reply to post by tezzajw
tezz, you persist in playing such a silly game, it doesn't put you in a very good light, in other's eyes, does it?
This post, for example, is as silly as if I told you that a V-6 reciprocating car engine that breaks a connecting rod might 'throw' that rod through
the side of the crankcase and you insisted on seeing the charts and diagrams to prove it! Seeing an example of how an engine works, and having even a
basic concept of physics that anyone who grew up on planet Earth would have, should be sufficient to understand the concepts of centripetal and
centrifugal force.
I provided a video, with narration, showing an engine test to see what happens when a large fan blade lets loose...your silliness may seem cute to
you, but it would not be tolerated in most segments of civilised society, and
especially in a court of law, which is the game you are
attempting here, it would seem.
Since I had a few minutes of time, here's a narrative to indulge you. Hope it's OK? Of course, you can claim that every example cited has no
'chain of custody', but you don't want to look foolish, do you?
This is from a discussion of a certain model engine from a different manufacturer, but the principles behind a GE-built CF6 and the P/W engines on the
UAL93 accident airplane are the same.
www.upi.com...#
Uncontained failures are among the most dangerous types of jet engine malfunctions because material inside the engine can break off and
penetrate the housing, also called the cowl or shroud, that contains the engine's internal components. The debris could then strike portions of
the attachment holding the engine or other parts of a plane's wings, tail or fuselage.
It is just this type of in-flight failure than caused the crash of a United Airlines DC-10 during a landing at Sioux City, Iowa on July 19, 1989. In
that event, a CF6 installed in the aircraft's tail experienced what former National Transportation Safety Board Chairman Jim Hall called "a
catastrophic failure" while the plane was at 37,000 feet. During the emergency landing attempt, 111 people of the 296 aboard were killed.
"Fractured segments from the center engine's fan hub, blades and shrapnel perforated the aircraft's horizontal stabilizer and severed hydraulic
lines to all three hydraulic systems," Hall said during a 1997 speech in Chattanooga, Tenn., delivered four years to the day before Monday's
crash.
The NTSB investigation later revealed the failure of the CF6 started with a tiny, microscopic crack in the engine's hub that occurred years before
the 1989 accident. NTSB documents also showed the engine had been inspected six times before the crash and never detected. The cause of the crack,
which grew to one-half inch in length by the time of the Sioux City accident, was metal fatigue.
In its analysis of the 61 CF6 uncontained failures, the FAA review stated in one variant of the engine, the CF6-50, there have been 16 events "where
the debris escaped the engine case, 12 where debris escaped both the case and the nacelle, and nine where the debris escaped the entire engine area
and struck other parts of the aircraft."
The other engine variant, the CF6-80C2 had experienced 16 events where "the debris escaped the engine case, six where the debris escaped both the
case and nacelle, and two where the debris struck the aircraft." Nacelles are the housing that holds both the engine and its exterior casing.
Other uncontained failures involving CF6 engines include:
-An Air France Boeing 747, which sustained an uncontained failure of a CF6 when the engine was fired up at Charles de Gaulle Airport on March 24,
1996. Fractured bolts found after the incident caused the failure.
-A United Airlines DC-10, which sustained an uncontained engine failure during its take-off roll from Chicago's O'Hare International Airport on May
1, 1995. According to an NTSB report, the flight crew heard a loud crack and successfully aborted the take-off. Later inspection revealed fractured
bolts and other parts had broken off of the engine.
-A Continental Airlines DC-10 suffered a failure during takeoff from Narita International Airport in Tokyo in March 1995. NTSB's investigation
revealed fragments of the CF6's turbine blades had broken off and penetrated the engine's housing.
Now, as to
your silliness, please provide evidence to discredit the foregoing.
As to charts, graphs and calculations? I'll leave that to you, since apparently it's so important to your understanding. People with logical,
rational thinking skills can understand the basics, without exact details being needed.
Can you?