
U-60 Bug
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IPACS Kinda needs to make the animation during rough operations better.. maybe some sparks or breaking or rotoa would be nice!
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This is how these rotor blades actually move when the helicopter is flying forward. The one moving forward rises and falls behind, the one moving backwards sinks and rushes forward. In reality, however, this back-and-forth movement and flapping up and down is limited by bumpers and dampened by shock absorbers. Maybe this is not well simulated.
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Your recent co-axial Kamov crop duster picture looked very extreme but it was real life! Can they have one lower ‘plane’ rotor tilting up on the same side as the other (opposite rotation) rotor tilting down?
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Yes, that's the case. That is why the designers had to determine the distance between the two rotor planes in such a way that it was not too much, but that the blades did not collide. This danger is greater at low rotor speed (idling on the ground). Therefore, the left pedal must be engaged below 60% rotor speed. In this case, the lower rotor is at a low pitch angle, the upper one at a high pitch angle. Then the distance between the two rotor planes is the largest.
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The autorotation maneuver is somewhat complicated in the UH60 Black hawk since the rotor blades lose energy even if the nose is turned down. But it is possible with practice. Instead the R22 and EC 135 is easy. I love helicopters. What do you think?
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Meanwhile the main post was the rotors clipping in the body😅
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Meanwhile the main post was the rotors clipping in the body😅
Yes, and I also wrote that the up and down movement of the rotor blades is (also) probably exaggerated in the simulator, this may be the reason. Sorry if I made it too complicated.
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The autorotation maneuver is somewhat complicated in the UH60 Black hawk since the rotor blades lose energy even if the nose is turned down. But it is possible with practice. Instead the R22 and EC 135 is easy. I love helicopters. What do you think?
Autorotations are not implemented correctly...
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Autorotations are not implemented correctly...
What's wrong with them?
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Las autorrotaciones no están implementadas correctamente...
I understand. But if I like to do the maneuver, although complicated in the UH60 but it is possible.
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What's wrong with them?
Energy management is not correctly modelled...
You cannot get any speed by losing altitude when engine fails...
If you want to know what I mean follow these for ec135:
1. Takeoff like a real helicopter does(Takeoff backwards keeping an eye on helipad... Takeoff decision point for ec135 is 120ft AGL).
2. Fail both engines at 120ft.
3. TRY to land in helipad which is in front of you.
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I understand. But if I like to do the maneuver, although complicated in the UH60 but it is possible.
Yes, autorotations with forward speed can be achieved and it is also not realistic.
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Takeoff decision point for ec135 is 120ft AGL
Is there any description of this take off procedure?
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Is there any description of this take off procedure?
Watch rotorsimxp for detailed ec135 procedures:
RotorSimXPHerzlich willkommen bei RotorSimXP, dem Youtube-Kanal von rotorsim. rotorsim ist das deutschsprachige Portal für die Hubschraubersimulation. Bei uns ist die…youtube.com -
Watch rotorsimxp for detailed ec135 procedures:
I wached this video:
Tutorial VTOL Procedures EC 135 V5
External Content youtu.beContent embedded from external sources will not be displayed without your consent.Through the activation of external content, you agree that personal data may be transferred to third party platforms. We have provided more information on this in our privacy policy.This is where the 120 ft decision height really comes into play. I'm not very good at English, but I think this refers to the stoppage of only one engine, not two. Land below 120 ft, continue the flight above it in one engine mode.
I think this because every helicopter has a height/velocity diagram, on which the areas where a safe landing is not guaranteed are marked. I couldn't find the EC135 anywhere on the internet, maybe because it has two engines. That's why I'm uploading a diagram with a single engine, the EC135 can be almost similar without an engine. This shows the approximate altitude from which you can land safely without an engine starting from a horizontal speed of 0 kt.
Here is the article:
https://www.flight-study.com/2020/07/heightvelocity-diagram-helicopter.html
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Do you need to release a clutch to autorotate the 135 or the Black Hawk? I do on the R-22 on PC (via joystick buttons). The 'expert mode' PC R-22 is .... interesting.
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