Aircraft Technical

Commercial aircraft usually fly at high altitude to get advantage of fuel economy and calm weather. As the aircraft climb, the atmospheric pressure falls with increase in altitude. The low pressure at high altitude is created the unsafe environment for passengers and crews. Aircraft operating at high cruising altitude is typically equipped with pressurized cabin to protect the aircraft occupant against low atmospheric pressure. Aircraft cabin pressurized with constant pressure is usually maintained 8000 ft cabin altitude.  The cabin internal pressure is regulated by automatic cabin pressure control system. Cabin pressure also regulated by flight crew through manual control if automatic cabin pressure control system failed. When cabin pressure is lower than atmospheric pressure negative pressure differential condition developed which is dangerous for aircraft structure. Positive pressure condition is developed when cabin pressure is greater than atmospheric pressure which is hazardous s

Aircraft structural components is the main load carrying member. How efficiently structure will take load depends on its structural components design and material.Thus , primary consideration in aircraft design is placed on structural components. Generally,  three different types of  design philosophies used in designing of structural components which are such as safe-life , fail-safe and damage tolerant design. Please read below article on  safe-life and fail-safe design philosophy. https://aircrafttechnicalinfo.blogspot.com/2021/08/aircraft-structural-components-design.html Damage Tolerant Design Concept ;  As we know fail safe structure so designed that after failure of one part there is still sufficient strength in the reminder part to prevent catastrophic failure until damage part found by routine inspection.The inspection criteria developed for fail safe design failed to specify inspection technique and inspection frequencies were not sufficient to detect discrepancies prior to c

  Engine nacelle strake is vortex generator which enhance aerodynamic performance of an aircraft. It is mounted on engine nacelle. Encircled part in this picture is engine nacelle strake.Many aircraft engine have strake only one side and that will be on inboard of nacelle but few aircraft have strake on both the sides. Fig 01 Engine Nacelle Strake  Fig 02 Strake View from Cabin The purpose of nacelle strake is to generate vortex which energize the low energy airflow over the wing when aircraft operating at high angle of attack and low speed condition such as takeoff and landing phase of flight. We have seen many modern aircraft have their engine mounted beneath of wing and inlet of engine nacelle  forward of wing leading edge. There are many advantages of installing engine below the wing but there are some disadvantage and one of the disadvantages is engine nacelle /wing assembly interaction which disturb the airflow over the wing and it affect the lift production capability of wing. A

An aircraft structural components is the main load carrying member. How efficiently structure will take load depends on structural components design and material.Thus , primary consideration in aircraft design is placed on structural components. There are generally three different types of  design philosophies used in designing of structural components which are such as safe-life , fail-safe and damage tolerant design. Safe-Life Design ;        Original or initial accepted theory of structural components design was safe-life design.According to safe life design concept, the structure designed for finite fatigue life and on reaching this fatigue life structure should be retired from service.A safe life structure components must be remain crack free during their entire time in service.  Safe life structural components service fatigue life is normally consider 25 percent of average life but this consideration of life will not ensure safety of aircraft throughout of its operation because r