Take a tip for greener trips when you upgrade to Split Scimitar Winglets. The combined aerodynamic elements of the retrofit to the existing Blended Winglet — ventral strakes, scimitar tips, and trailing edge wedges — provide a drag reduction, and corresponding range increase, of 2 percent or more for long-range missions. See why: https://lnkd.in/ebZsjBk5 #ThinkWinglets #bbj #winglets #sustainability
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🚨 The usual #caveat applies: always check ⚠ #official ⚠ briefing products for the #FIR you will be flying in. So #icing and #tubulence… Two big #hazards for #aviation. ✈ For icing 🧊 to occur, we need to have two #ingredients: 📉 #AirTemperature close to #freezing 🥶 or sub-freezing and 🚰 visible #moisture – either #clouds ☁ or #precipitation 🌧 . Icing can occur in a variety of ways: 🔺 freezing #drizzle 🔺 freezing #rain 🔺 #EngineIcing 🔺 icing of the #PitotTube 🔺 icing of the #StaticPressurePort. #Pilots should – and do – of course, consult the #WeatherOffice or #flight service station for a forecasing on expected #IcingConditions. On the right ➡ the #EllrodIndex. Accounts for #ClearAirTurbulence (#CAT) – does ❗ NOT ❗ account for low-level turbulence due to #thunderstorms, #mountain ranges. If > 9, 🟡 #moderate 🟡, and > 20, 🔴 #severe 🔴. #FreezingRain #FreezingDrizzle #FlightLevel #SigWX #WAFC #WAFCLondon #SigWX #AviationMeteorology #AeronauticalMeteorology #aeronautics #SIGMET #SignificantWeather #MetX #Meteomatics #EURO1k #WeatherVisualization #WeatherGraphics #NumericalModel #NumericalWeatherPrediction #NWP #HighResolution #WeatherChart #WeatherForecast #WeatherForecasting #AviationForecast #FlightInformationRegion #CivilAviation #foot #feet #hectofeet #altitude #altimeter #AltimeterSetting #MSLP
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Heliport Lighting Packages - Aviation Windsock / Heliport Nylon Windsock windsock is made of corrosion-resident and high-temperature-resident nylon anti-UV material. The color is red(orange) and white, have 5 sections, the start color is red(orange). The windsock including 3 dimensions according to the pole's height. #1 The diameter is 300mm, the diameter at small end is 150mm and the length is 1.2m #2 The diameter is 600mm, the diameter at small end is 300mm and the length is 2.4m #3 The diameter is 900mm, the diameter at small end is 450mm and the length is 3.6m How to choose the windsock? Below 4m, use the first type; between 4m to 6m, use the second type; above 6m, use the third type. More detail emma@chendongtech.com what'sapp: 0086 13342512879 #heliportlighting #helipad #windsocks
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Higher lift, longer reach sums up the 2024 JCB 2TS-7T Tracked Teleskid – the world's first and only small platform compact track loader with a telescopic boom. It's just what you need when you need a little more in a compact machine. Learn more at https://bit.ly/3SUoufI.
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Enhanced for Versatility – Meet the New ARCUBE-SE! ARCUBE-SE has now been adapted to support your older lift systems. With this new edition, ARCUBE-SE ensures compliance, safety, and seamless operation for older lifts. #ARKEL #wedrivethebesttechnologies #ARCUBESE #ElevatorUpgrade #SafetyStandards #ElevatorModernization
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Unlocking The Secrets of Pod Systems on Yachts! Join Christopher in this insightful discussion on yacht propulsion as he explores the maneuverability and complexity of pod systems. Discover the advantages of Volvo IPS pods, including superior efficiency and handling in both high and low-speed scenarios. Don't miss out on this essential marine engineering knowledge! #YachtPropulsion #PodSystems #MaritimeEngineering #VolvoIPSPods #Maneuverability #MarineTechnology #BoatEfficiency #YachtingLife #HighSpeedHandling #NauticalKnowledge
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Redefine Cruising by Setting Sails : Chapter 4. The ship with hydrodynamic levelling The ship, as designed according to the invention, can be adapted to suit a variety of functions, including those as a cargo, passenger, military or work ship. In the operation of these ships, hydrodynamic levelling is achieved through the utilisation of outboard wings, situated on either side of the vessel and positioned in opposition to one another. The wings can be extended or swivelled out and are equipped with a variable, three-part wing profile that is aligned with the underwater hull in a plane parallel to the longitudinal and transverse axes of the ship. This configuration serves to counteract the heeling tendency of the ship when sailing. The leading edge segment and the trailing edge segment of the three-part wing profile can be synchronously adjusted via a hydraulically or electrically operated gearbox integrated into a central wing segment. It is proposed that torque compensation be implemented at the centre of gravity of the ship for the purpose of facilitating sailing operations. A primary torque, resulting from the transverse force generated by the sailing device, is counterbalanced by a secondary torque. This second torque is the result of a hydrodynamic force generated by the outboard wings, which create lift and downforce. The aforementioned wings are arranged in pairs, situated in opposition to one another in the region of the underwater hull. Furthermore, the shifting of the water ballast from one side of the ship to the other, either from the forecastle to the stern or vice versa, allows for the levelling of the plane spanned by the longitudinal and transverse axes. This allows the telescopic axes of the telescopic masts to be aligned parallel to the vertical axis, with the centre of buoyancy, the centre of gravity and the metacentre of the ship on the vertical axis perpendicular to each other. #ResSS4 #resoceanwind #ResSS1 to #ResSS8 #reslevelcontrol #resail #resship #rescruiseship #restelescopicmast #excellence from #theländ Res-institue.com
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Wing shapes take flight Birds can dynamically alter the shape of their wings during flight. Variable feather overlap enables birds to morph their wings. How flight feathers stick together to form a continuous morphing wing https://lnkd.in/g4j_G2JA
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mobile crane with a complex multi-axle configuration and a long telescopic boom
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IAR 80 scale 1:3 - pneumatic actuation of the canopy The pneumatic control system of the canopy was introduced starting with plane no. 241. Its need arose due to the difficulty of opening the canopy at speeds over 250 km/h, in case of leaving the cabin for parachuting.
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