Disc reach ultimate material strength by spinning too fast

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Discussion Overview

The discussion revolves around the mechanics of a spinning engine rotor, specifically focusing on the conditions under which the rotor might reach its ultimate yield strength and fail. Participants explore calculations related to the rotor's speed, material properties, and the implications of a real-world incident involving an A380 aircraft.

Discussion Character

  • Technical explanation
  • Mathematical reasoning
  • Debate/contested

Main Points Raised

  • One participant describes a scenario where an A380's engine rotor spins too fast due to a speed limiter failure, leading to material failure, and seeks to calculate the speed at which this occurs.
  • Participants discuss the assumptions made in the calculations, such as the rotor being a perfect disk and the simplification of material properties.
  • Another participant questions the reasonableness of the calculated speed of 263 rad/sec, suggesting it might be a normal operating speed.
  • There is a discussion about where the largest forces act on the rotor, with some suggesting that the inner radius experiences the greatest forces due to inertia.
  • Published reference speeds for engine spools are provided, indicating typical operational RPMs that are significantly lower than the calculated speed.
  • A participant corrects an earlier claim about the A380 incident, providing details about the investigation and clarifying that the aircraft was able to land safely despite the engine issue.

Areas of Agreement / Disagreement

Participants express differing views on the validity of the calculations and the implications of the A380 incident. There is no consensus on the accuracy of the speed calculation or the interpretation of the incident's outcome.

Contextual Notes

Participants note various assumptions in the calculations, including the simplification of the rotor's shape and material properties, which may affect the results. The discussion also highlights the complexity of forces acting on the rotor, which remains unresolved.

swraman
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So, I am watching this show about airline crashes and apparently, a A380 has gone down because the speed limiter on a spinning engine rotor broke, and the part spun so fast its ultimate yield strength was reached and the material shatterted.

Thats got to be one really fast spinning rotor! But how fast? It was made of a nickel alloy, but since I don't know exactly what it is let's use steel. Its safe to assume that the part was lighter and stronger than steel, so this will be an underestimate. I also am going to simplify the shape, assume It is rigid (undergoes no elastic or plastic deformation) untile its ultimate strength is reached.

5500MPa and a material density of 7.8g/cm^3. Let's say for simplicity it is a perfect disk of outer radius 1.5m, inner radius 5cm, thickness 5cm . How would you go about calculating the speed at which it hss to spin to break?

Here's what I did, but I get an answer that makes no sense in the end. Can you see where I am going wrong, or is my entire plan of attack wrong?

t = .05 % thickness
r1 = .05 % inner radius
r2= 1.5 % outer radius
rho = 7800 % density
u = 5500000000% N/m^2

The mass of the disk:
m = rho * (r2^2 - r1^2) * t * 2*pi

I assume initial fracture would be at the inner radius, so the effective area:
area = 2 * pi * r1 * t;

force to keep the mass at bay:
F = .5 * (wr)^2 * dm
= .5 * (wr)^2 * rho * t * 2 * pi * dr

Integrating over r on the range r1 to r2:
F = (pi/3) * w^2 * (r2-r1)^3 * rho * t

So the pressure at the inner surface:
P = F/Area
P = 79264.25 w^2

Set that equal to ultimate stresss, solve for speed:
5500000000 = 79264.25 w^2

And I get 263 rad/sec, which I am assuming is wrong, since that's a very reasonable RPM.

Thanks.
 
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swraman said:
outer radius 1.5m
swraman said:
initial fracture would be at the inner radius
Where are the largest forces?
swraman said:
263 rad/sec ... ... reasonable RPM.
"Reasonable?"
 
The largest forces would be at the inner circle, wouldn't they?

An infinitesimal area at the inner circle has a mass of (m = rho * t * (r2-r1) * dTheta) that is trying to escape due to its inertial, with the radial force of (F = .5 * (wr)^2 * rho * t * dTheta * dr)

By reasonable, I mean that it would be considered a normal operating speed, so my calculation is obviously wrong.
 
From published information :

Sample 100% reference speeds for a Trent series engine :

LP spool N1 2700 rpm
IP spool N2 8200 rpm
HP spool N3 12600 rpm

Note that actual running speeds are less - usually in the range 94 to 98 % .
 
Last edited:
swraman said:
So, I am watching this show about airline crashes and apparently, a A380 has gone down because the speed limiter on a spinning engine rotor broke, and the part spun so fast its ultimate yield strength was reached and the material shatterted.

I think the incident you are describing only damaged the A380 aircraft, which was able to land safely. Since the aircraft was owned by Qantas, the Australian authorities performed an investigation of this incident, and a report of findings was prepared:

https://web.archive.org/web/2015011...ia/2888854/ao-2010-089 preliminary report.pdf

https://en.wikipedia.org/wiki/Qantas_Flight_32

As a result of the investigation, the cause of the engine failure was determined to be a manufacturing defect in one of the Rolls-Royce engines. This particular aircraft underwent some $145 million in repairs and was returned to service. There was no loss of life.
 

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