A. Sidi‐Yekhlef
Thomas Jefferson National Accelerator Facility
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Featured researches published by A. Sidi‐Yekhlef.
TRANSACTIONS OF THE CRYOGENIC ENGINEERING CONFERENCE—CEC: Advances in Cryogenic Engineering | 2010
P. Arnold; Lutz Decker; D. Howe; J. Urbin; Jonathan Homan; Carl Reis; J. Creel; Venkatarao Ganni; P. Knudsen; A. Sidi‐Yekhlef
The James Webb Telescope is the successor to the Hubble Telescope and will be placed in an orbit of 1.5 million km from earth. Before launch in 2014, the telescope will be tested in NASA Johnson Space Center’s (JSC) space simulation chamber, Chamber A. The tests will be conducted at deep space conditions. Chamber A’s helium cryo‐panels are currently cooled down to 20 K by two Linde 3.5 kW helium refrigerators. The new 12.5 kW, 20‐K helium coldbox described in this paper is part of the upgrade to the chamber systems for this large test program. The Linde coldbox will provide refrigeration in several operating modes where the temperature of the chamber is being controlled with a high accuracy due to the demanding NASA test requirements. The implementation of two parallel expansion turbine strings and the Ganni cycle—Floating Pressure process results in a highly efficient and flexible process that minimizes the electrical input power. This paper will describe the collaboration and execution of the coldbox pr...
TRANSACTIONS OF THE CRYOGENIC ENGINEERING CONFERENCE—CEC: Advances in Cryogenic Engineering | 2010
Jonathan Homan; Michael Montz; Venkatarao Ganni; A. Sidi‐Yekhlef; P. Knudsen; J. Creel; D. Arenius; Sam Garcia
NASA at the Johnson Space Center (JSC) in Houston is presently working toward modifying the original forced flow liquid nitrogen cooling system for the thermal shield in the space simulation chamber‐A in Building 32 to work as a natural flow (thermo siphon) system. Chamber A is 19.8 m (65 ft) in diameter and 35.66 m (117 ft) high. The LN2 shroud environment within the chamber is approximately 17.4 m (57 ft) in diameter and 28 m (92 ft) high. The new thermo siphon system will improve the reliability, stability of the system. Also it will reduce the operating temperature and the liquid nitrogen use to operate the system. This paper will present the requirements for the various operating modes. System level thermodynamic comparisons of the existing system to the various options studied and the final option selected will be outlined. A thermal and hydraulic analysis to validate the selected option for the conversion of the current forced flow to natural flow design will be discussed. The proposed modification...
ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering#N#Conference - CEC, Vol. 53 | 2008
D. Arenius; J. Creel; K. Dixon; Venkatarao Ganni; P. Knudsen; A. Sidi‐Yekhlef; Mathew Wright
In February 2006, Jefferson Laboratory in Newport News, VA, received “Critical Decision 1” (CD-1) approval to proceed with the engineering and design of the long anticipated upgrade to increase the beam energy of CEBAF, the Continuous Electron Beam Accelerator Facility, from 6 GeV to 12 GeV. This will require the installation of 10 new cryomodules, and additional 2.1-K refrigeration beyond the available 4600 W to handle the increased heat loads. Additionally, a new experimental hall, Hall D, is planned that will require the installation of a small, available refrigerator. This paper will present an overview of the integration of the new proposed refrigeration system into CEBAF, the installation of the available refrigerator for Hall D, and includes planned work scope, current schedule plans and project status.
IOP Conference Series: Materials Science and Engineering | 2017
F. Casagrande; Venkatarao Ganni; P. Knudsen; S. Jones; A. Sidi‐Yekhlef; H. Tatsumoto; C. Nguyen; A. Fila; Gerardo Vargas; C. Dudley; N. Joseph; S. Stanley; K. Dixon; Robert O. Norton; Nathaniel A. Laverdure; S. Yang
Construction and installation of the FRIB 4.5 K helium refrigeration system is nearing completion, with compressor system commissioning and 4.5 K refrigerator commissioning on schedule to occur in late 2017. The LINAC 4.5 K helium distribution system, all major process equipment, and the cryogenic distribution for the sub-systems have been procured and delivered. The sub-atmospheric cold box fabrication is planned to begin the summer of 2017, which is on schedule for commissioning in the spring of 2018. Commissioning of the support systems, such as the helium gas storage, helium purifier, and oil processor is planned to be complete by the summer of 2017. This paper presents details of the equipment procured, installation status and commissioning plans.
TRANSACTIONS OF THE CRYOGENIC ENGINEERING CONFERENCE—CEC: Advances in Cryogenic Engineering | 2010
Jonathan Homan; Venkatarao Ganni; A. Sidi‐Yekhlef; J. Creel; Robert O. Norton; Robert Linza; Gerardo Vargas; John Lauterbach; J. Urbin; D. Howe
Two helium refrigerators, each rated for 3.5 KW at 20 K, are used at NASA’s Johnson Space Center (JSC) in Building No. 32 to provide cryogenic‐pumping within two large thermal‐vacuum chambers. These refrigerators were originally commissioned in 1996. New changes to the controls of these refrigerators were recently completed. This paper describes some of the control issues that necessitated the controls change‐over. It will describe the modifications and the new process control which allows the refrigerators to take advantage of the Ganni Cycle “floating pressure” control technology. The controls philosophy change‐over to the floating pressure control technology was the first application on a helium gas refrigeration system. Previous implementations of the floating pressure technology have been on 4 K liquefaction and refrigeration systems, which have stored liquid helium volumes that have level indications used for varying the pressure levels (charge) in the system for capacity modulation. The upgrades ha...
ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering#N#Conference - CEC, Vol. 53 | 2008
R. Than; J. Tuozzolo; A. Sidi‐Yekhlef; Venkatarao Ganni; P. Knudsen; D. Arenius
Brookhaven National Laboratory continues its multi-year program to improve the operational efficiency, reliability, and stability of the cryogenic system, which also resulted in an improved beam availability of the Relativistic Heavy Ion Collider (RHIC). This paper summarizes the work and changes made after each phase over the past four years to the present, as well as proposed future improvements. Power usage dropped from an initial 9.4 MW to the present 5.1 MW and is expected to drop below 5 MW after the completion of the remaining proposed improvements. The work proceeded in phases, balancing the Colliders schedule of operation, time required for the modifications and budget constraints. The main changes include process control, compressor oil removal and management, elimination of the use of cold compressors and two liquid-helium storage tanks, insulation of the third liquid-helium storage tank, compressor-bypass flow reduction and the addition of a load turbine (Joule-Thomson expander) with associat...
ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering Conference, CEC | 2006
A. Sidi‐Yekhlef; Roberto Than; J. Tuozzolo; Venkatarao Ganni; P. Knudsen; D. Arenius
An ongoing program at Brookhaven National Laboratory (BNL) consists of improving the efficiency of the Relativistic Heavy Ion Collider (RHIC) cryogenic system and reducing its power consumption. Phase I and II of the program addressed plant operational improvements and modifications that resulted in substantial operational cost reduction and improved system reliability and stability, and a compressor input power reduction of 2 MW has been demonstrated. Phase III, now under way, consists of plans for further increasing the efficiency of the plant by adding a load “wet” turbo‐expander and its associated heat exchangers at the low temperature end of the plant. This additional stage of cooling at the coldest level will further reduce the required compressor flow and therefore compressor power input. This paper presents the results of the plant characterization, as it is operating presently, as well as the results of the plant simulations of the various planned upgrades for the plant. The immediate upgrade includes the changes associated with the load expander. The subsequent upgrade will involve the resizing of expander 5 and 6 to increase their efficiencies. The paper summarizes the expected improvement in the plant efficiency and the overall reduction in the compressor power.An ongoing program at Brookhaven National Laboratory (BNL) consists of improving the efficiency of the Relativistic Heavy Ion Collider (RHIC) cryogenic system and reducing its power consumption. Phase I and II of the program addressed plant operational improvements and modifications that resulted in substantial operational cost reduction and improved system reliability and stability, and a compressor input power reduction of 2 MW has been demonstrated. Phase III, now under way, consists of plans for further increasing the efficiency of the plant by adding a load “wet” turbo‐expander and its associated heat exchangers at the low temperature end of the plant. This additional stage of cooling at the coldest level will further reduce the required compressor flow and therefore compressor power input. This paper presents the results of the plant characterization, as it is operating presently, as well as the results of the plant simulations of the various planned upgrades for the plant. The immediate upgrade inc...
ADVANCES IN CRYOGENIC ENGEINEERING: Transactions of the Cryogenic Engineering Conference - CEC | 2004
A. Nicoletti; A. Reuter; A. Sidi‐Yekhlef; P. Talty; E. Quimby
A stand‐alone cryogenic system designed to maintain the magnets of the Relativistic Heavy Ion Collider (RHIC) at between 80 and 100 K during accelerator shutdown periods has been conceived and designed at Brookhaven National Laboratory and built by PHPK Technologies of Columbus, Ohio. Since most thermal contraction occurs above this temperature, this unit, referred to as the 80‐K Cooler, will eliminate the stresses associated with thermal cycling. The cooling system will provide the necessary refrigeration by circulating cooled helium gas at approximately 1500 kPA through the RHIC heat shields and magnets. This helium is cooled by heat exchange with liquid nitrogen and circulated via three cold centrifugal pumps. The nominal delivered cooling capacity required to maintain the magnets at temperature is approximately 36 kW, primarily intercepted at the heat shield. The system also has separate heat exchangers for use as a pre‐cooler from room temperature to 82 K. Selection of sextant or sextants for pre‐coo...
Nuclear Instruments & Methods in Physics Research Section A-accelerators Spectrometers Detectors and Associated Equipment | 2006
C. Montag; R. Bonati; Joseph Brennan; J. Butler; P. Cameron; G. Ganetis; P. He; W. Hirzel; L. Jia; P. Koello; W. Louie; G. McIntyre; A. Nicoletti; J. Rank; T. Roser; T. Satogata; J. Schmalzle; A. Sidi‐Yekhlef; J. Sondericker; T. Tallerico
25th Space Simulation Conference 2008, SSC 2008 | 2008
Jonathan Homan; Robert Linza; Sam Garcia; Gerardo Vargas; John Lauterbach; Venkatarao Ganni; A. Sidi‐Yekhlef; Robert O. Norton; J. Creel; John Urbin; Don Howe