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Journey to HX50 | Episode 34: Building the Main Rotor System 

Hill Helicopters
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In this episode, we explore the detailed assembly of the HX50's main rotor system and learn how its design prioritises the needs of inexperienced pilots without compromising on safety, with an emphasis on high inertia for emergency manoeuvrability and low drag for efficient flight.
Now that you’ve had an inside look into the latest developments at Hill Helicopters, sign up for a group presentation to preorder your own HX50 👉 www.hillhelico...
Mischa Gelb (aka Pilot Yellow) and Ruben Dias, ambassadors for the HX50, will outline all the highlights of this unique helicopter and answer any questions you might have.
Discover more ► www.hillhelico...
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5 окт 2024

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Комментарии : 19   
@pilotpeego1820
@pilotpeego1820 11 месяцев назад
Wow! Nice to see HX50 taking shape.
@stachowi
@stachowi 10 месяцев назад
This is thing is going to be unreal. I can't wait to own one of these.
@sheepdog1102
@sheepdog1102 11 месяцев назад
Can not wait to see one in the air it’s going to be fantastic!😊
@vandavis000
@vandavis000 6 месяцев назад
I love that type tail rotor , kinda reminds me of the Eurocopter/Airbus tail rotor all inclosed. So if tail impact your tail rotor doesnt bash the ground.😊
@BoBo-SpackleMunkey
@BoBo-SpackleMunkey 10 месяцев назад
I'm chopping at the bit to get mine!
@eddyriley2055
@eddyriley2055 11 месяцев назад
it reminds me of Rolls and Royce, when they decided that the basics worked, but they could do it so much better, but the end result was very expensive but superb. yes RollsRoyce was a coming together of two great engineers...The rest is history, in automotive and aviation.
@kevingallen1678
@kevingallen1678 11 месяцев назад
At this rate I won’t live long enough to see it fly!
@CalebO587
@CalebO587 11 месяцев назад
Very cool to see the surface patch layout in Autodesk Alias; no spans in sight!
@AC-jk8wq
@AC-jk8wq 11 месяцев назад
Dr. Hill, Who on the team… Has what background… To identify all of the proven systems… And bring them all together…? It seems, from the outside, that you have a very experienced team… There are so many parts that interact with each other, being a few mil off on one part design, is going to affect several other parts… Remaking parts to prove a different design… is beyond large corporate expensive! I searched around your website… but didn’t find the team background… Can you point me in the right direction? Best regards… 😃
@bibowang8057
@bibowang8057 10 месяцев назад
the heli will fly a thousand years later,trust me
@ipemidayo
@ipemidayo 11 месяцев назад
What CAD/CAE/CAM tool(s) are you using sir?
@sinfulcoin
@sinfulcoin 8 месяцев назад
How do you get around patent infringement or IP ownership on this project? Wasn't Bell sued into oblivion by Airbus for something so simple as the skid design?
@IsaacWarrenMurrell
@IsaacWarrenMurrell 11 месяцев назад
Let's see some blades!
@adr1uno638
@adr1uno638 8 месяцев назад
Can someone explain me the feature of the central sliding disc that seems to affect the flaping of the blades ?
@brianb-p6586
@brianb-p6586 6 месяцев назад
Do you mean the swashplate? Don't expect a video like this, or comments by other viewers, to explain the most basic and fundamental aspects of helicopter design... but now you have the keyword for a search to learn about the "swashplate" in a rotor system.
@adr1uno638
@adr1uno638 6 месяцев назад
@@brianb-p6586 Not the swashplate, I was talking about the Pink plate at 0:15 and you see it at 4:12. It is located upper than the Swashplate and on another video, we see that the blades have a contact surface with this plate and seems to counter act other blades by pushing on it. Never seen this on other rotors before
@brianb-p6586
@brianb-p6586 6 месяцев назад
Interesting,@@adr1uno638. I assume that it is structural, rather than being a controlling element. If I'm looking at the same component, it looks like this ring (rather than disk) with an I-beam cross section and holes through the web is the lowest element above the control fork at 5:17, and the highest ring-shaped element at 5:34 and lowest element at 5:40. When a blade root is moved at 5:20 the ring doesn't appear to affect pitch or flap motion, but perhaps only due to the limited travel or the incomplete hub assembly in this case. Given Hill's "use proven designs" approach this must be a conventional component, but I do not know what it is.
@SsgtMcNasty1
@SsgtMcNasty1 7 месяцев назад
I see a preflight nightmare. What I don't see is anything that actually functions.
@brianb-p6586
@brianb-p6586 6 месяцев назад
"Revolutionized product"? Fluency in English is apparently not a required skill for helicopter design and manufacturing.
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