The work described consists of two parts. In the first part, a survey is performed to assess the state of the art in rotor balancing technology as it applies to Army gas turbine engines and associated power transmission hardware. The second part evaluates thermal spray processes for balancing weight addition in an automated balancing procedure. The industry survey reveals that: (1) computerized balancing equipment is valuable to reduce errors, improve balance quality, and provide documentation; (2) slow-speed balancing is used exclusively, with no forseeable need for production high-speed balancing; (3) automated procedures are desired; and (4) thermal spray balancing is viewed with cautious optimism whereas laser balancing is viewed with c...
Rotary dynamics test facility investigates and corrects imbalances in rotary components at speeds up...
Tutorialpg. 253-258Most turbomachinery users refer to bearing vibration as one of their major indic...
The paper investigates the use of compensating balancing sleeves positioned at the shaft’s end for t...
The NASA Lewis Research Center has developed and implemented a time-efficient methodology for dynami...
Tutorialpg. 147-150The details of shop balancing flexible shaft rotors are discussed with an explana...
Test rig for predicting thermal stress cracking in turbine stator or rotor blade
Research was conducted to demonstrate the ability of influence coefficient based multispeed balancin...
LecturePg. 67-76This paper describes the design modifications and active balancing on a 19,000 hp i...
Experimental tests were conducted to demonstrate the ability of the influence coefficient method to ...
Tutorialpg. 209-214The mechanics of balancing, including details concerning tolerances and specifica...
The effects of coating TBC on a CF6-50 stage 2 high-pressure turbine blade were analyzed with respec...
A prototype high speed balancing system was developed for assembled gas turbine engine modules. The ...
Technical BriefsWhen unbalance induced vibrations exceed allowable limits, a more accurate system ba...
The work performed under Contracts NAS3-23929 and NAS3-24633 is presented. MTI evaluated the feasibi...
The practical aspects of balancing real, flexible rotors were investigated through inclusion of roto...
Rotary dynamics test facility investigates and corrects imbalances in rotary components at speeds up...
Tutorialpg. 253-258Most turbomachinery users refer to bearing vibration as one of their major indic...
The paper investigates the use of compensating balancing sleeves positioned at the shaft’s end for t...
The NASA Lewis Research Center has developed and implemented a time-efficient methodology for dynami...
Tutorialpg. 147-150The details of shop balancing flexible shaft rotors are discussed with an explana...
Test rig for predicting thermal stress cracking in turbine stator or rotor blade
Research was conducted to demonstrate the ability of influence coefficient based multispeed balancin...
LecturePg. 67-76This paper describes the design modifications and active balancing on a 19,000 hp i...
Experimental tests were conducted to demonstrate the ability of the influence coefficient method to ...
Tutorialpg. 209-214The mechanics of balancing, including details concerning tolerances and specifica...
The effects of coating TBC on a CF6-50 stage 2 high-pressure turbine blade were analyzed with respec...
A prototype high speed balancing system was developed for assembled gas turbine engine modules. The ...
Technical BriefsWhen unbalance induced vibrations exceed allowable limits, a more accurate system ba...
The work performed under Contracts NAS3-23929 and NAS3-24633 is presented. MTI evaluated the feasibi...
The practical aspects of balancing real, flexible rotors were investigated through inclusion of roto...
Rotary dynamics test facility investigates and corrects imbalances in rotary components at speeds up...
Tutorialpg. 253-258Most turbomachinery users refer to bearing vibration as one of their major indic...
The paper investigates the use of compensating balancing sleeves positioned at the shaft’s end for t...