|
US3283497A
|
|
Burner for gas turbine engine
|
|
US3324655A
|
|
Gas turbine engine with controllable power output
|
|
US3128063A
|
|
Airfoil with boundary layer control
|
|
US3064327A
|
|
Hose clamp with adjustable closure device
|
|
US3058788A
|
|
Anti-friction bearing
|
|
US3031238A
|
|
Anti-friction bearing assembly
|
|
US3079660A
|
|
Clamp having stamped hook bolt
|
|
US3010172A
|
|
Integrally reinforced v-band clamp
|
|
US3038699A
|
|
Nozzle ring assembly
|
|
US3042430A
|
|
Fast action coupling and clamping assembly
|
|
US2982846A
|
|
Laminated structure and method of fabricating the same
|
|
US3010680A
|
|
Airfoil with boundary layer control
|
|
US3057767A
|
|
Method of making compressor blades
|
|
US2999146A
|
|
Fluid-pervious sheet material
|
|
US2920370A
|
|
Overcenter latch
|
|
US2959377A
|
|
Airfoil structure with boundary layer control means
|
|
US2914918A
|
|
Gas turbine jet engine starter with serially-connected concentrically-arranged combustion chambers
|
