Add to ORKGA damping seal between a high speed rotor member and stator member that separates pressurized fluid compartments is described. It is characterized by the rotor member having a smooth outer surface and the stator member having its bore surface roughened by a plurality of pockets or depressions
LecturePg. 55-64The rotordynamic and leaking characteristics of two types of gas damper seals, honey...
Balance piston gas seals restrict leakage at the discharge of centrifugal compressors. There are mul...
Experiments conducted at the Texas A&M Turbomachinery Laboratory and field applications have shown t...
LecturePg. 59-72A new type of labyrinth seal that reduces cross coupled rotor forces and produces a ...
High side loads reduce the life of the Space Shuttle Main Engine (SSME) High Pressure Oxygen Turbopu...
A dual clearance hydrodynamic liquid squeeze film damper for a gas turbine engine is described. Unde...
A theory is presented, based on a simple modification of Hirs' turbulent lubrication equations, to a...
A rotor seal is proposed that restricts leakage like a labyrinth seal, but extends the stabilizing s...
A gas path seal suitable for use with a turbine engine or compressor is provided. A shroud wearable ...
A seal assembly is provided for reducing the escape of fluids from between a housing and a shaft rot...
A damper seal (310) and method of sealing and damping a rotating shaft (312) are disclosed. The damp...
LecturePg. 9-14The rotating equipment industry's ever-increasing demand for efficient, safe and reli...
A damper seal (10) and method of sealing and damping a rotating shaft (12) is provided with a stator...
The paper presents theoretical investigations that deal with the steady state mass flow rate, labyri...
Due to the character of the original source materials and the nature of batch digitization, quality ...
LecturePg. 55-64The rotordynamic and leaking characteristics of two types of gas damper seals, honey...
Balance piston gas seals restrict leakage at the discharge of centrifugal compressors. There are mul...
Experiments conducted at the Texas A&M Turbomachinery Laboratory and field applications have shown t...
LecturePg. 59-72A new type of labyrinth seal that reduces cross coupled rotor forces and produces a ...
High side loads reduce the life of the Space Shuttle Main Engine (SSME) High Pressure Oxygen Turbopu...
A dual clearance hydrodynamic liquid squeeze film damper for a gas turbine engine is described. Unde...
A theory is presented, based on a simple modification of Hirs' turbulent lubrication equations, to a...
A rotor seal is proposed that restricts leakage like a labyrinth seal, but extends the stabilizing s...
A gas path seal suitable for use with a turbine engine or compressor is provided. A shroud wearable ...
A seal assembly is provided for reducing the escape of fluids from between a housing and a shaft rot...
A damper seal (310) and method of sealing and damping a rotating shaft (312) are disclosed. The damp...
LecturePg. 9-14The rotating equipment industry's ever-increasing demand for efficient, safe and reli...
A damper seal (10) and method of sealing and damping a rotating shaft (12) is provided with a stator...
The paper presents theoretical investigations that deal with the steady state mass flow rate, labyri...
Due to the character of the original source materials and the nature of batch digitization, quality ...
LecturePg. 55-64The rotordynamic and leaking characteristics of two types of gas damper seals, honey...
Balance piston gas seals restrict leakage at the discharge of centrifugal compressors. There are mul...
Experiments conducted at the Texas A&M Turbomachinery Laboratory and field applications have shown t...