The design of axial inducers for turbo-pumps

February 1958

Bibliographic Details
Main Author: Stenning, Alan H. (Alan Hugh)
Other Authors: Massachusetts Institute of Technology. Gas Turbine Laboratory
Format: Technical Report
Published: Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1958] 2016
Subjects:
Online Access:http://hdl.handle.net/1721.1/104702
_version_ 1826188945459773440
author Stenning, Alan H. (Alan Hugh)
author2 Massachusetts Institute of Technology. Gas Turbine Laboratory
author_facet Massachusetts Institute of Technology. Gas Turbine Laboratory
Stenning, Alan H. (Alan Hugh)
author_sort Stenning, Alan H. (Alan Hugh)
collection MIT
description February 1958
first_indexed 2024-09-23T08:07:26Z
format Technical Report
id mit-1721.1/104702
institution Massachusetts Institute of Technology
last_indexed 2024-09-23T08:07:26Z
publishDate 2016
publisher Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1958]
record_format dspace
spelling mit-1721.1/1047022019-04-09T16:47:17Z The design of axial inducers for turbo-pumps Stenning, Alan H. (Alan Hugh) Massachusetts Institute of Technology. Gas Turbine Laboratory TJ778.M41 G24 no.44 Pumping machinery February 1958 Includes bibliographical references (page 15) In many turbopump applications it is desirable to run the pump at the highest possible speed to minimise the size and weight of the unit and facilitate matching with a drive turbine. Frequently, a limit on rotational speed is imposed by pump cavitation with its associated deterioration in performance and structural damage. For conventional single sided centrifugal pumps cavitation occurs when the suction specific speed ... exceeds 8-10,000 (1) so that for such pumps the maximum rotational speed without cavitation is determined by the flow and the suction head available. To permit operation at higher speeds an inducer or boost pump may be mounted in front of the main pump (f ig. 1). A typical axial inducer is simply a very lightly loaded axial pump which raises the pressure of the fluid sufficiently to avoid cavitation in the main pump. It has been found possible to operate inducers successfully at suction specific speeds up to 30,000, so that considerable reductions in total pump weight can be achieved when they are employed. Of course, since the inducer is simply a lightly loaded pump which is capable of handling a cavitating fluid, the functions of inducer and main pump may be combined by designing the main pump so that the inlet is lightly loaded. However, it is not always convenient to do this and in many applications conventional centrifugal pumps are still used, preceded by a separate inducer. The objective of this report is to put the design of such inducers on a rational basis by developing a method of calculating blade shapes for the optimum pressure distribution. Under the sponsorship of General Electric Company Westinghouse Electric Corporation Allison Division of the General Motors Corporation 2016-10-06T21:22:03Z 2016-10-06T21:22:03Z 1958 Technical Report http://hdl.handle.net/1721.1/104702 14173572 GTL report #44 15, [7] pages application/pdf Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1958]
spellingShingle TJ778.M41 G24 no.44
Pumping machinery
Stenning, Alan H. (Alan Hugh)
The design of axial inducers for turbo-pumps
title The design of axial inducers for turbo-pumps
title_full The design of axial inducers for turbo-pumps
title_fullStr The design of axial inducers for turbo-pumps
title_full_unstemmed The design of axial inducers for turbo-pumps
title_short The design of axial inducers for turbo-pumps
title_sort design of axial inducers for turbo pumps
topic TJ778.M41 G24 no.44
Pumping machinery
url http://hdl.handle.net/1721.1/104702
work_keys_str_mv AT stenningalanhalanhugh thedesignofaxialinducersforturbopumps
AT stenningalanhalanhugh designofaxialinducersforturbopumps