Forum: F-35 Lightning II

Why is the F-135's T/W low vs other jet engines?



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thestealthfighterguy
PostPosted: Dec 16, 2011 - 08:11 PM Reply with quote Back to top
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JetTest wrote:
Similar core, not exactly the same. Bigger fan and inlet case, as well as fan duct. No such part as an "engine case".

Yep, Sorry I been building my WV stroker motor. It has a "engine case".
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That_Engine_Guy
PostPosted: Dec 17, 2011 - 12:51 AM Reply with quote Back to top
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thestealthfighterguy wrote:
I've been reading up on the thrust to weight of the newer jet fighter engines.
Rafale M88-2= 18,000 lbs thrust/ 1,978 lbs = T/W 9.1
Eurofighter EJ-200= 20,250 lbs thrust/ 2,180 lbs = T/W 9.3
Raptor F-119= 35,000 lbs thrust/ 3,900 lbs = 9.0
F-35 F-135= 43,000 lbs thrust/ 5,400 lbs =7.96

The F-135 has a very low T/W of only 7.96 to 1. This is lower than some engines built in the 70's and 80's. Why?
This also seems low because it has a inlet temp of 3600 deg. F vs. only 2871 deg and 2700 deg for the M88 and the EJ-200.

What gives? Whatever help you can give would be great. Thank you.


Where did this magic chart come from? Where has anyone ever publicly indicated the F135 weighs anything specific? Last I knew the weight of the engine was still c|@$sified.

No mention on any of PW's pages:
http://www.f135engine.com/proven-tech/e ... cter.shtml
http://www.pw.utc.com/products/military/f135.asp

Our friend J@ne'$ still cites the F135's weight as c|@$$ified as well, though the F135 weight is cited as 'in the 4300lb class' at their site.

If the F136 was suppose to be plug-n-play with the F135 the weights should be almost identical. Otherwise serious weight & balance issues would have been encountered moving from one type to the other.

The F135-PW-600 (as a whole propulsion system) had a 'not to exceed weight' of 6504lbs. My comments on that topic here.

http://www.f-16.net/f-16_forum_viewtopic-t-11547.html

Again, numbers at this point can be VERY misleading (for reason) when it comes to performance. No need to lay all the cards out for public (and foreign competitor/opposition) consumption.

For that matter many of the F119 specifications are still c|@s$ified too.

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TEG

(edit - typo repair)

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sirsapo
PostPosted: Dec 17, 2011 - 02:10 AM Reply with quote Back to top
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I would also doubt that the F135 has a turbine inlet temperature of 3600 degrees Fahrenheit. Its probably more in the ballpark of 3600 Rankine, which would put it in the level of technology of the F119...
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That_Engine_Guy
PostPosted: Dec 17, 2011 - 02:34 AM Reply with quote Back to top
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sirsapo wrote:
I would also doubt that the F135 has a turbine inlet temperature of 3600 degrees Fahrenheit. Its probably more in the ballpark of 3600 Rankine, which would put it in the level of technology of the F119...


I'd say Fahrenheit, as the F100-PW-229's TET runs ~2500*F which is around 3000*R

Our friend J@nE'$ says the F135's "HPT rotates at speeds exceeding 15,000 rpm, generating 47,725 kW (64,000 shp) from gas at just over 1,649°C (3,000°F), cooled by air supplied at 538°C (1,000°F) from the HPC.

That would be a TET of 3459.87 degree Rankine (or 1922.15 kelvin)

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alloycowboy
PostPosted: Dec 17, 2011 - 05:21 AM Reply with quote Back to top
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Who the heck uses Rakine any more??? Some of you might find this interesting. It's a map of countries that still use the British Imperial system.

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popcorn
PostPosted: Dec 17, 2011 - 06:27 AM Reply with quote Back to top
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alloycowboy wrote:
Who the heck uses Rakine any more??? Some of you might find this interesting. It's a map of countries that still use the British Imperial system.


The US and Burma sure make an odd couple..
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PostPosted: Dec 17, 2011 - 06:20 PM Reply with quote Back to top
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That_Engine_Guy
PostPosted: Dec 17, 2011 - 08:35 PM Reply with quote Back to top
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alloycowboy wrote:
Who the heck uses Rakine any more???


I believe gas-turbine engineers use Rakine as it's more related to their operations. (or at least they DID use it when jets were born)

I remember having to convert *R to *F during my early days as an 'engine guy' on 1960s PW turbojets.

If memory serves, there was a chart in the back of our Technical Order to convert the 3 temperature scales to each other. *F / *R / *C

The Pratt & Whitney / UTC Aeronautical Vest-Pocket Handbook - AKA "Little Blue Book" also has a *F / *R / *C conversion table.

Cheers TEG

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fiskerwad
PostPosted: Dec 19, 2011 - 12:15 PM Reply with quote Back to top
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alloycowboy wrote:
Who the heck uses Rakine any more??? Some of you might find this interesting. It's a map of countries that still use the British Imperial system.



So why did I have all those metric wrenches out while putting a water pump on my wife's Ford Explorer? Laughing

Next they will be wanting a metric equivalent for time.

fisk

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delvo
PostPosted: Dec 19, 2011 - 01:49 PM Reply with quote Back to top
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fiskerwad wrote:
Next they will be wanting a metric equivalent for time.
They wanted to, but the committee couldn't agree on whether a year should have 100 days or 1000.
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Pecker
PostPosted: Dec 19, 2011 - 03:48 PM Reply with quote Back to top
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alloycowboy wrote:
Who the heck uses Rakine any more???


Anyone in the gas turbine industry with a vested interest in calculating compressor and/or turbine efficiency but doesn't want to use Kelvin...... Wink

Efficiency calcs require the use of absolute scales of temperature, either from the outset or through intermediate conversions.

Convert F to R by adding 459.67
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