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Opinion: The 40,000-Lb. Question Facing Aircraft Development

RISE propfan

Will engine-makers be enticed to try to meet requirements for the two new notional civil and military aircraft that need an engine that does not yet exist?

Credit: Safran

There are two large unfilled requirements in civil and military aero markets today. Both of these notional new aircraft need an engine that does not yet exist. And the path forward for a new engine in this class is far from clear.

Opportunity One is a new midmarket jetliner. As I and others have been saying for over a decade, (AW&ST March 24, 2014, p. 14), airline fleet planning is increasingly favoring midsize, midrange fragmentation machines. This has resulted in a stream of orders for the Airbus A321neo, which is not perfect for this role but is the only choice in its class.

Boeing CEO David Calhoun’s November 2022 announcement that Boeing would not launch a new jet in this class turned this stream into a flood, with 1,300 orders in 2023 alone. As the chart below shows, the A321neo is now central to the airline industry’s future. Incredibly, 58% of all Airbus jets on backlog, and 34% of all Airbus and Boeing jets on backlog, are A321neos.

New management might well change Boeing’s self-destructive position on a new aircraft in this class. Alternatively, a new market entrant, such as Embraer or JetZero, might try to enter the segment. Airbus could act first, reinforcing its position with a reengined, rewinged A322. Either way, the A321neo would be vulnerable to disruption; even the XLR version does not have the midmarket capabilities the market really wants.

The second opportunity is a new U.S. strategic military airlifter. The C-5 fleet is aging, while C-17 flight hours have exceeded expectations. An emphasis on Pacific operations only will increase both the U.S. military airlift requirement and the strain in the legacy fleet. So, the U.S. Air Force is moving forward on a new C-X program (AW&ST Nov. 7-20, 2022, p. 16). The requirement to lift outsize equipment such as tanks or helicopters means it might look a lot like the previous airlifters.

Coincidentally, both market opportunities call for an engine in the exact same thrust class. Any good midmarket jet designed to beat the A321neo would likely be somewhat more capable than Boeing’s 757, which uses 40,000-lb.-thrust engines. Any new strategic lifter also would require similarly powerful engines, assuming it is a quadjet—the C-17 and C-5 were each built with four 40,000-43,000-lb.-thrust turbofans.

Yet no new engine in that size class is being planned. Not only is nothing in development; nothing is being built. Production ended years ago on both Pratt & Whitney’s PW2000 and Rolls-Royce’s RB211-535. CFM’s Leap 1 and Pratt’s PW1000 geared turbofan families are rated below 35,000 lb. thrust, with no plans to exceed that. A 25,000-lb.-thrust gap exists between those models and the next series of production engines, which start at around 60,000 lb. thrust.

There is clearly a strong case for at least one of the three engine OEMs to invest in a new 40,000-45,000-lb.-thrust engine. But that is where things get complicated. While the consensus is that there will be at least another generation of gas turbine powerplants, no firm agreement exists on its architecture. CFM is pressing ahead with its RISE program, focused on a geared propfan. Pratt and Rolls seem to prefer a ducted engine with a gearbox.

Test results from a RISE propfan will not be known for another few years at least, with GE-Safran aiming for 20% fuel-burn reduction over today’s engines. If Pratt were to launch a larger geared turbofan, or if Rolls were to launch an engine in this class using its UltraFan technology, they could be vulnerable if RISE were to achieve its stated goals.

Or a propfan could be vulnerable if ducted engines are close in performance and score stronger customer preference. In particular, it is not clear whether the military will accept a propfan, for whatever reason. In any event, engine OEMs will be loath to launch a new engine family without clear signals from the airframers. The age of “if we build it, they will come,” as when the original CFM56 engine was launched, are probably over.

There is a positive way to view this problem. Perhaps the impressive rewards presented by these two opportunities will motivate one or more engine OEMs to press ahead with architecture-agnostic technology developments scaled for something in the 40,000-lb.-thrust class—combustors, gearboxes, etc. There would be risk, but the rewards are enticing, too.

Richard Aboulafia

Contributing columnist Richard Aboulafia is managing director at Aerodynamic Advisory. He is based in Washington.

Comments

4 Comments
There won’t be a middle of the market aircraft as there won’t be a 40,000# class engine. Pratt lost money on their PW2000. Rolls only made money on the 535 because it was a small fan derated version of a larger engine. Naturally it consumed 10% more fuel than the Pratt.

Unless the government underwrites a new 40000# class engine there won’t be one. And so far the government has no need.

The PW1000 and Leap powering the 320/1 and 737 probably can’t grow to 40000#. Reliability (an issue already at 30000# class would be miserable at 40000#.
C17 and B757 had same engine, but Im not sure if for future strategic military airlifter they will continue with 4 engines, or they change to twin engines of the existing 80 Klb thtust.
Like McDonnell Aircraft and North American Aviation (NAA), the Boeing Company no longer exists. For new passenger aircraft requirements, designs, and construction.

That was one of the few (if any) strategic business decisions made by the Boeing Company, and that is at least passingly aligned with the company's reality.

Boeing's backlog is the sum of the company's programmatic horizon for the foreseeable future.
As no engine equals no airplane, I believe Mr. Aboulafia is entirely correct. The 757 was and is awesomely adaptable to market opportunities. I flew it some, and rode in the back. The present and trending airline market space has and will most likely continue to need enough of that type of capability to totally validate the business case for a new aircraft of 250-300 thousand pounds. Reliable new engines seem difficult to manage, so those manufacturers should start right now. Design for 50 thousand pounds nominal thrust and use derated versions to serve the new airliner. A theoretically heavy engine won't make a noticeable dent in economics, but it being under-stressed should bring initial reliability while providing data from the operating environment. Growth versions of the jet are going to need all that thrust growth potential, anyway. As to fuselage cross-section, please make it a good bit wider than the old '57. People are bigger now, and aisle width is a safety issue. Also, the baggage holds need to accommodate containers. The next generation of airliners will still be tube-and-wing, and we should anticipate a biggish pair of ducted fans, probably geared, slung underwing, per usual. Other airframe configurations are emerging that might not need symmetrical pairs of engines: three times 50 thousand pounds thrust would enable lots of novel thinking. Aviation has a long history of great engines enabling great aircraft. Here is a major chance for another.