Презентация, доклад по английскому языку по теме Авиационные приборы

I. Pitot-static systemBasic system which is located onboard Mi-8 called the pitot-static system.This system measures air pressure and compares it to static pressure to indicate the aircraft's speed through the air.The pitot-static system supplies power to three basic aircraft instruments:-

Слайд 1The Pitot-Static System Powers Aircraft Instruments

The Pitot-Static System Powers Aircraft Instruments

Слайд 2I. Pitot-static system
Basic system which is located onboard Mi-8 called the pitot-static system.
This

system measures air pressure and compares it to static pressure to indicate the aircraft's speed through the air.


The pitot-static system supplies power to three basic aircraft instruments:
- the airspeed indicator, 
- altimeter, 
- vertical speed indicator.

I. Pitot-static systemBasic system which is located onboard Mi-8 called the pitot-static system.This system measures air pressure and compares it

Слайд 3II. Main components
Pitot tube
The pitot tube is an L-shaped device located

on the exterior of the aircraft that is used to measure airspeed.
Some types or pitot tubes have an electronic heating element inside of the tube that prevents ice from blocking the air inlet or drain hole.




II. Main componentsPitot tubeThe pitot tube is an L-shaped device located on the exterior of the aircraft

Слайд 4II. Main components
Static Port(s)
The static port is a small air inlet,

usually located on the side of the aircraft, flush against the fuselage. 
The static port measures static (non-moving) air pressure, which is also known as ambient pressure or barometric pressure. Some aircraft have more than one static port, and some aircraft have an alternate static port in case one or more of the ports becomes blocked.
On Mi-8 this port is located on PVD-6M




II. Main componentsStatic Port(s)The static port is a small air inlet, usually located on the side of

Слайд 5II. Main components
Instruments
The pitot-static system involves three instruments: The airspeed indicator,

altimeter, and vertical speed indicator. Static lines connect to all three instruments and ram air pressure from the pitot tube connects to only the airspeed indicator.




II. Main componentsInstrumentsThe pitot-static system involves three instruments: The airspeed indicator, altimeter, and vertical speed indicator. Static

Слайд 6III. Normal Operation


The pitot-static system works by measuring and comparing static

pressures and in the case of the airspeed indicator, both static and dynamic pressure.
1. Airspeed: The airspeed indicator is a sealed case with an aneroid diaphragm inside of it.
When airspeed increases, the dynamic pressure inside of the diaphragm increases as well, causing the diaphragm to expand. 
Through mechanical linkage and gears, the airspeed is depicted by a needle pointer on the face of the instrument.






III. Normal OperationThe pitot-static system works by measuring and comparing static pressures and in the case of

Слайд 7III. Normal Operation


The pitot-static system works by measuring and comparing static

pressures and in the case of the airspeed indicator, both static and dynamic pressure.
1. Altimeter: The altimeter acts as a barometer and is also supplied with static pressure from the static ports.
They expand and contract as the pressure rises and falls in the surrounding instrument case. A Kollsman window inside of the cockpit allows the pilot to calibrate the instrument to the local altimeter setting to account for non-standard atmospheric pressure.






III. Normal OperationThe pitot-static system works by measuring and comparing static pressures and in the case of

Слайд 8III. Normal Operation


The pitot-static system works by measuring and comparing static

pressures and in the case of the airspeed indicator, both static and dynamic pressure.
1. VSI: The vertical speed indicator has a thin sealed diaphragm connected to the static port. The surrounding instrument case is also sealed and supplied static air pressure with a metered leak at the back of the case.
Once the aircraft levels off, the pressures from both the metered leak and the static pressure from inside the diaphragm equalize, and the VSI dial returns to zero to show level flight.






III. Normal OperationThe pitot-static system works by measuring and comparing static pressures and in the case of

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