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General Electric 's approach wasto designa single spool 17 stage axial flow compressor with variable stators to prevent rotor blades from stalling
ice ... can causedamage to fan blades , engine compressor stall , or combustor flameout
ice ... a running enginecan causedamage to fan blades ... engine compressor stall , or combustor flameout
a running enginecan causedamage to fan blades , engine compressor stall , or combustor flameout
the manufacturing and installationcauseasymmetric radial clearance which decreased the compressor performance in whole operating range
theoretical basesto designcasing treatments and tip air injection for stall margin extension of axial compressor
both engines ... ice ingestionledto compressor stall , destruction of the compressors and over - temperature of the turbine blades
This damagehad ledto cracking in a compressor blade in the third - stage compressor
a huge venturidesignedto handle excess pressure build - up against the turbo compressor impeller blades
the water injectioncan causedroplet erosion on the first stages of blades of the compressor
A compressor stall ... a jet enginecan resultfrom a stall of the blades within the compressor 's rotor
a running enginecan causeto fan blades , engine compressor stall , or combustor flameout
where the air in the by - pass will slow owncausinga compressor stall at the forward stages of the compressor ( i.e. the fan blades
when severecan causean uneven blade loading of the compressor wheel blades
damagecould leadto stress risers on a couple of the compressor blades
The proceduresleadingto successful design of an axial flow compressor
rods on shutterswill causeindentations on the blades ( where the tilt rod closes onto the blade
Vibrationwill causeuneven cutting of the circumferential edge of the end mill
by Eastman Jacobs and Eugene(passive) designed byNACA eight - stage axial - flow compressor
Eastman Jacobs and Eugene Wasielewski(passive) designed byThe NACA eight - stage axial - flow compressor
to provide balance flow control(passive) are designedFan outlet multi - louver opposed blade dampers
Found condenser fan motor not alignedcausingcondenser fan blade to rub on housing
the nozzle exit area requiredto setan axial compressor running - line
as longdid ... resultin compressor blade stall ( ' surging
airborne particles such as dust , sand , salt , pollen , smog , insects and the like(passive) is caused byThe fouling of the turbine blades in the axial compressor
with UNIVERSAL FITMENT(passive) is designedOscillating Flush Cut Blade
the corrosionresultingfrom sulfidation on the gas turbine compressor blades
by the bending of a spool in the Rolls - Royce Turbomeca RTM322 engine due to uneven cooling after shutdown(passive) caused bycompressor blade rubbing
Factorsinfluencingaxial compressor stalls
This ad(passive) was prompted byThis ad
developed and used in all of the manufactured impellershave been ... designeddeveloped and used in all of the manufactured impellers
This AD(passive) was prompted byThis AD
These stationary components(passive) are setThese stationary components
the whistling(passive) was caused bythe whistling
the whistling(passive) was caused bythe whistling
The engine failure(passive) was caused byThe engine failure
on the basis of airfoil theorydesignedon the basis of airfoil theory
Valve BOV Kit(passive) is designedValve BOV Kit
it to make drag instead of thrust in that region of the bladeare causingit to make drag instead of thrust in that region of the blade
condensationcausedcondensation
for carving marble or other soft stonespecially designedfor carving marble or other soft stone
the conveyed gas to be compressed within a full revolutioncausesthe conveyed gas to be compressed within a full revolution
in cracking ormay resultin cracking or
to the industrydesignedto the industry
in uneven cutsresultingin uneven cuts
on the basis of airfoil theorydesignedon the basis of airfoil theory
a mechanical failure within the compressoreventually causinga mechanical failure within the compressor
The unique combination of surfactants and emulsifiers in Conntect 6000(passive) are specifically designedThe unique combination of surfactants and emulsifiers in Conntect 6000
in a power loss ... and forced landingresultedin a power loss ... and forced landing
to a relatively wider operating range and a better operabilityleadingto a relatively wider operating range and a better operability
for an emergency response liquefied gas transfer applicationsdesignedfor an emergency response liquefied gas transfer applications
for high pressure ratio designedfor high pressure ratio
for high pressure ratiodesignedfor high pressure ratio
9fa gas turbine Eighteen - stage(passive) is designed9fa gas turbine Eighteen - stage
stallingmight ... causestalling