An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket Turbopumps

Abstract There is a consensus in the aerospace field that the development of reusable liquid rockets can effectively reduce the launch expense. The pursuit of a long service life and reutilization highly depends on the bearing components. However, the rolling element bearings (REBs) used in the exis...

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Main Authors: Jimin Xu, Changhuan Li, Xusheng Miao, Cuiping Zhang, Xiaoyang Yuan
Format: Article
Language:English
Published: SpringerOpen 2020-03-01
Series:Chinese Journal of Mechanical Engineering
Subjects:
Online Access:http://link.springer.com/article/10.1186/s10033-020-00442-6
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spelling doaj-1588c735fa25487c9da44f7af18fe6be2020-11-25T02:08:26ZengSpringerOpenChinese Journal of Mechanical Engineering1000-93452192-82582020-03-0133111310.1186/s10033-020-00442-6An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket TurbopumpsJimin Xu0Changhuan Li1Xusheng Miao2Cuiping Zhang3Xiaoyang Yuan4Institute of Tribology, School of Mechanical Engineering, Hefei University of TechnologyAerospace Propulsion Institute, China Aerospace Science and Technology CorporationAerospace Propulsion Institute, China Aerospace Science and Technology CorporationSuperconducting Materials Research Center Laboratory, Northwest Institute for Non-ferrous Metal ResearchKey Laboratory of Education Ministry for Modern Design and Rotor-Bearing System, Xi’an Jiaotong UniversityAbstract There is a consensus in the aerospace field that the development of reusable liquid rockets can effectively reduce the launch expense. The pursuit of a long service life and reutilization highly depends on the bearing components. However, the rolling element bearings (REBs) used in the existing rocket turbopumps present obvious and increasing limitations due to their mechanical contacting mode. For REBs, high rotational speed and long service life are two performance indexes that mutually restrict each other. To go beyond the DN value (the product of the bearing bore and rotational speed) limit of REBs, the major space powers have conducted substantial explorations on the use of new types of bearings to replace the REB. This review discusses, first, the crucial role of bearings in rocket turbopumps and the related structural improvements of REBs. Then, with the prospect of application to the next generation of reusable liquid rocket turbopumps, the bearing candidates investigated by major space powers are summarized comprehensively. These promising alternatives to REBs include fluid-film, foil, and magnetic bearings, together with the novel superconducting compound bearings recently proposed by our team. Our more than ten years of relevant research on fluid-film and magnetic bearings are also introduced. This review is meaningful for the development of long-life and highly reliable bearings to be used in future reusable rocket turbopumps.http://link.springer.com/article/10.1186/s10033-020-00442-6AerospaceReusable liquid rocket turbopumpsRolling element bearingsBearing candidatesReview
collection DOAJ
language English
format Article
sources DOAJ
author Jimin Xu
Changhuan Li
Xusheng Miao
Cuiping Zhang
Xiaoyang Yuan
spellingShingle Jimin Xu
Changhuan Li
Xusheng Miao
Cuiping Zhang
Xiaoyang Yuan
An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket Turbopumps
Chinese Journal of Mechanical Engineering
Aerospace
Reusable liquid rocket turbopumps
Rolling element bearings
Bearing candidates
Review
author_facet Jimin Xu
Changhuan Li
Xusheng Miao
Cuiping Zhang
Xiaoyang Yuan
author_sort Jimin Xu
title An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket Turbopumps
title_short An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket Turbopumps
title_full An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket Turbopumps
title_fullStr An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket Turbopumps
title_full_unstemmed An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket Turbopumps
title_sort overview of bearing candidates for the next generation of reusable liquid rocket turbopumps
publisher SpringerOpen
series Chinese Journal of Mechanical Engineering
issn 1000-9345
2192-8258
publishDate 2020-03-01
description Abstract There is a consensus in the aerospace field that the development of reusable liquid rockets can effectively reduce the launch expense. The pursuit of a long service life and reutilization highly depends on the bearing components. However, the rolling element bearings (REBs) used in the existing rocket turbopumps present obvious and increasing limitations due to their mechanical contacting mode. For REBs, high rotational speed and long service life are two performance indexes that mutually restrict each other. To go beyond the DN value (the product of the bearing bore and rotational speed) limit of REBs, the major space powers have conducted substantial explorations on the use of new types of bearings to replace the REB. This review discusses, first, the crucial role of bearings in rocket turbopumps and the related structural improvements of REBs. Then, with the prospect of application to the next generation of reusable liquid rocket turbopumps, the bearing candidates investigated by major space powers are summarized comprehensively. These promising alternatives to REBs include fluid-film, foil, and magnetic bearings, together with the novel superconducting compound bearings recently proposed by our team. Our more than ten years of relevant research on fluid-film and magnetic bearings are also introduced. This review is meaningful for the development of long-life and highly reliable bearings to be used in future reusable rocket turbopumps.
topic Aerospace
Reusable liquid rocket turbopumps
Rolling element bearings
Bearing candidates
Review
url http://link.springer.com/article/10.1186/s10033-020-00442-6
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