Air Intakes - Aircraft Gas Turbine Engines #04

แชร์
ฝัง
  • เผยแพร่เมื่อ 5 ก.ย. 2024
  • Aircraft Gas Turbine Engines #04 - Air Intakes
    Chapters
    0:00 - Intake Locations & Purpose Aircraft Engine Intakes
    0:53 - Circular Cross-Section Pitot Type Intakes
    3:19 - Secondary Inlet Doors
    4:47 - Supersonic Intakes
    10:51 - Intake Stall & Serge
    11:55 - Intake Icing
    12:28 - Intake Damage & Ingestion
    Playlist
    • Aircraft Gas Turbine E...
    Aircraft Gas Turbine Engines #01 - Introduction Part 1
    • Aircraft Gas Turbine E...
    Aircraft Gas Turbine Engines #02 - Introduction Part 2
    • Aircraft Gas Turbine E...
    Aircraft Gas Turbine Engines #03 - Introduction Part 3
    • Aircraft Gas Turbine E...
    Air Intakes - Aircraft Gas Turbine Engines #04
    • Air Intakes - Aircraft...
    Compressors Part 1 - Aircraft Gas Turbine Engines #05
    • Compressors Part 1 - A...
    Compressors Part 2 - Aircraft Gas Turbine Engines #06
    • Compressors Part 2 - A...
    Compressors Part 3 - Aircraft Gas Turbine Engines #07
    • Compressors Part 3 - A...
    Combustion Chambers Part 1 - Aircraft Gas Turbine Engines #08
    • Combustion Chambers Pa...
    Combustion Chambers Part 2 - Aircraft Gas Turbine Engines #09
    • Combustion Chambers Pa...
    Turbine Assembly - Aircraft Gas Turbine Engines #10
    Exhaust System - Aircraft Gas Turbine Engines #11
    • Exhaust System - Aircr...
    Reverse Thrust - Aircraft Gas Turbine Engines #12
    • Reverse Thrust - Aircr...
    Performance - Aircraft Gas Turbine Engines #13
    • Performance - Aircraft...
    Thrust Augmentation - Aircraft Gas Turbine Engines #14
    • Thrust Augmentation - ...
    Bleed Air - Aircraft Gas Turbine Engines #15
    • Jet Engine Bleed Air -...
    Gear Boxes & Accessory Drives - Aircraft Gas Turbine Engines #16
    • Gear Boxes & Accessory...
    Ignition Systems - Aircraft Gas Turbine Engines #17
    • Ignition Systems - Air...
    Engine Starting - Aircraft Gas Turbine Engines #18
    • Engine Starting - Airc...
    Engine Fuel Systems Part 1 - Aircraft Gas Turbine Engines #19
    • Engine Fuel Systems Pa...
    Engine Fuel Systems Part 2 - Aircraft Gas Turbine Engines #20
    • Engine Fuel Systems Pa...
    Gas Turbine Fuels - Aircraft Gas Turbine Engines #21
    • Gas Turbine Fuels - Ai...
    Lubrication Part 1 - Aircraft Gas Turbine Engines #22
    • Lubrication Part 1 - A...
    Lubrication Part 2 - Aircraft Gas Turbine Engines #23
    • Lubrication Part 2 - A...
    Auxiliary Power Unit (APU) - Aircraft Gas Turbine Engines #24
    • Auxiliary Power Unit (...
    Engine Instrumentation Part 1 - Aircraft Gas Turbine Engines #25
    • Engine Instrumentation...
    Engine Instrumentation Part 2 - Aircraft Gas Turbine Engines #26
    • Engine Instrumentation...
    Engine Instrumentation Part 3 - Aircraft Gas Turbine Engines #27
    • Engine Instrumentation...
    Engine Instrumentation Part 4 - Aircraft Gas Turbine Engines #28
    • Engine Instrumentation...
    Propellers Part 1 - Aircraft Gas Turbine Engines #29
    • Propellers Part 1 - Ai...
    Propellers Part 2 - Aircraft Gas Turbine Engines #30
    • Propellers Part 2 - Ai...
    Propellers Part 3 - Aircraft Gas Turbine Engines #31
    • Propellers Part 3 - Ai...
    Propellers Part 4 - Aircraft Gas Turbine Engines #32
    • Propellers Part 4 - Ai...
    Merch:
    teespring.com/...
    Support:
    www.subscribes...
    / aeroandair
    Social Media
    Twitter: / aeroandair
    Tumblr: / aeroandair
    Instagram: / aeroandair
    Minds: www.minds.com/...
    Affiliate Links:
    Brave Browser: brave.com/aer491

ความคิดเห็น • 13

  • @rudyandersson38Star
    @rudyandersson38Star 3 ปีที่แล้ว +2

    I didn't know how many parts there was such as the spike . Thumbs up for the explained

  • @alex458897
    @alex458897 6 หลายเดือนก่อน +2

    Thank you for this high quality content!

  • @ChrisZoomER
    @ChrisZoomER 3 ปีที่แล้ว +2

    Brilliant explanation. The only thing you missed is that many other high-bypass engines have a convergent inlet to maximize "ram intake" in order to slow the airflow down to Mach 0.5 when a jetliner is cruising at transonic speeds.

  • @owouwu9032
    @owouwu9032 2 ปีที่แล้ว +2

    With the sr71 the bypass wasn’t from the intake but it was from the 6th stage of the compressor directly to the afterburner

  • @natigahmet1903
    @natigahmet1903 3 ปีที่แล้ว

    Well explained, but sometimes need to make a stress on that stall and stonewall absolutely different phenomena

  • @mohammedpilot2335
    @mohammedpilot2335 2 ปีที่แล้ว

    Thanks

  • @thomashvnmusic
    @thomashvnmusic 3 ปีที่แล้ว

    Thank you!

  • @anubhavparihar5706
    @anubhavparihar5706 3 ปีที่แล้ว

    Nice work

  • @martinmilev611
    @martinmilev611 3 ปีที่แล้ว

    Perfect

  • @gazmchurcty7485
    @gazmchurcty7485 2 ปีที่แล้ว

    Can someone explain the stages of compression?

  • @gabrielibarcena7481
    @gabrielibarcena7481 ปีที่แล้ว +2

    lol @ 12:53

  • @aqumant
    @aqumant ปีที่แล้ว

    Why does it auto-generate Dutch subtitles?? Just why :D