y al mismo tiempo representa el 80% del empuje (trust) total que hace que le avion se desplace.
El flujo del aire primario el cual es el 20% pasa atravez de las diferentes componentes internos de la turbina : Compresores de altas y bajas , La camara de comprension y finalmente a la seccion que realmente hace la funcion de turbina (donde se encuentran un compresor de baja y 4 de alta presion) y luego a la parte final o de escape y en donde se combinan el 80% + el 20% de los distintos procesos.
es reducida y al mismo tiempo hace que las hacen girar los compresores y los abanicos (fans).
5) Hay 5 distintos pasos de compresion (stages) (a) uno de alta presion y 4 de bajas.
6) y finalmente la parte de salida con su distintoscomponentes.
La turbina CFM56 es una turbina donde el aire fluye por diferentes partes
a)El flujo de aire tiene dos vias (a) un 20% pasa atravez de los quemadores y el otro 80% de aire pasa atravez del abanico del frente este 80% se usa para enfriamiento.
Para hacer que un Aeronave se desplace se necesita que el aire se desplace desde el frente hasta la parte tracera de la turbina con una gran fuerza que lo empujes (Trust), esta fuerza es generada al acelerar y comprimir el aire a una gran velocidad atravez del lo interno de la tubina usando determinadas cantidades de abanicos (Fans) los cuales aceleran y comprimen el aire en su trayectoria.
All jet engine also called gas turbines, work on the same principle using the application of Sir Isaac Newton's third law of physics: for every action there is an equal and opposite reaction.
The engine sucks air in at the front with a fan. A compressor raises the pressure of the air. The compressor is made up of fans with many blades and attached to a shaft. The blades compress the air. The compressed air is then sprayed with fuel and an electric spark lights the mixture. The burning gases expand and blast out through the nozzle, at the back of the engine. As the jets of gas shoot backward, the engine and the aircraft are thrust forward.
1) Hold your breath. 2) Copy all of these steps. 3) Go to two other video. 4) Paste it in the comments. If you can do all of this without breathing you just wasted 60* seconds of your life. *Number of seconds can differentiate depending on your internet provider, please see back panel for details.
1700ºC ???? Too much. I think is 1700 K (kelvin degrees). Sorry but aeronautical engineers haven't got that temperature in combustion chamber of jet engines yet...
1700ºC ???? Too much. I think is 1700 K (kelvin degrees). Sorry but aeronautical engineers haven't got that temperature in combustion chamber of jet engines yet...
O motor a jato nada mais é do que um compressor de ar a jato, daí vem o "jato" de turbina a jato, pois ela comprimi ar e o super aquece, junto ao combustível.
na verdade, é exatamente o que o motor dos eu carro faz, quando os pistões comprimem o ar junto a gasolina, depois as velas o inflamam, da vem a explosão que abaixa o pistão e transfere a forma para as rodas.
N1 is the rotation of the fan in front of the engine, the one you can see when you look straight at the front of the engine. It is connected to a shaft that runs through the engine and is turned by a turbine at the aft of the engine.N2 is the rotation speed of the central core. The turbine immediately aft of the burner can receive the highest velocity airflow and turns a turbine that is hidden behind the N1 fan.
bueno el video pero chevere estubiara al menos subtitulado en español para entenderlo mejor.
Saidsneider 1 day ago
y al mismo tiempo representa el 80% del empuje (trust) total que hace que le avion se desplace.
El flujo del aire primario el cual es el 20% pasa atravez de las diferentes componentes internos de la turbina : Compresores de altas y bajas , La camara de comprension y finalmente a la seccion que realmente hace la funcion de turbina (donde se encuentran un compresor de baja y 4 de alta presion) y luego a la parte final o de escape y en donde se combinan el 80% + el 20% de los distintos procesos.
lubime10 6 months ago
es reducida y al mismo tiempo hace que las hacen girar los compresores y los abanicos (fans).
5) Hay 5 distintos pasos de compresion (stages) (a) uno de alta presion y 4 de bajas.
6) y finalmente la parte de salida con su distintoscomponentes.
La turbina CFM56 es una turbina donde el aire fluye por diferentes partes
a)El flujo de aire tiene dos vias (a) un 20% pasa atravez de los quemadores y el otro 80% de aire pasa atravez del abanico del frente este 80% se usa para enfriamiento.
lubime10 6 months ago
Los varios componentes del CF-M56 Son :
1) El abanico (Fan) el cual esta formados por largas paletas (Propelers).
2) Los compresores debajas y alta presiones con 13 fases (stages) los cuales paso a pasoincrementa la presion del aire al fluir atravez ellos.
3) La camara de compresion en el cual el combustible que se injecta es mezclado con el aire y se crea la combustion usando al ignarlo con las bujias.
4)Las bajas y altas turbina de compresion en las cuales la presion del aire caliente es
lubime10 6 months ago
Como funciona una tubina de Avion ?
Para hacer que un Aeronave se desplace se necesita que el aire se desplace desde el frente hasta la parte tracera de la turbina con una gran fuerza que lo empujes (Trust), esta fuerza es generada al acelerar y comprimir el aire a una gran velocidad atravez del lo interno de la tubina usando determinadas cantidades de abanicos (Fans) los cuales aceleran y comprimen el aire en su trayectoria.
lubime10 6 months ago
This has been flagged as spam show
All jet engine also called gas turbines, work on the same principle using the application of Sir Isaac Newton's third law of physics: for every action there is an equal and opposite reaction.
lubime10 6 months ago
The engine sucks air in at the front with a fan. A compressor raises the pressure of the air. The compressor is made up of fans with many blades and attached to a shaft. The blades compress the air. The compressed air is then sprayed with fuel and an electric spark lights the mixture. The burning gases expand and blast out through the nozzle, at the back of the engine. As the jets of gas shoot backward, the engine and the aircraft are thrust forward.
lubime10 6 months ago
Comment removed
lubime10 6 months ago
no ma no le entendi y si me interesa
navegantedefuegojon 7 months ago
ahhh entendi!!!! ""porra nenhuma""
joni13zao 7 months ago
ESTE TAMBIEN ESTA CHIDO!!
wazon206 7 months ago
This has been flagged as spam show
1) Hold your breath. 2) Copy all of these steps. 3) Go to two other video. 4) Paste it in the comments. If you can do all of this without breathing you just wasted 60* seconds of your life. *Number of seconds can differentiate depending on your internet provider, please see back panel for details.
mrelasticband 8 months ago
porra porque não portugues :X
rrobert789456123 9 months ago
This has been flagged as spam show
1700ºC ???? Too much. I think is 1700 K (kelvin degrees). Sorry but aeronautical engineers haven't got that temperature in combustion chamber of jet engines yet...
vortichero 10 months ago
1700ºC ???? Too much. I think is 1700 K (kelvin degrees). Sorry but aeronautical engineers haven't got that temperature in combustion chamber of jet engines yet...
vortichero 10 months ago
@vortichero you mean they lied in the video?
plasmasoro 8 months ago
@plasmasoro Not lying, but exaggerating...
vortichero 8 months ago
I AGRE SIT EM LUES ERERR RAR BE AT.COMO DIZ ALBORGUETTE:POOOORRRRAAAAAAAAAHHHHHHH
giovani737300 10 months ago
O motor a jato nada mais é do que um compressor de ar a jato, daí vem o "jato" de turbina a jato, pois ela comprimi ar e o super aquece, junto ao combustível.
na verdade, é exatamente o que o motor dos eu carro faz, quando os pistões comprimem o ar junto a gasolina, depois as velas o inflamam, da vem a explosão que abaixa o pistão e transfere a forma para as rodas.
BrunoLRck 10 months ago
Muy bueno.
seria mucho mejor si explicase con mas detalle el ciclo brayton que interviene en el proceso
FonseXO6 11 months ago
ansnois ta certo mano poderia pelo menos ter um corno p traduzir esta merda
Escobar896 11 months ago
dfm,jhbuhvjbnjc ngsb (NÃO ENTENDI PORRA NENHUMA)
gusullazullai 11 months ago
Genial.
marcelocelidonio1 11 months ago
po meu eu nao fiz um bom curso de ingles!!!!!
brunomsartori 11 months ago
This has been flagged as spam show
Belza, agora me paga um CCAA
CondeTERRAN0VA 1 year ago
so sad that the camera is moving all the time. i got dizzy watching this
boogie0815 1 year ago
Achei muito bom, valeu!
andrefeith 1 year ago
Comment removed
luan15750 1 year ago
claro... me dejaste clarito
jonasitouk 1 year ago
romulo@8ball.com me sigan no twitter flw
playboy3675 1 year ago
This has been flagged as spam show
N1 is the rotation of the fan in front of the engine, the one you can see when you look straight at the front of the engine. It is connected to a shaft that runs through the engine and is turned by a turbine at the aft of the engine.N2 is the rotation speed of the central core. The turbine immediately aft of the burner can receive the highest velocity airflow and turns a turbine that is hidden behind the N1 fan.
e081194eng 1 year ago
ha tah, agora entendi tudinho
alexandremorcino 1 year ago
@alexandremorcino ahora entendi todito.
LyderSlyder 1 year ago
acho melhor estudarem o português pra depois irem para o inglês.
nilvanfranca 1 year ago
estudem ingles!!!!
tadaocpv 1 year ago 17
Com s tbm, não convence ninguem
rogersubzero 2 years ago
affs , se o audio fosse pelo menos em portugues :( , fora isso o video o muito bom...
ansnois 2 years ago
Èssa explicação não me convenseu
TGFHTY 2 years ago
CONVENCEU COM ( C )
federalbureau 2 years ago
Convenceu se escreve assim...
njneumann 2 years ago
mto bom, e a explicação eu achei ótima. ;D
granmaxwe 2 years ago
opa
lucasiglesiaslucigl 2 years ago
legal só 1que devia esplicar melhor, mais é legal
sapateta 3 years ago