Arjun Singh Profile picture
Jun 11 7 tweets 4 min read Twitter logo Read on Twitter
The #A350's 64.75m wing-span is designed using nature’s perfect understanding of aerodynamics to maximise lift and reduce drag, further optimising fuel burn and lowering CO2 emissions.

Here are 2 ways the #A350 reduces drag & fuel burn. Image
1. Variable Camber (VC) symmetrically in cruise optimizes wing profile by small flap deflection & aileron droop in order to manage the center of lift of the wing & adjust the camber or the wing in order to reduce drag & slightly improve performance.
👆One can see and hear the flaps actuators work in cruise.

📹 @WorldAviationHD

This gives better control of the longitudinal loads on the wing optimising the lift over drag ratio in cruise. Image
2. The Differential Flaps Settings (DFS), unique to the #A350, optimises cruise aerodynamic efficiency and lateral loads through the control of the wing centre of the lift position where inner and outer flaps are deflected differentially.

📸 FlightGlobal & Airbus Image
The Flap Cruise Deployment Function performs symmetrical small deflection (uniform & differential) during cruise in the limited range of -2° (flaps up) to +4° (flaps down) for the inner flap & -2° to +1° for the outer flap. Image
Asymmetrical small deflections up to 3° generate a roll effect & called lateral trim function.

Together, these 2 functions Optimize the wing camber to reduce wing loads and drag & Perform an optimized Lateral Trim function. Image
The result is an extremely efficient wing that produces more lift with less weight & is capable of advanced load handling performance that helps reduce fuel burn & CO2 emissions.

Both VC & DFS are fully transparent to the pilots & are embedded into the flight control laws. Image

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More from @chainsawrocks

Feb 3
When aircraft are flown outside of their established operating limits – the flight envelope – and correction efforts are not made or occur too late, it can lead to loss of control in flight (LOC-I).

Safety innovation 🧵 on The Airbus flight envelope protection.
High angle-of-attack protection: This protects against the risk of an aerodynamic stall, including in situations of wind shear, as well as during dynamic manoeuvres or in gusty conditions
High-speed protection: The aircraft is protected against overspeed situations that may eventually result in potential control difficulties, as well as structural concerns due to high aerodynamic loads
Read 9 tweets
Jan 25
Aircraft doors & emergency exits are for ingress/egress of pax & crew on ground only.

A question asked by many : Can these doors/exits be opened in-flight ?

🧵 Image
Operating the opening handle, the door moves slightly inward (0.5-4mm depending on door rigging) then upward before opening outward & moving fwd parallel to the fuselage.

The initial inward movement brings a gap between door & fuselage door stops, thus allowing the door to go up
In-flight, the lever can only be moved up until reaching about 30°-35°. This motion is sufficient to trigger the door closed & the latch sensors to indicate an unsafe door on ECAM. Image
Read 7 tweets
Jul 13, 2022
The engine idle speed control is used to prevent stall during idle. The goal-to idle at as ⬇️ RPM as possible yet keep it from running rough/stalling when power-consuming accessories - air conditioning and alternators, turn on
Q. How many engine idle’s are there for CFM56 #A320 ?
• Reverse Idle ( approx.70% N2 )
= Approach Idle + 1000 RPM FADEC sets the engine speed at reverse idle when the throttle is set in the reverse idle detent position.
• Approach idle (approx.70% N2)varies as a function of Total Air Temperature (TAT and altitude)
This idle speed is selected to ensure sufficiently short acceleration time to go around thrust & is set when the a/c is in an approach configuration. (Flap Lever Position -" NOT UP")
Read 7 tweets

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