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Design Of A Small Turbjojet Compressor Test Facility
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Book Synopsis Design of a Small-turbjojet Compressor Test Facility by : Justin T. Reinhart
Download or read book Design of a Small-turbjojet Compressor Test Facility written by Justin T. Reinhart and published by . This book was released on 2021 with total page 105 pages. Available in PDF, EPUB and Kindle. Book excerpt: Validation of compressor aerodynamic design can be obtained through in-engine testing with considerable investment of time and money, or in rig testing, wherein a range of interchangeable designs can be tested without exposure to effects of other engine components. To more rapidly explore centrifugal and mixed-flow compressor designs for small, thrust-producing aviation gas-turbine engines, called turbojets, the Air ForceResearch Laboratories (AFRL) initiated development of a test apparatus to be integrated into an existing test facility at Wright-Patterson Air Force Base (WPAFB). Design of the inlet flow conditioning and measuring system, mechanical systems, exhaust discharge valve, and exhaust collector is accomplished through sizing calculations, aerodynamic and mechanical analysis. This thesis project presents the final design of this small-turbojet compressor test facility, capable of testing virtually the entire operating map of compressors in the desired size range. Fabrication of the test rig is underway as of the conclusion of this thesis; component testing, assembly, and initial test article testing is planned thereafter.
Book Synopsis Portable Static Test Facility for Small, Expendable, Turbojet Engines. Phase 1 by :
Download or read book Portable Static Test Facility for Small, Expendable, Turbojet Engines. Phase 1 written by and published by . This book was released on 1994 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt: Test Devices, Inc. has completed the preliminary design for the Portable Static Test Facility (PSTF) for small, expendable, turbojet engines (50 - 1000 lb thrust) as part of the Phase I effort under SBIR contract DAAH01-94-C- RO32. The goal of providing a preliminary design for a development and test facility at a reasonable cost, assembled from standard, transportable modules and requiring minimum setup was achieved. During the Phase I activities a detailed analysis was performed that covered the description of engines to be tested, engine test procedures, general test specifications, test facility requirements and design considerations, installation, and engine control and test data requirements. From this a preliminary design for the portable test facility was prepared, plus a conceptual installation design and a preliminary design for the engine control and data system. Turbojet engine testing, Engine test cell, Static test facility, Engine control system, Expendable jet engine, Test cell instrumentation.
Book Synopsis DESIGN CONSIDERATIONS FOR ENCLOSED TURBOFAN/TURBOJET ENGINE TEST CELLS by : EG-1E Gas Turbine Test Facilities and Equipment
Download or read book DESIGN CONSIDERATIONS FOR ENCLOSED TURBOFAN/TURBOJET ENGINE TEST CELLS written by EG-1E Gas Turbine Test Facilities and Equipment and published by . This book was released on 1995 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Information Report (AIR) has been written for individuals associated with the ground-level testing of large and small gas turbine engines and particularly for those who might be interested in upgrading their existing or acquiring new test cell facilities.
Author :Canada. Energy, Mines and Resources Canada Publisher :Energy, Mines and Resources Canada ISBN 13 : Total Pages :190 pages Book Rating :4.:/5 (31 download)
Book Synopsis Compressors and Turbines by : Canada. Energy, Mines and Resources Canada
Download or read book Compressors and Turbines written by Canada. Energy, Mines and Resources Canada and published by Energy, Mines and Resources Canada. This book was released on 1987 with total page 190 pages. Available in PDF, EPUB and Kindle. Book excerpt: Manual on energy management for compressors and turbines, introducing these pieces of equipment as used in the industrial, commercial and institutional sectors; defining methods of determining the approximate energy consumption; providing potential energy and cost savings available; and providing a series of worksheets to establish a standard method of calculating energy and cost savings. Also included is a glossary and specific details for energy calculations for electric motor drives and alternatives.
Book Synopsis Design, Construction, and Operation of a Laboratory Test Facility for Small Turbines and Compressors by : Andrew Vito De Stena
Download or read book Design, Construction, and Operation of a Laboratory Test Facility for Small Turbines and Compressors written by Andrew Vito De Stena and published by . This book was released on 1959 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on with total page 994 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book STAR written by and published by . This book was released on 1973 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design and Operation of a Counter-rotating Aspirated Compressor Blowdown Test Facility by : David Vickery Parker
Download or read book Design and Operation of a Counter-rotating Aspirated Compressor Blowdown Test Facility written by David Vickery Parker and published by . This book was released on 2005 with total page 141 pages. Available in PDF, EPUB and Kindle. Book excerpt: A unique counter-rotating aspirated compressor was tested in a blowdown facility at the Gas Turbine Laboratory at MIT. The facility expanded on experience from previous blowdown turbine and blowdown compressor experiments. Advances in thermocouple and facility designs enabled efficiency estimates through total temperature and total pressure measurements. The facility was designed to provide at least 100 ms of available test time, approximately a factor of five greater than previous blowdown compressor facilities. The adiabatic core efficiency of the compressor was estimated with an uncertainty of 0.8% and the corrected flow was estimated with an uncertainty of 1.0%. The compressor was tested at several operating conditions and two speed lines were partially mapped. The maximum measured total pressure ratio across the two stages was 3.02 to 1. The measured adiabatic efficiency for that point was 0.885. The span-wise total pressure, total temperature, and efficiency profiles were compared to the predicted profiles for runs with the corrected speeds of the two rotors at 90% of design and 100% design. There appears to be reasonable agreement between the predictions and the measurements.
Book Synopsis Systems Study of a Compressor Research Test Facility by : H. N. Ketola
Download or read book Systems Study of a Compressor Research Test Facility written by H. N. Ketola and published by . This book was released on 1967 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was made to define functional requirements and establish design criteria for a new compressor research test facility. The program resulted in the selection of a facility configuration along with recommendations for implementing its design and construction. It was found that a facility capable of testing all future fans and compressors would not be economically attractive. The initial design of the facility should be for open cycle operation with an eventual expansion to closed cycle operation. The recommended closed cycle design makes maximum use of existing equipment while providing a wide range of operational capability. Cost tradeoff studies also favored the recommended configuration. A digital simulation model of the selected facility capable of reproducing both off design and dynamic performance was developed and delivered to the Air Force to allow for further investigations. (Author).
Book Synopsis Redesign of the Low Speed Three Stage Axial Flow Compressor Test Facility by : Michael Hans Vavra
Download or read book Redesign of the Low Speed Three Stage Axial Flow Compressor Test Facility written by Michael Hans Vavra and published by . This book was released on 1973 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flow configuration of an existing low-speed, axial flow compressor test facility at the Turbopropulsion Laboratory, Naval Postgarduate School, Monterey, California, was redesigned in order to improve compressor inlet velocity distribution, improve mass flow measurement, and increase the power input. The design of the new configuration, consisting of an inlet nozzle, ducting, throttling device upstream of the compressor, and a diffusor downstream of it, is reported. The redesign is based on using the existing free-vortex type and solid-body type bladings, and the newly designed symmetrical blading. (Author).
Book Synopsis Design of a Small Engine Test Facility by : Brian Wayne Hampton
Download or read book Design of a Small Engine Test Facility written by Brian Wayne Hampton and published by . This book was released on 1995 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Gas Turbine Performance by : Philip P. Walsh
Download or read book Gas Turbine Performance written by Philip P. Walsh and published by John Wiley & Sons. This book was released on 2008-04-15 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt: A significant addition to the literature on gas turbine technology, the second edition of Gas Turbine Performance is a lengthy text covering product advances and technological developments. Including extensive figures, charts, tables and formulae, this book will interest everyone concerned with gas turbine technology, whether they are designers, marketing staff or users.
Book Synopsis Small, low-cost, expendable turbojet engine by : Robert P. Dengler
Download or read book Small, low-cost, expendable turbojet engine written by Robert P. Dengler and published by . This book was released on 1976 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Utilization of a Dual Spool Compressor Test Facility to Aid Development of Turbofan Engines by : A. Walter Stubner
Download or read book Utilization of a Dual Spool Compressor Test Facility to Aid Development of Turbofan Engines written by A. Walter Stubner and published by . This book was released on 1974 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Congressional Record by : United States. Congress
Download or read book Congressional Record written by United States. Congress and published by . This book was released on 1967 with total page 1434 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Production Test Facilities for Turbojet and Turbofan Engines - 1975 to 1995 by : David Laurence Bailey
Download or read book Production Test Facilities for Turbojet and Turbofan Engines - 1975 to 1995 written by David Laurence Bailey and published by . This book was released on 1972 with total page 83 pages. Available in PDF, EPUB and Kindle. Book excerpt: A review is made of test cell design options in order to identify characteristics of jet engine test facilities to be constructed in the 1970's and designed to be operable for a minimum of twenty years. The necessity of providing replacements for many current facilities is documented, and the factors which will ensure future production capability and economic feasibility are detailed. Present turbine engines are reviewed and projections of future engines and aircraft are made. A confidential supplement is available for qualified recipients. (Author).
Download or read book Jet Web written by Dietrich Eckardt and published by Springer Nature. This book was released on 2023-02-03 with total page 748 pages. Available in PDF, EPUB and Kindle. Book excerpt: The present book describes the development history of turbojet engines, mainly in the web-type triangle Great Britain (USA) - Germany - Switzerland from early beginnings in the 1920s up to the first practical usage in the 1950s, before the still unbroken, grand impact of aero propulsion technology on global air traffic started. interconnections are highlighted, including the considerable impact of axial-flow compressor design know-how of the Swiss/German company BBC Brown Boveri & Cie. on both sides. The author reveals significant undercurrents which led to a considerable exchange, and thus change in understanding of the technical-historical perspective, especially in the decisive years before WWII, and thus closes gaps in the unilateral views of this ground-breaking technical advancement. The old ‘Whittle vs. von Ohain Saga’ is not repeated in full, but addressed in sufficient detail to understand the considerably enlarged narrative scope.
