|
US2307789A
|
|
Process relating to the operation of explosion turbines
|
|
US2316813A
|
|
Bearer for the stationary vanes of rotary motors
|
|
US2413324A
|
|
Gas purifying apparatus
|
|
US2266600A
|
|
Arrangement for reducing temperature stresses in the end and corner portions of castings
|
|
US2221816A
|
|
Cooled nozzle segment for combustion turbines
|
|
US2256479A
|
|
Blade for rotary machines operated by high temperature media
|
|
US2257745A
|
|
Explosion turbine and method of operating same
|
|
US2207762A
|
|
Process for operating combustion turbines and apparatus therefor
|
|
US2339779A
|
|
Liquid cooled, multiringed turbine rotor
|
|
US2217694A
|
|
Method and apparatus for charging elongated explosion chamber
|
|
US2271642A
|
|
Method and apparatus for purifying gases
|
|
US2231912A
|
|
Method and apparatus for charging explosion chambers with precompressed operating media
|
|
US2100360A
|
|
Nozzle channel construction
|
|
US2118814A
|
|
Combustion engine power plant for driving vehicles
|
|
US2131047A
|
|
Method and apparatus for controlling the ignition in explosion chambers
|
|
US2063928A
|
|
Heat exchange with explosion gases
|
|
US2086553A
|
|
Apparatus for carrying the peak loads of power plants
|
|
US2049446A
|
|
Explosion turbine with full admission high speed rotor
|
|
US2040090A
|
|
Method and apparatus for heat interchange with compressed gases
|
|
US2095984A
|
|
Explosion turbine plant
|
