Boron/epoxy and graphite/epoxy composite blades were impacted in a rotating whirligig facility with conditions closely simulating those which might be experienced by a STOL engine impacted with various foreign objects. The tip speed of the rotating blades was 800 feet per second. The blades were impacted with simulated birds, real birds, ice balls, and gravel. The results of composite blade impact tests were compared with a titanium blade tested under similar conditions. Neither composite material indicated a clear superiority over the other. Blades made from both composite materials showed more damage than the titanium blades
Processing procedures were developed to enhance boron/aluminum bond behavior and foreign object dama...
Structural and dynamic analyses are presented for a shroudless, hollow titanium fan blade proposed f...
Six filament-wound, composite spar-shell fan blades were impact tested in a whirligig relative to fo...
The resistance of current-design Pratt and Whitney Aircraft low aspect ratio advanced fiber reinforc...
The results of impact tests on large, fiber composite fan blades for aircraft turbofan engine applic...
Composite spar-shell fan blades for a 1.83 meter (6 feet) diameter fan stage were fabricated and tes...
The results of a 20-month program, designed to investigate parameters which effect the foreign objec...
Improved resistance to foreign object damage was demonstrated for hybrid composite simulated blade s...
Application of polymer matrix composite materials for jet engine fan blades is becoming attractive a...
Efforts to improve the impact resistance of B/Al are reviewed and analyzed. Thin sheet Charpy and Iz...
Recent developments in the analysis of high velocity impact of composite blades are described, using...
The development of containment concepts for use with large composite fan blades, taking into account...
The technical program was comprised of two technical tasks. Task 1 encompassed the preliminary boron...
Resin matrix composites having improved resistance to foreign object damage in gas turbine engine fa...
Application of polymer matrix composite materials for jet engine fan blades is becoming attractive a...
Processing procedures were developed to enhance boron/aluminum bond behavior and foreign object dama...
Structural and dynamic analyses are presented for a shroudless, hollow titanium fan blade proposed f...
Six filament-wound, composite spar-shell fan blades were impact tested in a whirligig relative to fo...
The resistance of current-design Pratt and Whitney Aircraft low aspect ratio advanced fiber reinforc...
The results of impact tests on large, fiber composite fan blades for aircraft turbofan engine applic...
Composite spar-shell fan blades for a 1.83 meter (6 feet) diameter fan stage were fabricated and tes...
The results of a 20-month program, designed to investigate parameters which effect the foreign objec...
Improved resistance to foreign object damage was demonstrated for hybrid composite simulated blade s...
Application of polymer matrix composite materials for jet engine fan blades is becoming attractive a...
Efforts to improve the impact resistance of B/Al are reviewed and analyzed. Thin sheet Charpy and Iz...
Recent developments in the analysis of high velocity impact of composite blades are described, using...
The development of containment concepts for use with large composite fan blades, taking into account...
The technical program was comprised of two technical tasks. Task 1 encompassed the preliminary boron...
Resin matrix composites having improved resistance to foreign object damage in gas turbine engine fa...
Application of polymer matrix composite materials for jet engine fan blades is becoming attractive a...
Processing procedures were developed to enhance boron/aluminum bond behavior and foreign object dama...
Structural and dynamic analyses are presented for a shroudless, hollow titanium fan blade proposed f...
Six filament-wound, composite spar-shell fan blades were impact tested in a whirligig relative to fo...