2025/2026 Hybrid Powerunit speculation

[wuzak]

How likely are we to see 450KW~600hp from the engine 54% eff at the start of 2026 season

Unlikely, IMO.

I think they'll be 420-430kW, around 50-52% TE.

[FW17]

How likely are we to see 450KW~600hp from the engine 54% eff at the start of 2026 season

Unlikely, IMO.

I think they'll be 420-430kW, around 50-52% TE.

The last engines hit 51% at start of 2022 season when it was frozen

[wuzak]

How likely are we to see 450KW~600hp from the engine 54% eff at the start of 2026 season

Unlikely, IMO.

I think they'll be 420-430kW, around 50-52% TE.

The last engines hit 51% at start of 2022 season when it was frozen

With turbo-compounding?

[saviour stivala]

How likely are we to see 450KW~600hp from the engine 54% eff at the start of 2026 season

Unlikely, IMO.

I think they'll be 420-430kW, around 50-52% TE.

The last engines hit 51% at start of 2022 season when it was frozen

If you mean '600HP' from the ICE, That in my opinion is likely, Also in my opinion the new power unit will take-off with a better thermal efficiency than the previous best of power unit left of, and progress to maybe 3-4 percentage points more.

[FW17]

Unlikely, IMO.

I think they'll be 420-430kW, around 50-52% TE.

The last engines hit 51% at start of 2022 season when it was frozen

With turbo-compounding?

What compounding?

[wuzak]

The last engines hit 51% at start of 2022 season when it was frozen

With turbo-compounding?

What compounding?

The maximum efficiency was when the MGUH fed power directly to the MGUK.

This is turbo-compounding.

[djos]

With turbo-compounding?

What compounding?

The maximum efficiency was when the MGUH fed power directly to the MGUK.

This is turbo-compounding.

In not sure you understand the definition of the word compounding, you can’t compound a turbo without a second turbine!

[FW17]

With turbo-compounding?

What compounding?

The maximum efficiency was when the MGUH fed power directly to the MGUK.

This is turbo-compounding.

With compounding of MGU H it was 59%

51% was only from ICE

[wuzak]

What compounding?

The maximum efficiency was when the MGUH fed power directly to the MGUK.

This is turbo-compounding.

In not sure you understand the definition of the word compounding, you can’t compound a turbo without a second turbine!

Turbo-compounding is where a turbine feeds power back to the crankshaft of an engine to enhance ouput.

Like the Wright R-3350 turbo-compound engine used in the Douglas DC-7 and some versions of the Lockheed Constellation.

The Wright R-3350 was supercharged, but not turbocharged. It had 3 "power recovery turbines" connected to the crankshaft.

A compound turbo setup uses two, or more, I guess, turbos.

[wuzak]

What compounding?

The maximum efficiency was when the MGUH fed power directly to the MGUK.

This is turbo-compounding.

With compounding of MGU H it was 59%

51% was only from ICE

Was it?

Where is the source for that?

[FW17]

The maximum efficiency was when the MGUH fed power directly to the MGUK.

This is turbo-compounding.

With compounding of MGU H it was 59%

51% was only from ICE

Was it?

Where is the source for that?

Dont know the source, but a lot of online chatter on RA621H being 1014hp

which would be close to 59-60%

[wuzak]

With compounding of MGU H it was 59%

51% was only from ICE

Was it?

Where is the source for that?

Dont know the source, but a lot of online chatter on RA621H being 1014hp

which would be close to 59-60%

That'd be with battery assistance.

You can't count battery assistance in teh thermal efficiency calculation.

1014hp = 854hp from ICE.

Which is about 51% TE for the ICE.

Which is what you said.

Turbo-compounding would not give 160hp to the MGUK without battery assistance.

[BassVirolla]

The maximum efficiency was when the MGUH fed power directly to the MGUK.

This is turbo-compounding.

In not sure you understand the definition of the word compounding, you can’t compound a turbo without a second turbine!

Turbo-compounding is where a turbine feeds power back to the crankshaft of an engine to enhance ouput.

Like the Wright R-3350 turbo-compound engine used in the Douglas DC-7 and some versions of the Lockheed Constellation.

The Wright R-3350 was supercharged, but not turbocharged. It had 3 "power recovery turbines" connected to the crankshaft.

A compound turbo setup uses two, or more, I guess, turbos.

Totally (w)right.

I'd like to note that the MGUH to MGUK is an electrically linked turbo compounding in place of the mechanical link of the Wright PRT.

Sometimes is overlooked (and understated) such electrical compounding link.

[FW17]

Was it?

Where is the source for that?

Dont know the source, but a lot of online chatter on RA621H being 1014hp

which would be close to 59-60%

That'd be with battery assistance.

You can't count battery assistance in teh thermal efficiency calculation.

1014hp = 854hp from ICE.

Which is about 51% TE for the ICE.

Which is what you said.

Turbo-compounding would not give 160hp to the MGUK without battery assistance.

Numbers are clouded on how much the MGU H could generate, so let us say it generated its capacity

[saviour stivala]

The type of turbo compounding used by the formula 1-2025 power unit, ''ETC'' - electric turbocharger, which was a totally different type of compounding to the turbo compounding ''mechanical turbo compounding'' used by the Wright aero engine, could add 160 HP to the crankshaft, and unlike the Wright system, it did not required an extra blow-down exhaust turbine.