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IgnitionleadsInlet guide vanes
to work with a range of wire sizes(passive) are designedInlet guides
to pre - rotate or spin the air in the direction of fan / compressor rotation(passive) are designedDampers ‘ IGVs ( Inlet Guide Vanes
commandswill causethe inlet guide vane
to guide the inlet air into the fan in the direction of impeller rotation and , therefore , improve performance , resulting in somewhat better energy efficiency than damper controlled operation(passive) are designedThe inlet guide vanes
the low pressure turbine ( LPT ) stage , and the EGVs(passive) have been designedThe inlet guide vanes ( IGVs
to direct the airflow onto the last stage rotors at an appropriate angle of attack(passive) are designedThe inlet guide vanes
to direct the airflow onto the first stage rotors at an appropriate angle of attack(passive) are designedThe inlet guide vanes
another JASCdesignedInlet Guide Vane Actuator
to direct the airflow onto the last stage rotors at an high angle of attack(passive) are designedThe inlet guide vanes
to ensure maximum centrifugal action for the gas entering the cyclone on its spiraling path down the cyclone towards the dust discharge points resulting in an increase in the collection efficiency of the Multi Cyclones(passive) are specifically designedThe inlet guide vanes
to direct the airflow onto the first stage rotors at an high angle of attack(passive) are designedThe inlet guide vanes
16a(passive) are causedThe inlet guide vanes
at nine vane setting angles for the 100 and 120 percent of design speedssetat nine vane setting angles for the 100 and 120 percent of design speeds
into a core engine flow pathleadinginto a core engine flow path
Concepts of Real - Time Embedded SystemsdesigningConcepts of Real - Time Embedded Systems
to the compressor sectionleadingto the compressor section
a swirling air stream into the second impellercreatinga swirling air stream into the second impeller
products with systemon - a - chip SoC type solutions inlet guide vanes designing inet large Field Programmable Gate Arraydesigningproducts with systemon - a - chip SoC type solutions inlet guide vanes designing inet large Field Programmable Gate Array
on compressors 3 and 35 , and the firing rate of combustor 7settingon compressors 3 and 35 , and the firing rate of combustor 7
to facilitate the transition of the fluid horizontal momentum to downward momentum through useare designedto facilitate the transition of the fluid horizontal momentum to downward momentum through use
to present the first stage axial compressor with air at the proper AOAdesignedto present the first stage axial compressor with air at the proper AOA
at a 0 ° angle ( shown in solid linessetat a 0 ° angle ( shown in solid lines
vanes to coupled pneumatically operated positioning ring stereoscopic 182 control signals that the computer is generated to be sent to a ( not shown ... FIG . 11 and figuresetvanes to coupled pneumatically operated positioning ring stereoscopic 182 control signals that the computer is generated to be sent to a ( not shown ... FIG . 11 and figure
to allow the minimum flow necessary to match or exceed the pressure of the flow from the turbine compressor 30setto allow the minimum flow necessary to match or exceed the pressure of the flow from the turbine compressor 30
ice forming thereto preventice forming there
to allow the minimum flow necessary to provide any necessary remainder flow not provided by the main air compressor 12 to the master turbine combustor 32setto allow the minimum flow necessary to provide any necessary remainder flow not provided by the main air compressor 12 to the master turbine combustor 32
a much bigger portioncontributea much bigger portion
to allow the minimum flow necessary to match or exceed the pressure of the flow from the master turbine compressor 30setto allow the minimum flow necessary to match or exceed the pressure of the flow from the master turbine compressor 30
to allow the minimum flow necessary to provide any necessary remainder flow not provided by the main air compressor 12 to the turbine combustor 32setto allow the minimum flow necessary to provide any necessary remainder flow not provided by the main air compressor 12 to the turbine combustor 32
in the basic MS5001 M design which has led to today 's modern compressorsresultingin the basic MS5001 M design which has led to today 's modern compressors
at nine anglessetat nine angles
to a predetermined full open condition and compressor capacityare setto a predetermined full open condition and compressor capacity
to some maximum open position and the rotational speed of the impeller at the lowest possible speed that does not induce surge conditionssetto some maximum open position and the rotational speed of the impeller at the lowest possible speed that does not induce surge conditions
Microsoft Excel file to a Shapefile for Use in ArcGISdesigningMicrosoft Excel file to a Shapefile for Use in ArcGIS
el diagnóstico temprano y preciso del embarazo ectópicodesigningel diagnóstico temprano y preciso del embarazo ectópico
to allow the minimum flow necessary to provide any necessary remainder flow not provided by the main air compressor 12 to the slave turbine combustor 72setto allow the minimum flow necessary to provide any necessary remainder flow not provided by the main air compressor 12 to the slave turbine combustor 72