Skip to main content

๐๐ซ๐ž๐œ๐ข๐ฌ๐ข๐จ๐ง ๐€๐ฉ๐ฉ๐ซ๐จ๐š๐œ๐ก ๐๐š๐ญ๐ก ๐ˆ๐ง๐๐ข๐œ๐š๐ญ๐จ๐ซ (๐๐€๐๐ˆ)


Precision Approach Path Indicator





๐Ÿ›ฉ️A precision approach path indicator (PAPI) is a visual aid that provides guidance information to help a pilot acquire and maintain the correct approach (in the vertical plane) to an airport or an aerodrome.

๐Ÿ›ฉ️It is generally located on the left-hand side of the runway approximately 300 meters beyond the landing threshold of the runway.

๐Ÿ›ฉ️The ratio of white to red lights seen is dependent on the angle of approach to the runway.

๐Ÿ›ฉ️Above the designated glide slope a pilot will observe more white lights than red.

๐Ÿ›ฉ️At approaches below the ideal angle more red lights than white will be seen.

๐Ÿ›ฉ️For the optimum approach angle the ratio of white to red lights will remain equal throughout, for most aircraft, the exceptions being the Boeing 747 and now retired Concorde.

๐Ÿ›ฉ️With the 747, because the cockpit is approximately 20 feet behind the nose and much higher than other aircraft, the flight crew in a 747 will typically see one red and three white lights when they are on the glide slope.

๐Ÿ›ฉ️The aircrew of Concorde would see four white lights as the Concorde's approach angle was higher than traditional aircraft.

๐Ÿ›ฉ️These lights are visible from 5 miles in normal sunlight days, and upto 20 miles at night.

➡️Subscribe us for more aircraft knowledge and aircraft fact⬅️

➡️Do Share with your Friends⬅️







Comments

Popular posts from this blog

๐— ๐—ผ๐—ป๐—ผ๐—ฐ๐—ผ๐—พ๐˜‚๐—ฒ ๐˜ƒ๐˜€ ๐—ฆ๐—ฒ๐—บ๐—ถ-๐—บ๐—ผ๐—ป๐—ผ๐—ฐ๐—ผ๐—พ๐˜‚๐—ฒ ๐—ฆ๐˜๐—ฟ๐˜‚๐—ฐ๐˜๐˜‚๐—ฟ๐—ฒ

๐Ÿ›ซA monocoque structure uses its outer shell to support stresses and loads applied to it, whereas a semi-monocoque structure has an internal "skeleton" of supports and braces to keep its shape rigid and strong. ๐Ÿ›ซThe vast majority of pressurized aircraft are semimonocoque to help distribute stresses equally along the fuselage during flight. ๐Ÿ›ซHowever, some helicopters use monocoque structure to maximize internal space in the flight compartment. ๐Ÿ›ซMonocoque fuselage has its skin holding the skeleton structure together while the semi-monocoque has both the skin and the skeleton holding together. ๐Ÿ›ซSemi-monocoque also has "stringers" running horizontally down the plane to help hold the frame together. ๐Ÿ›ซThe monocoque fuselage also cannot be used for airframes after a certain size (small aircraft with single engine), but the semi-monocoque has been used from single piston engines to commercial airliners. ๐Ÿ›ซA monocoque design would also have ...

๐“๐ฒ๐ฉ๐ž๐ฌ ๐จ๐Ÿ ๐‚๐จ๐ฆ๐›๐ฎ๐ฌ๐ญ๐ข๐จ๐ง ๐‚๐ก๐š๐ฆ๐›๐ž๐ซ๐ฌ

๐Ÿ›ฉ️A combustor is a component or area of a gas turbine, ramjet, or scramjet engine where combustion takes place. It is also known as a burner, combustion chamber or flame holder. In a gas turbine engine, combustion chamber is fed high pressure air by the compression system. ๐Ÿ›ฉ️The combustor then heats this air at constant pressure. After heating, air passes from the combustor through the nozzle guide vanes to the turbine. In the case of a ramjet or scramjet engines, the air is directly fed to the nozzle. ๐€๐ง๐ง๐ฎ๐ฅ๐š๐ซ ๐“๐ฒ๐ฉ๐ž ✈️The most commonly used type of combustor is the fully annular combustor. Annular combustors do away with the separate combustion zones and simply have a continuous liner and casing in a ring. There are many advantages to annular combustors, including more uniform combustion, shorter size, lighter, and less surface area. Annular combustors tend to have very uniform exit temperatures. They also have the lowest pressure drop of the three...

๐Ÿ“ ๐Œ๐š๐ฃ๐จ๐ซ ๐’๐ญ๐ซ๐ž๐ฌ๐ฌ

Five Major Stresses ๐Ÿ›ฉ️Aircraft structural members are designed to carry a load or to resist stress. Aircraft parts must be planned to carry the load to be imposed upon it. ๐Ÿ›ฉ️The term stress is often used interchangeably with the word “strain.” They are not the same thing. External loads or forces cause stress. Stress is a material’s internal resistance, or counterforce, that opposes deformation. The degree of deformation of a material is strain. When a material is subjected to a load or force, that material is deformed, regardless of how strong the material is or how light the load is. ๐Ÿ›ฉ️Here 5 major stresses to which aircraft is subjected ✳️Tension ✳️Compression ✳️Torsion ✳️Shear ✳️Bending ✈️Tension is the stress that resists a force that tends to pull something apart. The engine pulls the aircraft forward, but air resistance tries to hold it back. The result is tension, which stretches the aircraft. The tensile strength of a material is measured in pounds per square inc...