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.
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.
This gives better control of the longitudinal loads on the wing optimising the lift over drag ratio in cruise.
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
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.
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.
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.
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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
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 ?
🧵
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.
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")