Hybrid combinations of hydrostatic and ball bearings can improve bearing performance for liquid hydrogen and liquid oxygen turbopumps. Analytic studies were conducted to optimize hybrid bearing designs for the SSME-type turbopump conditions. A method to empirically determine damping coefficients was devised. Four hybrid bearing configurations were designed, and three were fabricated. Six hybrid and hydrostatic-only bearing configurations will be tested for steady-state and transient performance, and quantification of damping coefficients. The initial tests were conducted with the liquid hydrogen bearing
There is a spectrum of pressure-fed journal bearings ranging from the purely hydrostatic bearing cha...
Experiments were performed on a Hybrid Magnetic Bearing designed for cryogenic applications such as ...
The mechanism of centering stiffness in seals. Force coefficients for short-length pressure seals. D...
Data are presented for two different experimental programs which were conducted to investigate the c...
A hybrid hydrostatic bearing was designed to operate in liquid hydrogen at speeds to 80,000 rpm and ...
A high speed, high pressure liquid hydrogen turbopump was designed, fabricated, and tested under a p...
A new fluid film bearing package has been tested in the Space Shuttle Main Engine (SSME) High Pressu...
Most high speed cryogenic turbopumps for liquid propulsion rocket engines currently use ball or roll...
The service life of the Space Shuttle Main Engine (SSME) turbomachinery bearings was a predominant f...
The space shuttle main engine (SSME) high-pressure oxygen turbopumps (HPOTP) have not experienced th...
Evaluating series hybrid bearing concept by testing lubricated fluid film thrust bearing at high spe...
The life requirement for the angular contact ball bearings in the Space Shuttle Main Engine (SSME) h...
The design of 20-mm bore ball bearings is described for cryogenic turbo-machinery applications, oper...
In the paper authors undertake the design of hydrostatic bearings and hybrid bearings for a specific ...
For truly reusable rocket propulsion systems, the next generation first-stage engines have to ensure...
There is a spectrum of pressure-fed journal bearings ranging from the purely hydrostatic bearing cha...
Experiments were performed on a Hybrid Magnetic Bearing designed for cryogenic applications such as ...
The mechanism of centering stiffness in seals. Force coefficients for short-length pressure seals. D...
Data are presented for two different experimental programs which were conducted to investigate the c...
A hybrid hydrostatic bearing was designed to operate in liquid hydrogen at speeds to 80,000 rpm and ...
A high speed, high pressure liquid hydrogen turbopump was designed, fabricated, and tested under a p...
A new fluid film bearing package has been tested in the Space Shuttle Main Engine (SSME) High Pressu...
Most high speed cryogenic turbopumps for liquid propulsion rocket engines currently use ball or roll...
The service life of the Space Shuttle Main Engine (SSME) turbomachinery bearings was a predominant f...
The space shuttle main engine (SSME) high-pressure oxygen turbopumps (HPOTP) have not experienced th...
Evaluating series hybrid bearing concept by testing lubricated fluid film thrust bearing at high spe...
The life requirement for the angular contact ball bearings in the Space Shuttle Main Engine (SSME) h...
The design of 20-mm bore ball bearings is described for cryogenic turbo-machinery applications, oper...
In the paper authors undertake the design of hydrostatic bearings and hybrid bearings for a specific ...
For truly reusable rocket propulsion systems, the next generation first-stage engines have to ensure...
There is a spectrum of pressure-fed journal bearings ranging from the purely hydrostatic bearing cha...
Experiments were performed on a Hybrid Magnetic Bearing designed for cryogenic applications such as ...
The mechanism of centering stiffness in seals. Force coefficients for short-length pressure seals. D...