United States Patent 2735612
US Patent References:
Intake-manifold
- - 1333142

Device for conveying gaseous streams
- - 2017043

Air conditioning conduit fitting
- - 2216046

Airplane construction
- - 2340195

Turbine apparatus
- - 2474258


Publication Date:
02/21/1956
View Patent Images:
Download PDF 2735612 pdf       PDF help
Export Citation:
Click for automatic bibliography generation
Primary Class:
415/208.100
Other Classes:
415/914, 415/199.500, 138/39, 138/111, 415/183
International Classes:
F01D5/14; F02C7/04
US Patent References:
2503973Air intake arrangement for supersonic aircraft
2527971Axial-flow compressor
2575682Reaction propulsion aircraft power plant having independently rotating compressor and turbine blading stages
2648492Gas turbine incorporating compressor
2648493Compressor
2650752Boundary layer control in blowers
Foreign References:
GB564336A
GB596784A
FR988736A