RTX, P&W parent, posts strong 3Q results

By Scott Hamilton

Oct. 22, 2024, © Leeham News: RTX Corp, the parent of troubled engine maker Pratt & Whitney, posted strong financial results for the third quarter today.

PW continues to struggle with replacing engines plagued by technical defects that have grounded nearly 600 Airbus A320neos worldwide. But year-over-year financial results are markedly improved.

Another subsidiary, Collins Aerospace, which makes a variety of components and interiors, reported higher results YOY.

RTX reported $20.1bn in revenues (+6% YOY)m operating cash flow of $2.5bn, free cash flow of $2bn, and returned $1.1bn of capital to shareholders. Net income was $1.472bn vs a loss of $984m in the prior year.

PW reported $7.2bn in revenue for the period vs a mere $926m in 3Q2023. The operating profit was $557m vs a loss of $2.48bn. Despite all the costs taken against the Geared Turbo Fan engines as PW struggles to replace a defective powder on a large installed fleet, aftermarket maintenance, repair and overhaul work drive the YOY improvements on the commercial side. The defense side of PW also saw a 20% increase in revenues.

Collins is hampered by delays in its interiors division, but revenues were up 7% YOY, largely through a 14% increase in components sales to the military. The commercial aftermarket was up 9%. Collins reported an operating profit of just over $1bn on sales of $7.07bn.

Despite these positive results, investment bank Goldman Sachs reported the results were below consensus.

“Segment Earnings Before Interest and Taxes (EBIT) is below driven by the Collins margin. Revenue is ahead at Pratt, and slightly below at Collins and Raytheon. EBIT is ahead at Pratt and Raytheon and below at Collins. Segment EBIT margin of 11.4% is below implied consensus at 11.9%,” Goldman wrote.

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Bjorn’s Corner: New engine development. Part 28. Wrapup.

By Bjorn Fehrm

October 11, 2024, ©. Leeham News: We have done an article series on why engine development takes longer than airframe development. Part of the reason is that advancements in engine technology can deliver considerably higher fuel consumption reductions than airframe advancements.

The change of engines for the A320 series and 737 MAX delivered a 15% improvement in engine efficiency. In contrast, the airframe improvement was less than half, mainly by stacking cabin seats closer together.

Figure 1. The 4:1 gear ratio Utrafan demonstrator in the Rolls-Royce test cell. Source: Rolls-Royce.

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Bjorn’s Corner: New engine development. Part 25. New versus old, CFM56 vs. LEAP

By Bjorn Fehrm

September 20, 2024, ©. Leeham News: We do an article series about engine development and why it has longer timelines than airframe development. It also carries larger risks of product maturity problems when it enters service than the airframe of an airliner.

In our look at examples of recent developments with problems and these put in a historical perspective, we compare the CFM56 to the LEAP, comparing their reliability and durability.

Figure 1. The CFM56 with its mid-span shrouded titanium fan. Source: CFM.

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Bjorn’s Corner: New engine development. Part 24. New versus old, GTF versus V2500

By Bjorn Fehrm

September 13, 2024, ©. Leeham News: We do an article series about engine development and why it has longer timelines than airframe development. It also carries larger risks of product maturity problems when it enters service than the airframe of an airliner.

We have covered the engine’s different parts and their technology challenges. We now look at some examples of recent developments with problems and put them in a historical perspective.

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Bjorn’s Corner: New engine development. Part 22. High Turbine technologies.

By Bjorn Fehrm

August 30, 2024, ©. Leeham News: We do an article series about engine development and why it has longer timelines than airframe development. It also carries larger risks of product maturity problems when it enters service than the airframe of an airliner.

We reached the turbine part on our way through the engine, where we last looked at high-pressure turbine temperatures. It’s the most stressed part of the engine and, in most cases, decides its durability. To understand why, we look closer at turbine technologies.

Figure 1. Our example engine, the LEAP-1A, is in cross-section with booster to compressor bleed valve area marked with a red circle. Source: CFM.

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Bjorn’s Corner: New engine development. Part 18. Combustors.

By Bjorn Fehrm

August 2, 2024, ©. Leeham News: We do an article series about engine development. The aim is to understand why engine development now has longer timelines than airframe development and carries larger risks of product maturity problems.

To understand why engine development has become a challenging task, we need to understand engine fundamentals and the technologies used for these fundamentals.

We have covered the problem areas of (Figure 1) compression in the compressor and combustion, with its requirements on low Soot and NOx emissions. Now we look at how combustors are designed to achieve such low emissions.

Figure 1. The gas turbine cycle and its parts. Source: Rolls-Royce: The Jet Engine.

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Bjorn’s Corner: New engine development. Part 16. Compressor air use.

By Bjorn Fehrm

July 19, 2024, ©. Leeham News: We do an article series about engine development. The aim is to understand why engine development now has longer timelines than airframe development and carries larger risks of product maturity problems.

To understand why engine development has become a challenging task, we need to understand engine fundamentals and the technologies used for these fundamentals.

We have covered the problem areas of a compressor and how these achieve power-to-air-pressure conversion efficiencies of over 90% by using advanced 3D airflow modeling. Now, we look at the users of the air from the engin’s compressor.

Figure 1. The gas turbine cycle and its parts. Source: Rolls-Royce: The Jet Engine.

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To what extent can the A321XLR replace the Boeing 757, Part 3

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By Bjorn Fehrm

July 11, 2024, © Leeham News: We are comparing the Airbus a321XLR to the Boeing 757 to understand to what extent it can replace the 757 on the longer routes it operates for major airlines like United, American, and Delta.

We have looked at the development and operational history of the aircraft, their Apples-to-Apples capacity and range. Now, we use Leeham’s Aircraft Performance and Cost Model (APCM) to compare the operational costs of the aircraft.

Summary:
  • The Boeing 757-200 has the same passenger capacity as the A321LR/XLR and a larger cargo capacity.
  • Its range can compete with the A321LR but not the XLR. Both beat the 757 on operational economics.

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Bjorn’s Corner: New engine development. Part 13. The compressor.

By Bjorn Fehrm

June 28, 2024, ©. Leeham News: We do an article series about engine development. The aim is to understand why engine development now has longer timelines than airframe development and carries larger risks of product maturity problems.

To understand why engine development has become a challenging task, we need to understand engine fundamentals and the technologies used for these fundamentals.

We have covered the need for the axial speed of the core air to decrease and increase depending on the needs of the core engine’s sections. Now, we will start to look at the different parts of the core in more detail. We start with the compressor.

 

Figure 1. The gas turbine cycle and its parts. Source: Rolls-Royce: The Jet Engine.

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Bjorn’s Corner: New engine development. Part 10. Propeller, Rotor or Fan?

By Bjorn Fehrm

June 7, 2024, ©. Leeham News: We do an article series about engine development. The aim is to understand why engine development now has longer timelines than airframe development and carries larger risks of product maturity problems.

To understand why engine development has become a challenging task, we need to understand engine fundamentals and the technologies used for these fundamentals.

Following the last Corner on airframe integration, several comments were made about the definition of propeller, open rotor, and/or fan. So, we’ll explore this further.

Figure 1. Evolution of Wright Brothers propellers from 1903 to 1905. Source: wright-brothers.org

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