Jesus nut
en.wikipedia.org
en.wikipedia.org
It is believed that Jesus Code is the reason the second coming of Christ has not yet occurred. As Jesus would be flooded with support requests, jira tickets, and zoom meetings. (Some people believe the modern SDLC to be the devil’s way of keeping Jesus from coming.)
Bit of trivia: the bigger danger to helicopters is actually the rotor slowing down too much. If that happens, the rotor will fold. Yes, centrifugal force is the major force keeping rotors in one piece.
So lose your engine, and you must slam the collective down to keep rotor speed. (Nit: higher energy rotors give you more time.)
ASCII diagram (the "o" is the j-nut):
| |
\.__o__./> The tips of the rotor blades move faster through the air than the parts of the blades near the hub, so they generate more lift, which pushes the tips of the blades upwards, resulting in a slight cone shape to the rotor disc. This is balanced by centrifugal force. If rotor RPM drops too low, the rotor blades fold up with no chance of recovery.
> Rotors are typically designed with washout (twist) so that lift is relatively uniform along the blades. However, because lift increases quadratically with airspeed, coning still occurs at higher RPMs.
> Some helicopters such as the Bell UH-1 Iroquois are designed with "pre-coned" blades, which are curved downwards but lay more flat in flight.
Good ol' Robinson Safety Notice SN-11:
https://robinsonheli.com/wp-content/uploads/2015/12/rhc_sn11...
(Though it does note that this scenario doesn't apply to an autorotation entry on engine loss, so I suppose you're okay in this example. Still terrifying though!)
And yes, they are complicated.
Boy, is it a rush when you get good enough to fly one by feel.
Edit/Append: He explained because the rotor turns the opposite direction of most of the other helicopters he flew, his instincts would get him killed.
Yes, Robinsons are known for mast bumping. On the other hand, they have the best tail rotor authority.
All aircraft in the US have a manufacturer-decided, and FAA-approved max amount of time between overhauls, and such overhauls are so thorough as to make the aircraft new again. (Sometimes, they even change enough things that the aircraft has to go through airworthiness tests again.)
These overhauls would definitely replace the Jesus nut if there's any hint of problems.
https://en.wikipedia.org/wiki/CHC_Helikopter_Service_Flight_...
> The term "Jesus clip" is a comical reference given to it due to its tendency to come loose and launch itself at high speed while removing or installing it, often leading to the remark "Oh Jesus, where did it go?"
Old kite surfers had a Jesus rope, that you pulled to collapse the canopy and stop you flying away in a gust.
https://i.pinimg.com/736x/4a/d0/d6/4ad0d68003a6d213e0a56f9b4... - CH-53K, No jesus nut
https://www.copters.com/mech/pictures/r22_head.jpg - R22, also none
update: I was unable to find any evidence for the rotor head story, but while looking I found this page full of -53 trivia and I wanted to share it.
https://sikorskyarchives.com/home/sikorsky-product-history/h...
A decade later we all realised that the new bikes were insanely reliable, and never had random electrical issues in the rain.
[1]: https://www.urbandictionary.com/define.php?term=jesus%20hand...
But the helicopter thing makes sense too.
I’ve personally heard of a tiny device called the “fuck wrench”…
Yeah: https://www.amazon.co.uk/BERGEON-Bergeon-Professional-Cleani...
FIFY
:-)
Learned that lesson the hard way a few decades ago.
MTBF on a WD Green is 1M hours, we’ll replace it at 900K and be golden…
This sounds logical, but I am not sure about it. I certainly make much much more errors based on similar sounding words in English than on my native language. (I believe I make a TON of such errors in English, and almost none in my native language, but hard to tell.)
Obviously many systems have a single point of failure, and can result in lost productivity, but is that designed as it should, or cause catastrophic results like a helicopter crash?
In Japan, motorcycle racing requires lockwire on almost everything. It's a shame helicopter safety engineering generally doesn't meet this basic standard. Although, in fairness, relying on a single spinny thing without an all operational envelope survival passive glide capability is itself inherently dangerous.
The nut was torqued to 3000 ft-lb so this was kind of superfluous. But it does show that the nut was torqued, witnessed, and wired.
I thought helicopters were so expensive because every part had to work and last, or else.
Yes, but the key to why helicopters are expensive is that is that aviation is highly regulated by the government. Individual manufacturers, pilots, airlines, etc. don't get to decide what is "safe enough," they have to obey the standards set by the law. Adhering to the standards of the law requires a lot of process and paperwork.
Just gaslight the regulator and produce the best selling airframe of all time.
Famous among kids who once attended Sunday school programs that asked them to recite a bible verse each Sunday. First kid to go always takes that one.
Amazing joke, I lol'd, fantastic work sir