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A Defense Technology Blog
ADVENT on show

One highlight in the exhibition hall at this year’s AIAA Joint Propulsion Conference in Denver, Colorado was an updated cutaway model of the U.S. Air Force Research Lab’s ADVENT (adaptive versatile engine technology) future strike/persistent engagement aircraft engine. Unlike earlier models, this latest version is rendered in a lighter plastic which makes for better photography of the innards.

The feature to notice most about ADVENT is the unusual extra duct for bypass air seen running along the top and bottom of the engine. This is the critical third flowpath which will be opened or closed as part of a variable cycle to transform it from a strike aircraft engine to a transport-type engine, or vice-versa. If the flowpath is open the bypass ratio will increase, reducing fuel burn, and enabling range to increase in a subsonic strike engine by 40% and loiter time by up to 60%. If the ducts are closed, additional air is forced through the core and high pressure compressor, enabling thrust and speed to increase.

 

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Front (above) and back (below)

 

 

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(Guy Norris photos)

 

The impact is even more dramatic on the more extreme cycle of a supersonic strike engine. With ducts closed for maximum performance in the combat zone, the flow would be opened up again for the transit to and from the target, resulting in increased engine efficiencies which would give up to an 80% range increase and a staggering 135% increase in loiter time.

Unfortunately there was no model on show of HEETE (highly efficient embedded turbine engine), the advanced engine aimed at producing similar range, payload and loiter time improvements for transport and persistent ISR aircraft. The new core of HEETE, which will feature a pressure ratio rumored to be in the 70:1 range, is what’s causing all the excitement. A leap beyond the advanced compressors on fifth generation high bypass turbofans like the GEnx and Rolls-Royce Trent 1000, it could give US engine makers – military and civil – an unbeatable advantage in the next decade and beyond.

For AFRL there’s more to come when ADVENT and HEETE are combined in around seven or eight years time to produce AD-HEETE. “That’s the whole enchilada,” exclaims AFRL engine division chief engineer Bill Koop.

My colleague Graham Warwick and I only had one issue with the new model – from time to time the ADVENT was prone to seizing up violently as if in the grip of the world’s most destructive surge. We were sure the stand manager was last seen heading off to find that most reliable of high-tech engine solutions – a can of WD 40.
Tags: ar99ADVENTAFRLHEETEUSAF
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Bill Sweetman wrote:
Dude, it's stereolithography. The fact that it works at all is amazing. WD-40 might attack the plastic, though - speaking from experience with the notoriously difficult Revell 1/40th Skyraider, a light veggie oil could be better.
8/6/2009 9:26 AM CDT
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more pics please!
8/6/2009 12:37 PM CDT
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sferrin wrote:
Video would be cool too!
8/6/2009 12:39 PM CDT
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Marcase wrote:
A pressure ratio of 70:1 ?! Now that, is one cool piece of engineering. Now all that needs to be done is hoping that it will be available this century, survives the usual Nunn-McCurdy, and be included in the supplementals.
8/6/2009 2:36 PM CDT
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jetcal1 wrote:
As an old engine guy a couple of things really stand out.
1. The combustion section is really small
2. By-pass? What by-pass?
3. The blade count on and angles on the compressor look very unorthodox
4. Ditto for the last turbine stages
5. How many shafts does this bad boy have?
6. Look Ma, no support for my bearings
7. The secondary and tertiary cooling for the tail appear to be asymmetric (photo angle maybe?)
8/6/2009 3:28 PM CDT
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jetcal1 - Guy may give a better answer, but here goes:

0 - this is a conceptual model for public display: it is NOT either the GE or the R-R ADVENT

1 - length (= weight) is critical, particuarly with the serpentine inlets and exhausts, so everything is as short as it can be. Also the core is smaller because the pressure ratio is higher - the compressor is squeezing the air into a smaller space

2 - there are two flowpaths that bypass the core. Today's fighter engines are described as low-bypass turbofans, but they are more like "leaky turbojets" - this one just leaks a bit more in certain modes

3 and 4 - see 0, and I seem to remember the unusual-looking stages are stators, not rotors, but they have learned a lot about assymmetry through the F135, so I would not be surprised if blade and vane row counts are not what one us used to seeing

5 - two shafts, counter-rotating

6 - that's what the funny-looking stator stages are there for (you can see how they extend out to the cases)

7 - the cooling plenum on this model varies in size from top to bottom becase basically it fills the gap between the outer mould line and the walls of the serpertine exhaust. But air would circulate around the plenum, and this engine would clearly pump a lot of cooling air when it's needed.
8/6/2009 6:11 PM CDT
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Bobbymike wrote:
Awesome technology, hope to see it on Gen 6 F/A type aircraft and NGB in the next decade or two.
8/6/2009 11:56 PM CDT
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It was going to miss NGB by a couple of years when it was the "2018 bomber", but with the delay an ADVENT technology engine could be ready when, and if, the next bomber comes along. It would give you some very interesting capabilities.
8/7/2009 8:03 AM CDT
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