F-16 Reference
5th Gen Fighters
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ViperEnforcer
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Posted: Jan 10, 2004 - 11:13 AM
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Joined: Dec 25, 2003
Posts: 536
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jetech wrote:
Working 4 months in a backshop does not make an engine troop. I was part of rivit as well and remember how it was. I could crew a jet until an engine problem came up, fix the engine then go back to my jet. Split cases are a good idea, so is a blisk for ease of maintenance, not soo sure on costs. So a F119 has split cases that makes it "feel like a GE"? Like I said both engines have there high points.
The GE isn't really a modular concept, PW used that term years ago so GE has strayed away form that like many other terms such as augmentor/augmenter ignitor/igniter.
Jetech
The GE-132 was installed in my old Jet 359 (Block 30) here at Edwards. It had some balls! Sort of like when we had the upgrade GE-129 out here, and we could not trim it below 33,000Lbs. After a few team meetings with compiled data from both upgraded motors, GE came out on top, not by a landslide but in front. Not sure who is going to get the motor now, and other interest discussed are still classified.
Also, I never said I was an Engine troop, but have worked it enough of both engines to know what's better, all round. Out of all the Engine troops I've known and Rivitised Mechs, most (By a huge majority) prefer GE, and Air Crews even more. Rivet work force helped take the load off the lone Engine troop assigned to the spec flight. Most of my time on the line was spent on replacing LRU's and trouble shooting. My time in backshop was short, but enough to see the break down of the GE motor in detail. GE had its problems when it came out, as did Pratt. Going to a DEC as opposed to the analog AFT Control (eliminating the EMSP) was a little late and ended up more advanced than Pratt's DEEC. Oh yeah, Pratt gave us wonderful AGeTS,
As far as terminology every manufacture gives their own acronyms and terms for their designs, even Pratt contradicts itself with it's 119, as most are similar to the GE; FADEC, Aug Igniter, VSV, Fan core Dist...... and even some of the power modes. And no, just because it is "Top-Halfed" like the GE, is not the only way it feels like a GE. No more AIR for nozzle operation either. Even running it has it's similarities.
GE is a modular design. It may not be a new concept, but it is. Pratt does to, but not the same level at GE. Like you said, each Engine has it's high points, but GE just has more. And don't think I am a GE spokesboy since you implied I feel maintenance on it was "Blisk for Ease", cause I sure the hell have spent my fair share of 15 hour nights working both motors.
Everyone has there preference, I guess I am with the majority on this one. When I was in QA/ ACFT Invt. team (Osan 02-03), I was able to research back some 8 years back, and found that Pratt(all versions combined) had more engine related (Failures) F-16 crashes than GE, by 4-1. Hell, Luke planted 7 within a 3 year frame.
Mike V. |
_________________ If it yanks, banks, turns, and burns, Crew Chiefs made it happen!
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STBYGAIN
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Posted: Jan 10, 2004 - 01:45 PM
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Joined: Jun 13, 2003
Posts: 188
Location: RJSM -- Japan
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| I've flown both the PW220 and the GE129. I'll take the GE any day of the week and twice on Sundays. The difference is night and day. As far as maintenance, I notice a few more squawks with the GE than the PW, but not enough to really make a difference. |
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jetech
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Posted: Jan 10, 2004 - 03:39 PM
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Newbie

Joined: Jan 07, 2004
Posts: 18
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ViperEnforcer wrote:
The GE-132 was installed in my old Jet 359 (Block 30) here at Edwards. It had some balls! Sort of like when we had the upgrade GE-129 out here, and we could not trim it below 33,000Lbs. After a few team meetings with compiled data from both upgraded motors, GE came out on top, not by a landslide but in front. Not sure who is going to get the motor now, and other interest discussed are still classified.
Also, I never said I was an Engine troop, but have worked it enough of both engines to know what's better, all round. Out of all the Engine troops I've known and Rivitised Mechs, most (By a huge majority) prefer GE, and Air Crews even more. Rivet work force helped take the load off the lone Engine troop assigned to the spec flight. Most of my time on the line was spent on replacing LRU's and trouble shooting. My time in backshop was short, but enough to see the break down of the GE motor in detail. GE had its problems when it came out, as did Pratt. Going to a DEC as opposed to the analog AFT Control (eliminating the EMSP) was a little late and ended up more advanced than Pratt's DEEC. Oh yeah, Pratt gave us wonderful AGeTS,
As far as terminology every manufacture gives their own acronyms and terms for their designs, even Pratt contradicts itself with it's 119, as most are similar to the GE; FADEC, Aug Igniter, VSV, Fan core Dist...... and even some of the power modes. And no, just because it is "Top-Halfed" like the GE, is not the only way it feels like a GE. No more AIR for nozzle operation either. Even running it has it's similarities.
GE is a modular design. It may not be a new concept, but it is. Pratt does to, but not the same level at GE. Like you said, each Engine has it's high points, but GE just has more. And don't think I am a GE spokesboy since you implied I feel maintenance on it was "Blisk for Ease", cause I sure the hell have spent my fair share of 15 hour nights working both motors.
Everyone has there preference, I guess I am with the majority on this one. When I was in QA/ ACFT Invt. team (Osan 02-03), I was able to research back some 8 years back, and found that Pratt(all versions combined) had more engine related (Failures) F-16 crashes than GE, by 4-1. Hell, Luke planted 7 within a 3 year frame.
Mike V.
The -132 is capable of being trimmed bwlow its 32,000 rating, its one of their selling points for increased durability. So tell me how is a DEC more advanced than a DEEC? GE's still have to use a EMSC where a PW is all engine contained and in time the EDU will not be needed the DEEC will do it all. Oh and how far back are you quoting AGETS? I have my time with AGETS, and that was probably prior to GE even being in a F-16, a little far back to be throwing stones at PW don't you think? Were you even in the AF when AGETS was around?
I dont have experience with the F119 so I can't give a take on that.
You will not find "modular concept" in any books by GE. To access mid sump on a F110 you drop gearbox, fan cases, remove fan rotor. That is not a modular concept. Argue as you will it just isnt modular. I never implied you felt the blisk was for ease of maintenance, that is why the blisk is there, its easier to swap a blisk, until you have to balance things.
I too worked Osan QA and so how long ago were PW in the F-16's there? I dont know but guessing 10-15 years ago at least. Again quoting pretty old history of PW. Were they even -220's or the ancient -200's?
And as for Luke losing 7 aircraft, if this was solely the blame of PW don't you think other bases would have similar problems? There is more to it than just 7 PW equipped jets crashed.
Lets not forget minor nicks on F110 fan blades causing blade liberation. Blending on a PW can be crude as hell and never cause a blade to fail.
To each their own opinion, I just dont feel either is absolutley the "best" as you do. Each has their good ideas.
Jetech |
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STBYGAIN
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Posted: Jan 10, 2004 - 03:52 PM
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Joined: Jun 13, 2003
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Quote:
And as for Luke losing 7 aircraft, if this was solely the blame of PW don't you think other bases would have similar problems? There is more to it than just 7 PW equipped jets crashed.
As a pilot, I've spent probably a cumulative hour in the engine shop in my life. Luke's mishaps during this span were a result of liberated nozzles due to a segmented augmenter duct rather than a solid, chemically milled piece. I have heard that the edges on some spot welding would become superheated, causing the whole augmenter duct to liberate, and thus reducing LPT pressure resulting in engine stalls. I believe most of Luke's 220s have been retrofitted with solid-piece ducts, but there are a few jets on the line without it and it says so in the 781. |
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ViperEnforcer
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Posted: Jan 11, 2004 - 05:21 PM
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Joined: Dec 25, 2003
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jetech wrote:
The -132 is capable of being trimmed bwlow its 32,000 rating, its one of their selling points for increased durability. So tell me how is a DEC more advanced than a DEEC? GE's still have to use a EMSC where a PW is all engine contained and in time the EDU will not be needed the DEEC will do it all. Oh and how far back are you quoting AGETS? I have my time with AGETS, and that was probably prior to GE even being in a F-16, a little far back to be throwing stones at PW don't you think? Were you even in the AF when AGETS was around?
I dont have experience with the F119 so I can't give a take on that.
You will not find "modular concept" in any books by GE. To access mid sump on a F110 you drop gearbox, fan cases, remove fan rotor. That is not a modular concept. Argue as you will it just isnt modular. I never implied you felt the blisk was for ease of maintenance, that is why the blisk is there, its easier to swap a blisk, until you have to balance things.
I too worked Osan QA and so how long ago were PW in the F-16's there? I dont know but guessing 10-15 years ago at least. Again quoting pretty old history of PW. Were they even -220's or the ancient -200's?
And as for Luke losing 7 aircraft, if this was solely the blame of PW don't you think other bases would have similar problems? There is more to it than just 7 PW equipped jets crashed.
Lets not forget minor nicks on F110 fan blades causing blade liberation. Blending on a PW can be crude as hell and never cause a blade to fail.
To each their own opinion, I just dont feel either is absolutley the "best" as you do. Each has their good ideas.
Jetech
We had the -132 pushing 34,000 on the thrust pad out here. Most of the time the engines push more than thier ratings Even the -229 was close to 30,000, & the -129 32,000 we when had them clamped down. The 119 is way under rated itself, so you can imagine 35,000 plus, what a power house it is!
The DEC offers more modes, Pri/Sec/Hybrid/Hybrid VSV and when came full authority engine operation. The DEEC (By the Pratt tech rep) was not a redundant and tasked as the DEC. It was not until the F_119 did it receive a Full up DEC. Once the Engineers got to time coefficients, Mach speed, EPLA/PLA differentiation, ACFT Intergration (Here the -229 had problems) got a little to in depth,and Yes the EMSC is located I the acft (PDU bay) but it has the same basic function as the EDU. Downloads are come from both respectively but I was able to retrieve more useable data with the GE CEDS. GE made trouble shooting more practical that Pratt, and many of the guys I worked with over the last 14 years can attest to this. AGETS was old, but not that old. It was still being used at NEllis (Block 25's till the 220E mod)when I got there in 91 and at Edwards when I first came here!
As far as the 4-1 issue, like I mentioned it was based on all Pratts, which at the time was 200 (small percentage, as was the -229) /220/220E/&229. Yes, other bases (mostly Guard) had there problems, but again, by the math alone. Luke has about 200 F-16's all Pratt powered, so the "7" lost to engine failure of one kind or another, then yeah that would be a blamed on the Pratt motor. So what would be more to it? The Air Force is stats and graph oriented, and that's what it was in full Power Point!
Yeah, fan blades for GE (mainly with the P3 blades) were critical, but in most cases blendable, and if not then it had to be R2. But at leas their turbine blades didn't burn away, and nozzles blow apart like Pratts. Also, GE is pumping allot more thrust through the a$$ end as well. I remember the CENC cable problems we had at Nellis, and not to mention the nozzle was worse to work on thean GE's.
Yes, everyone has their opinion, but from all my years in, I found GE to be the more popular choice. While I like a few things on Pratt I found GE more practical to work on. Funny though, one of my long time best firens is hung up on Pratts too. All in fun, we tens to rag him about
Mike V |
_________________ If it yanks, banks, turns, and burns, Crew Chiefs made it happen!
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jetech
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Posted: Jan 27, 2004 - 07:20 PM
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Joined: Jan 07, 2004
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bix wrote:
Engine types for the "C's" hold to the following rule
Ends in 0 - GE
Ends in 2 - PW
32, 42, 52, 62 - PW
30, 40, 50, 50 - GE
I'm not sure about the GE's but the PW's are as follows,
32/42 - F100-220
52 - F100-229
Our ANG unit has 42's and is one of three ANG units converting their 42's to -229 engines.
From information I've seen during the conversion a -229 equiped Block 42 has the HIGHEST thrust to weight ratio of ANY F-16C. Based on the dry weight of the aircraft/engine and the thrust produced.
The PW-229 engines are now almost completely maintainable at the base level not unlike the GE's
In my opinion the PW is a better engine, it may cost more, and require a little more work, but pound for pound it makes more power and is more reliable. It can absorb more damage, and tolerate more malfunction to still get the aircraft/pilot back to base. (That just cost me another 2 cents!)
Yea the block 30-60 is easy. The area that is a bit more vague is in the earlier blocks, and 200 or -220 engines.
Don't get the crew chiefs rattled here you will get another GE vs PW battle.
Jetech |
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elp
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Posted: Jan 27, 2004 - 07:32 PM
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F-16.net Editor

Joined: Sep 23, 2003
Posts: 2862
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Quote:
Don't get the crew chiefs rattled here you will get another GE vs PW battle.
Jetech
Cage match.... "Get Ready to Ruuuummmmmblllle" Sponsored by: GE and PW  |
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jetech
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Posted: Jan 27, 2004 - 10:13 PM
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bix wrote:
No kidding, I've started into that battle under the -129/-229 forum. Proves to be fun!
Would be interesting for a fly-off between identical block 50/52's but I don't think the USAF would allow it.
Would bring up the old F-14/F-15 fly-off data that wasn't released in the early 70's.........or was it? Seems someone in Congress didn't want to buy both? But I'm sure that would be at a different web site........
You must be in the Toledo ANG? F/L or shop? How are the -229's working out vs the -220's ? I worked both in JEIM. 229's in the viper seem to do pretty well. They seem to get beat up in the eagle though.
Jetech |
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elp
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Posted: Jan 28, 2004 - 02:04 AM
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Joined: Sep 23, 2003
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| Cool Bix, I used to live in Toledo 95-99. Only good thing about the airport is going to see the F-16s across the runway. |
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habu2
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Posted: Jan 28, 2004 - 04:27 AM
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Quote:
Would bring up the old F-14/F-15 fly-off data that wasn't released in the early 70's.........or was it?
How about the F-4 vs F-110 flyoff? Dead heat I'd say...  |
_________________ Reality Is For People Who Can't Handle Simulation
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91boost
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Posted: Jan 31, 2004 - 05:33 AM
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ViperEnforcer wrote:
GE Engineers designed it!
Um, actually they didn't....at least the turbine section they didn't. But, kind of humorously, alot of them ended up working for GE after the LME division dismantlement.
Mark
Stuart, FL |
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ViperEnforcer
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Posted: Jan 31, 2004 - 06:45 AM
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Nah, many Ex- GE Engineers were on the F-119 design, hell I work with field ones every day. Being heavily involved in this part of the program, you get more insight to the big picture than usual.
Mike V |
_________________ If it yanks, banks, turns, and burns, Crew Chiefs made it happen!
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91boost
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Posted: Jan 31, 2004 - 08:06 AM
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ViperEnforcer wrote:
Being heavily involved in this part of the program, you get more insight to the big picture than usual.
Big picture, yes. I only have experience in a small part of the design- the HPT and LPT turbine. I can say for a fact that no(or VERY few) former GE engineers worked on designing this part of the motor. |
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snapshot
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Posted: Jan 31, 2004 - 02:10 PM
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Quote:
It is not clear exactly what F-16A's with Pratt -200's were rebuilt as 220E's. Even here at Edwards, onl;y about 3 of our F-16B's wee moded. Also note that F-16C block 25's still came off the production line with -200's. Now, just about all of that block F-16 in service has been retrofitted with the 220E.
Hi Jetech,
We all know the F-100-PW-100 or ?200 series had some teething troubles until the fielding of the ?220 and its DECS (or DEEC) back in 1986.
Is that true that the early engines, though very powerful, could more frequently develop compressor stalls when going from idle to full afterburner very quickly ?
What about a -100 or ?200 series going from idle to AB in some 8 seconds, instead of 4,5 sec for the newer engines ? Is that a correct information ? Did F-16A pilots have to wait until the advent of the DECS to confidently slam the engines from whatever power ?
As a comparison, the R-29B engine as used by the MiG-23 fighter has a very short power response capability (around 4 sec), though it is a turbojet and the aircraft variable geometry air intakes look very similar to those of baby F-4.
Comments on that appreciated...thanks in advance.  |
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