An animation of a fully-articulated helicopter rotor system and swashplate showing these degrees of freedom: Collective pitch change Cyclic pitch change Flapping Lead-Lag
Пікірлер: 108
@KRAZEEIZATION4 ай бұрын
The rotor when at speed is pretty aggressive and has huge energy. What’s amazing is the small rods that pull the blades to pitch. Or the spinning shafts that drive the whole assembly and the tail rotor. All very complex and moving at incredible speeds! There’s a lot to go wrong!
@bzig49294 ай бұрын
Thanks for commenting! I agree, helicopters are amazing machines. I'm always fascinated to see how flexible the blades are, but to realize how stiff they become under CF loads.
@mudhutproductions8 ай бұрын
Those connecting rods must be insanely strong to take the assorted stresses placed on them.
@brodricj30238 ай бұрын
Point to note, with offset dual servo actuators as shown in this animation there has to be a mixing unit between the pilot controls and the servos. If you think this rotor system mechanism is complicated, it 'aint half as complicated as the mixing unit. And to think, these things were designed by engineers using slide rules.
@bzig49298 ай бұрын
Mechanical mixing units are works of art! And complicated... and really difficult to animate 🙂
@itzDrizzyyyman6 ай бұрын
im currently working on something for Unreal Engine i dont understand how a helicopter pitches left and right haha@@bzig4929
@Entertainment-mg6jx8 ай бұрын
Legendary machinery and concepts
@llwellyn19 ай бұрын
Excellent graphic presentation!
@bzig49299 ай бұрын
Thank you!
@AgentGG19679 ай бұрын
Love this...thanks for posting...!!!
@wbwilhite8 ай бұрын
It boggles the mind that people invent this stuff out of nothing. Human imagination can be truly awesome.
@flat-earther8 ай бұрын
hi wbwilhite, have you become a flat earther yet?
@bzig49298 ай бұрын
Absolutely! Even more so when you think that most of the complex systems around us came before computers, 3d modeling and simulations.
@wbwilhite8 ай бұрын
@@flat-earther Since 1975, I have been around the world multiple times by air and sea. To me, the world appears round. If I ever get to outer space, I will likely see it again, that the Earth is a sphere. How about you?
@muneneeric39038 ай бұрын
I will try one in Africa kenya
@flat-earther8 ай бұрын
@@wbwilhite okay. I became a flat earther in 2020 BTW wbwilhite, what do you think about all gubments drawing a line around you and saying you are not allowed to leave?(Antarctic Treaty) If you don't know what I mean, read my about tab.
@user-jv5kw1ve3q3 ай бұрын
This channel make me understand everything about helicopter
@darioinfini8 ай бұрын
Can you imagine the engineering brain that came up with this mechanical interface to account for all the motions described here. Damn.
@user-tw4fd4wu1g8 ай бұрын
and it needs to be reliable, crazy engineering
@Boss_Tanaka8 ай бұрын
Lots of try-and-errors lead to this state of the art engineering
@user-vp1sc7tt4m8 ай бұрын
I think modern helicopter design started with the work of Igor Sikorsky although exploration had been going on for many years before his first designs in the 1930's. (based on memory only)
@stachowi8 ай бұрын
it wasn't a single person (or company), it all started with the autogyro and then the flaws were worked out by many different people.
@stachowi8 ай бұрын
sikorsky was late in the game when it came to rotor systems, he perfected the helicopter design (main rotor with single tail rotor)@@user-vp1sc7tt4m
@arshu333 Жыл бұрын
Bruh. Such an amazing work.
@richardbeach83647 ай бұрын
Worked for me, thank you.
@rajeshankala71489 ай бұрын
A century old technology.
@tetttettamilli6761 Жыл бұрын
👍. Can u an animation on engine lubrication systems, specifically, those used in inverted piston-engine helicopters?
@siphesihlelanga57838 ай бұрын
Ingenious ❤
@samspade86129 ай бұрын
Outstanding video. The only thing that would make it better is if you established the helicopter forward position to show left & right turns & forward & back. Maybe even a small video insert showing the control movements while the swashplate is moving.
@bzig49299 ай бұрын
I'm on it!
@yzScott9 ай бұрын
Remember, the controls are phased 90 degrees from what you'd think. To control the pitch of the helicopter, the cyclic is "active" while the blades are perpendicular to forward flight. Also, I've never seen a head with "flap" pivots. The blades would droop to the ground when not turning.
@sc0tte1-4168 ай бұрын
I always thought the tail rotor did that but then again I know nothing lol
@WW5RM7 ай бұрын
@@sc0tte1-416it does but what I think he is meaning is pitch left and right. As you are pitched say forward at full collective, as the blades are at the rear they are at the maximum pitch, as they come forward they become flatter all depending on how much lift is needed. So I think he means left and right cyclic / stick or pitch. Not turn.
@edwardhunter36479 ай бұрын
Thanks,I will be building a prototype soon.
@user-yf8rz8ym8m9 ай бұрын
Замечательно!
@JoseLopez-xu8ue8 ай бұрын
Up down flapping used how it's relivent it's energy spent up
@helicopterovirtual-msfs62548 ай бұрын
Sensacional.
@user-sb3zd9vh3m5 ай бұрын
Спасибо, теперь я окончательно понял как работает автомат перекоса для направления движения вертолёта! Ещё хочется понять как происходит передача крутящего момента от двигателей к винту
@bzig49295 ай бұрын
Thanks for watching and thanks for the comment!
@jeffrenman41467 ай бұрын
dear content creator a beautiful beautiful super super good animation… But one thing are those control rods attached to the rotor grips dragging the swash plate ?
@bzig49297 ай бұрын
Good catch! This should have a component called a "drive scissors" that connects the rotating swashplate to the mast. The drive scissors is what drags the swashplate along to match the rotation of the rotors. I had a difficult time figuring out the relationship for movement of the scissors, so I did not animate it. I have another video with the scissors included. Thanks!
@sc0tte1-4168 ай бұрын
They need to reverse engineer UFO tech already. This seems too complicated with too much crap that could go wrong
@kwcnasa Жыл бұрын
Hello, helicopter pilots. Does a tail rotor auto re-center to it's center position when you release the foot pedal? Or should I ask were they spring loaded so that it will return to center position upon releasing the foot pedal? Does the cyclic spring loaded as well? Does it return to center like those computer joysticks? Thank you in advance.
@bzig4929 Жыл бұрын
Some larger helos, those with advanced flight controls, have a pedal trim feature. In these aircraft the pedals auto trim to a position selected by the pilot or the flight control computers. The pilot can retrim via a button on the cyclic control, or with microswitches on the pedals. In most smaller helicopters, the pedals do not trim to center... They stay (via friction) where the pilot last positioned them. On these aircraft the friction is usually adjustable.
@bzig4929 Жыл бұрын
The cyclic, even on small helos, generally has a trim feature that returns to the pilot select trim position. On more advanced aircraft, the pilot, or the computers, can adjust the trim position. For example, if a helo has a attitude retention feature, the computers can continually readjust the trim to hold pitch and roll attitude. Generally (different designs treat this differently) attitude retention is done via trim, wheras rate stabilization is done downstream of the pilot controls and does not move the trim position.
@brodricj30238 ай бұрын
@@bzig4929 Pedal trim switch is usually on the collective, not the cyclic control.
@brodricj30238 ай бұрын
1. When you take pressure off the foot pedal the pedal (and tail rotor pitch) should stay where you left it (by design). If it moves then maintenance needs to make adjustments. 2. In helicopters with cables that make the tail rotor pitch changes there is a special spring mechanism as a safety precaution if one cable breaks the other cable still has some control authority. 3. Yes, the cyclic has a spring mechanism (and magnetic brake) which is part of the force trim system. When engaged the cyclic control stays where you leave it.
@user-zz4he5eq2n8 ай бұрын
ドラえもんのタケコプターのように回転軸のシャフトの向きを変えることで浮力の方向を変えたい。
@SnowWhiteDuc8 ай бұрын
A year's worth of physics to be dissected in this video.
@menititehnik9 ай бұрын
Come, see and learn Sir..👍
@mooncrack378 ай бұрын
how about coaxial rotor? it is hard to imagine having 2 independent swashplate(if it true) with each can rotating in different speed
@bzig49298 ай бұрын
I think the way the coax works is the "stationary" swashplate of the upper rotor is not actually stationary, but it rotates with the lower rotating swashplate. That would be a fun project to 3d model.
@JoseLopez-xu8ue8 ай бұрын
Three significant use fifteen
@swashplate Жыл бұрын
Looks just like my MH-53E, only it has 7 blades.
@brodricj30238 ай бұрын
Yep. The animation is very similar to the way Sikorsky builds these things.
@zacharydutcher35869 ай бұрын
How many?
@smokescreen2146 Жыл бұрын
How fragile are the components of this system in practice?
@zombieregime9 ай бұрын
Well....there is video of a MH-60 cutting off its own refueling snorkel in an aerial refueling mishap. It survived, though probably with a good shimmy to it. Of course that is a LARGE military aircraft, so its built to withstand things most crafts will never see, like being shot at. The blades of a helicopter need some give to them, you dont want them to be too rigid or they'll shatter as they encounter forces around the cyclic....uh cycle. So the bend along the length is very much a design choice. the lead/lag dampeners are also a mitigation to allow the rotor to engage in some not that good for itself geometry and return to normal without too much issue. Some helis have counter weights at the blade mounting point that will counter flap to help disperse the energy of the flap and keep everything spinning right. As far as the rest of the mast and control structure.....well the mast itself supports at least the maximum takeoff weight of the craft, plus maneuvering forces as the fuselage is basically a pendulum under the rotor disk. The hub has to keep the blades from flying away via centrifugal force, and translate their lift to the vertical mast (remember the blades are the wings, they are airfoils that are moving through the air via rotation instead of linear motion. Also, helicopters do not create lift, they beat the air into submission😉). The part on top that keep the rotor hub from flying off the mast is colloquially known as 'the Jesus nut' because if you bust that nut, you're going to meet Jesus. Its the same as a plane losing its wings, the rest of the craft tries to hang in the air in exactly the same way that bricks dont. Usually with the same results.... The control linkages......are RIDICULOUSLY strong AND light. Every ounce counts when a rotor craft can fly laterally for hours, but only hover for 30 minutes. At least when its moving forward lift efficiencies take over and save fuel. But a dead hover just CHEWS through fuel like you wouldnt believe. Especially for the big birds. I cant quote you tensile strength numbers because honestly I dont know. But with forces like all of that involved, its safe to assume that while some compliance is built into some of the pieces, they are still incredibly strong. So, not very fragile at all. In fact, its the rotating balance of the rotor disk that is the most important. If thats out of whack, you better get to the ground before physics decides thats enough flying for you today.
@flat-earther8 ай бұрын
@@zombieregime hi zombieregime, have you become a flat earther yet?
@brodricj30238 ай бұрын
They are surprisingly robust considering the other design aim is to make them as light weight with as little metal as possible. There is 3000 psi of hydraulic pressure pushing those bits up and down. If it all stays straight it can take the flight loads with margin to spare.
@assassin30083 ай бұрын
Please make a video of how the cyclic and collective link to the swashplate
@bzig49293 ай бұрын
I did that a couple of weeks ago. Check out my helicopter playlist. Thanks!
@assassin30083 ай бұрын
@@bzig4929 i saw the video of how the cyclic moves and how the swashplate responds but i mean like the rods between the cyclic and the swashplate
@bzig49293 ай бұрын
Oh... I understand. That would be cool. These large helicopters have so much mixing in the controls, it would be very challenging to animate that. Maybe I can start with a smaller helicopter, with no mixing. I'll start working on it! But I've got a few other things I want to do before I get to that.
@assassin30083 ай бұрын
@@bzig4929 i have a diagram of the cyclic and collective, theres pedals but they're simple so not much use
@MattCantSpeakIt8 ай бұрын
Research has been proceeding to develop a line of automation products that establishes new standards for quality, technological leadership, and operating excellence. With customer success as our primary focus, work has been proceeding on the crudely conceived idea of an instrument that would not only provide inverse reactive current, for use in unilateral phase detractors, but would also be capable of automatically synchronizing cardinal grammeters. Such an instrument comprised of Dodge gears and bearings, Reliance Electric motors, Allen-Bradley controls, and all monitored by Rockwell Software is Rockwell Automation’s "Retro Encabulator".
@bzig49298 ай бұрын
You're comparing real technology to the retro encabulator? I'm fascinated by this. I think what you're saying is that everyday things can be so complex that they cause anxiety, but if we cover up the guts of the technology, so it's out of sight, then we're ok with it.
@MattCantSpeakIt8 ай бұрын
@@bzig4929 huh??? I'm not comparing anything. This was just a joke mate ... I think this animation is brilliant...
@bzig49298 ай бұрын
Oh, sorry... my reply was also an attempt at humor. Love the turbo encabulator 😉
@Vadimkatashid8 ай бұрын
The inventor of this device is Russian mechanic Boris Yuryev!
@bzig49298 ай бұрын
He was also the first to propose the tail rotor for anti-torque. Thanks for commenting!
@bestamerica9 ай бұрын
' this helicopter must have alot of harden ballbearrings
@brodricj30238 ай бұрын
Elastomeric bearings have been used for many years in helicopter rotor systems.
@lucid2128 ай бұрын
What controled flapping?
@bzig49298 ай бұрын
Flapping isn't controlled. It's an aerodynamic and inertial response to the control moments generated through blade feathering.
@lucid2128 ай бұрын
@@bzig4929 Ah yes, thank you sir! Superb video! ❤️👏
This is a very good observation. Control inputs are at one-per revolution, but it's not practical to move the controls this fast when the rotor is operating at a flight RPM. As you point out... something would break.
@bzig49298 ай бұрын
Also with noting... helicopters of the future may have higher harmonic control... where rotor control can be at frequencies higher than one-per-rev. The vision is HHC inputs will give airplane like ride quality using small high frequency inputs.
A little explanation wouldn't hurt.... and perhaps some soothing wind noise in the background would also be nice.
@bzig49298 ай бұрын
I like it! I've been thinking about expanding this video with exactly what you suggest.
@muneneeric39038 ай бұрын
I will be the first African to invent this rotary blade
@bzig49298 ай бұрын
Keep watching videos! We have faith in you!
@UdinSamsudin-zg9jo6 ай бұрын
Yang semua nya
@aleksandrmatveev93378 ай бұрын
Doesnt look like a solid construction.
@SantoshRajput-vn2lr10 ай бұрын
Hi
@SantoshRajput-vn2lr10 ай бұрын
Hii
@lahiruudara33563 ай бұрын
Amazing animation! Is there a way for me to use this for an explainer about Mars Helicopter, Ingenuity on my channel @octoberskyshow?
@lahiruudara33563 ай бұрын
www.youtube.com/@octoberskyshow
@bzig49293 ай бұрын
that's cool if you want to use the content inside one of your vids. I have done strikes against videos where it's just a 100% copy, but other than that I don't.
@lahiruudara33563 ай бұрын
@@bzig4929 Thank you very much for your kindness. I will send you the video before I publish it.
@miriahmpaloma80889 ай бұрын
But your derailed before you prayed rotor control
@4stringmanagmaildcom3 ай бұрын
The angle of attack of the airfoil changes due to the relative airflow speed right? As the bird is moving forward an advancing blade has a higher apparent wind speed (term from sailing) so less pitch is needed and a retreating blade has a slower apparent wind so more pitch is needed. Is this correct?
@bzig49293 ай бұрын
Yes! You are correct, but there is another influence. As the advancing blade generates more lift, some of this increase in lift causes the blade to flap upward, this changes the direction of the relative wind in a way that reduces lift. The purpose of the flapping hinge is to allow this and balance the disyemmetey of lift caused by the advancing and retreating sides.