Advances in Cryogenic Engineering 1963
DOI: 10.1007/978-1-4757-0528-7_26
|View full text |Cite
|
Sign up to set email alerts
|

A Refrigeration System Incorporating a Low-Capacity, High-Speed, Gas-Bearing-Supported Expansion Turbine

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

1965
1965
2019
2019

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 5 publications
(2 citation statements)
references
References 2 publications
0
2
0
Order By: Relevance
“…Both oil lubricated and pressurised gas lubricated bearings have been used (Patzelt et al 1973). A turbine developed by National Bureau of Standards, Boulder, Colarado, USA, has a shaft diameter of 8 mm and a design speed of 600,000 r.p.m, at 30 K inlet temperature (Mann et al 1963). Sixsmith & Wilson (1964) describe the turboexpander suitable for helium which operates at 500,000 r.p.m, using externally pressurised gas lubricated bearings.…”
Section: 2b Joule-thomson Ut) Liquefier~refrigeratormentioning
confidence: 99%
“…Both oil lubricated and pressurised gas lubricated bearings have been used (Patzelt et al 1973). A turbine developed by National Bureau of Standards, Boulder, Colarado, USA, has a shaft diameter of 8 mm and a design speed of 600,000 r.p.m, at 30 K inlet temperature (Mann et al 1963). Sixsmith & Wilson (1964) describe the turboexpander suitable for helium which operates at 500,000 r.p.m, using externally pressurised gas lubricated bearings.…”
Section: 2b Joule-thomson Ut) Liquefier~refrigeratormentioning
confidence: 99%
“…A previously reported [4] single stage impulse turbine was used for this purpose in a test apparatus illustrated in Fig. A previously reported [4] single stage impulse turbine was used for this purpose in a test apparatus illustrated in Fig.…”
Section: Fig I Turbine Test Apparatusmentioning
confidence: 99%