged for transferring control flow and volume flow of fluid,
a control slide valve is movably arranged within the control slide valve sleeve ( 16 ), with position of the valve within the control slide valve sleeve ( 16 ) controlled by flow of the fluid through said passages ( 20 , 20 ′, 20 ″) of the control slide valve sleeve ( 16 ),
at least one of the flow passages ( 20 , 20 ′, 20 ″) is formed by a pair of grooves ( 20 ′, 20 ′) arranged as spaced apart, parallel, oblong slits directly on top of an outermost surface of the jacket surface ( 18 ) of the control slide valve sleeve ( 16 ) with mirror symmetry to one another and main longitudinal axes of both said grooves ( 20 ′, 20 ′) extending one after another and aligned in parallel with the longitudinal axis of the control slide valve sleeve ( 16 ) for transferring the control fluid flow,
a radial interference press fit is provided between the control valve slide sleeve ( 16 ) and the valve block ( 14 ), with the control valve slide sleeve ( 16 ) arranged in and surrounded by the valve block ( 14 ) and pressed in the valve block ( 14 ),
hydraulic circuits arise between the control slide valve sleeve ( 16 ) and the valve block ( 14 ), and
additional flow passages ( 20 ″) are formed near both opposite ends ( 28 ) of the control slide valve sleeve ( 16 ).

2. A servo valve in accordance with claim 1 , wherein said plurality of flow passages ( 20 , 20 ′, 20 ″) are formed on the jacket surface ( 18 ) of the control slide valve sleeve ( 16 ), having different dimensions and being arranged symmetrically to one another on the jacket surface ( 18 ).

3. A servo valve in accordance with claim 1 , additionally comprising at least one seal for sealing the hydraulic circuits arising between the control slide valve sleeve ( 16 ) and the valve block ( 14 ).

4. A servo valve in accordance with claim 1 , wherein the control slide valve sleeve ( 16 ) has grooves or recesses ( 22 ) at two opposite ends ( 28 ) on which a respective O-ring seal ( 26 ) is attached.

5. A servo valve in accordance with claim 1 , wherein the valve block ( 14 ) of the power stage of the servo valve ( 10 ) has connector ports (C 1 , R, C 2 , P) which are formed at a lower side of the valve block ( 14 ), with the flow passages ( 20 , 20 ′, 20 ″) of the control slide valve sleeve ( 16 ) being in communication with the connector ports (C 1 , R, C 2 , P).

6. A servo valve in accordance with claim 1 , wherein the valve block ( 14 ) surrounding the control slide valve sleeve ( 16 ) comprises steel, titanium or aluminum.

7. A servo valve in accordance with claim 1 , wherein the control slide valve sleeve ( 16 ) comprises steel, titanium or aluminum.

8. An actuator for controlling one or more flaps of an aircraft, wherein the actuator is connected to the servo valve in accordance with claim 1 wherein the actuator is controlled hydraulically by the servo valve.

9. The actuator in accordance with claim 8 , wherein the actuator has a housing and/or a valve block; and the second stage of the servo valve is integrated in the housing and/or in the valve block of the actuator.

10. An aircraft having at least one servo valve in accordance with claim 1 .

11. A servo valve in accordance with claim 1 , comprising
a further flow passage ( 20 ) spaced apart from a plane of the mirror image flow passages ( 20 ′, 20 ′) is formed approximately at a center of the control slide valve sleeve ( 16 ) as an elongate groove extending along the longitudinal axis of the control slide valve sleeve ( 16 ) and parallel to the mirror image flow passages ( 20 ′, 20 ′).

12. A servo valve in accordance with claim 11 , wherein the opposite ends ( 28 ) of the control valve sleeve ( 16 ) each have a stepped, smaller outermost diameter ( 22 ) extending circumferentially around the ends ( 28 ) of the valve sleeve ( 16 ) to receive a respective O-ring seal ( 26 ) around an outermost circumference of the opposite valve sleeve ends ( 28 ) and circumferentially contacting the valve block ( 14 ).

13. A servo valve in accordance with claim 1 , wherein the opposite ends ( 28 ) of the control valve sleeve ( 16 ) each have a stepped, smaller outermost diameter ( 22 ) extending circumferentially around the ends ( 28 ) of the valve sleeve ( 16 ) to receive a respective O-ring seal ( 26 ) around an outermost circumference of the opposite valve sleeve ends ( 28 ) and circumferentially contacting the valve block ( 14 ).

14. A servo valve in accordance with claim 1 , wherein the position of the valve within the control slide valve sleeve ( 16 ) is controlled solely by flow of the fluid through said passages ( 20 , 20 ′, 20 ″) of the control slide valve sleeve ( 16 ).

15. A servo valve having
a first stage which works as a pilot stage, and
a second stage which works as a power stage, wherein
the second stage has a valve block ( 14 ) and a control slide valve sleeve ( 16 ) arranged in the valve block ( 14 ) and having a jacket surface ( 18 ),
the control slide valve sleeve ( 16 ) including the jacket surface ( 18 ) is provided with a plurality of flow passages ( 20 , 20 ′, 20 ″) arranged for transferring control flow and volume flow of fluid,
a control slide valve is movably arranged in the control slide valve sleeve ( 16 ),
at least one of the flow passages ( 20 , 20 ′, 20 ″) is formed by a pair of grooves ( 20 ′, 20 ′) arranged as spaced apart, parallel slits in the jacket surface ( 18 ) of the control slide valve sleeve ( 16 ) with mirror symmetry to one another and both extending one after another along a longitudinal axis of the control slide valve sleeve ( 16 ) and arranged for transferring the control fluid flow,
a press fit is provided between the control valve slide sleeve ( 16 ) and the valve block ( 14 ), with the control valve slide sleeve ( 16 ) arranged in the valve block ( 14 ) and pressed in the valve block ( 14 )
hydraulic circuits arise between the control slide valve sleeve ( 16 ) and the valve block ( 14 ), with said press fit sealing the hydraulic circuits,
additional flow passages ( 20 ″) are formed near both opposite ends ( 28 ) of the control slide valve sleeve ( 16 ),
additionally comprising
a further flow passage ( 20 ) spaced apart from a plane of the mirror image flow passages ( 20 ′, 20 ′) is formed approximately at a center of the control slide valve sleeve ( 16 ) as an elongate groove extending along the longitudinal axis of the control slide valve sleeve ( 16 ) and parallel to the mirror image flow passages ( 20 ′, 20 ′), and
the further flow passage ( 20 ) intercommunicates at opposite ends with two outermost grooves extending in a radial direction along an outer circumferential exterior of the control valve sleeve ( 16 ).

16. A servo valve in accordance with claim 15 , wherein the opposite ends ( 28 ) of the control valve sleeve ( 16 ) each have a stepped, smaller outermost diameter ( 22 ) to receive a respective O-ring seal ( 26 ) around an outermost circumference of the opposite valve sleeve ends ( 28 ).

Assignees

• Liebherr Aerospace Lindenberg GmbH

Inventors

• Frick Joern
• Gaile Anton
• Weixler Franz

Classifications

• F15B13/0402 Primary

  for linearly sliding valves, e.g. spool valves · CPC title

• F15B13/0433

  the pilot valves being pressure control valves (F15B13/0435, F15B13/0436, F15B13/0438 take precedence) · CPC title

• F16K31/42 Primary

  by means of electrically-actuated members in the supply or discharge conduits of the fluid motor (F16K31/40 takes precedence) · CPC title

• F15B13/043

  with electrically-controlled pilot valves · CPC title