Various applications exist where high-pressure valves are required, but the problem for control of such valves lies in that they have to move against a strong pressure differential that may require significant force, energy, and large actuators. The solution to this problem is to take advantage of the in situ pressure differential to operate valves by opening small valves to change the pressure on either chamber of a hydraulic cylinder that is connected to the valve’s moving element.

The specific solution for application to oil down-hole flow consists of a 4-port valve that is able to connect the pressure of inlet P2 and outlet P1 to a cylinder actuator to drive a sleeve choke valve that controls the flow from the outside of the inner pipe to the inside. A small pump is inserted into the high-pressure (P2) connection line in order to produce additional pressure difference of p and to increase the P2 to P2 + p in case the pressure difference of P = P2 – P1 is not large enough. In this configuration, the 4-port valve has three positions for three different outcomes.
This work was done by Xiaoqi Bao, Stewart Sherrit, Mircea Badescu, Yoseph Bar-Cohen, and Jeffery L. Hall of Caltech for NASA’s Jet Propulsion Laboratory.
In accordance with Public Law 96-517, the contractor has elected to retain title to this invention. Inquiries concerning rights for its commercial use should be addressed to:
Innovative Technology Assets Management
JPL
Mail Stop 321-123
4800 Oak Grove Drive
Pasadena, CA 91109-8099
E-mail: This email address is being protected from spambots. You need JavaScript enabled to view it.
Refer to NPO-48798.
This Brief includes a Technical Support Package (TSP).

Hydraulic High-Pressure Valve Controller Using the In Situ Pressure Difference
(reference NPO48798) is currently available for download from the TSP library.
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Overview
The document presents a technical disclosure regarding a Hydraulic High-Pressure Valve Controller developed by the Jet Propulsion Laboratory (JPL) under NASA's sponsorship. The primary focus is on a novel hydraulic system designed to control large choke valves in high-pressure environments, such as those found in oil wells. The system leverages the mechanical energy from ambient pressure differences to operate valves more efficiently, reducing the energy and power requirements typically associated with high-pressure valve control.
Key features of the system include a small valve that channels pressure from both sides of the choke valve into the chambers of a hydraulic cylinder (actuator), which then operates the valve. Additionally, a small pump is incorporated to provide an extra pressure differential when necessary. This innovative approach allows for the use of the existing pressure differential to drive the hydraulic cylinder, thereby minimizing the need for large actuators and reducing the overall power consumption.
The document outlines the specific problem being addressed: the significant force and energy required to control high-pressure valves, which often necessitates large actuators. The solution proposed involves utilizing the in-situ pressure differential to facilitate valve operation, thereby simplifying the control mechanism and enhancing efficiency.
The potential applications of this technology extend beyond oil well operations to various NASA and reimbursable projects that require high-pressure valve control. The document emphasizes that many aerospace applications could benefit from this technology, as it establishes compact controllers capable of managing high-pressure systems with reduced energy demands.
In summary, the Hydraulic High-Pressure Valve Controller represents a significant advancement in valve control technology, offering a more efficient and compact solution for managing high-pressure environments. This innovation not only addresses the challenges associated with traditional valve control methods but also opens up new possibilities for its application in aeronautical and space activities, showcasing the broader impact of this research on both scientific and commercial fronts.

