Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 04-May-2021

This is the surname of Wiktor Narkiewicz (sometimes Viktor), he was a well-known Polish engine designer and Director of Design for AVIA factories before WWII.

-During the war he was in England involved in the design of British engines.

-In Poland he went through IL, OKL y WSK.

-Just after the war he created its own engines, starting with the WN-1 that was manufactured by OKL initials of the Osrodek Konstrukcji Lotniczy, an aeronautical material factory founded around 1957 in Okecie next to Warsaw.

Narkiewicz, WN-3 Power Egg
“WN-3 Power Egg”

-He led the teams that designed the WN-1, WN-3, WN-5, WN-6 with its variants, as well as the WN-7 and -7R engines.

-A horizontally-opposed 2-cylinder and the NP-1 with four cylinders, horizontally-opposed as well.

-The WN-1 was a horizontally-opposed four cylinder, known as PZL-65KM, giving 58/65 CV.

-Interestingly, it was made in 1947 and offered again in the early 1960's by OKL. See more information about these engines on WN and Wiktor Narkiewicz.

-Below we can present the interesting WN-3, a 7 cylinder radial.

Narkiewicz, WN-3 side view
Narkiewicz, WN-3 angled-front view
“WN-3”

-It gave 300/340 hp at 2,500 rpm, and was from 1954. The following year and with reduction gear it reached 450 hp and was then called WN-5 but this one was unsuccessful and did not even go into production.

-The WN-6 had six horizontally-opposed cylinders, and the -6R was the geared version with a maximum power of 220 CV at 3,500 rpm of the crankshaft. The -6S version was a -6R with supercharger to fit on helicopters and other installations.

-That same engine with four cylinders instead of six was the WN-7 that gave 125 CV.. The geared version was the -7R that delivered 145 CV.

-Wiktor Narkiewicz prepared a study for a 1000 shp turboprop and a turbojet for aircraft in development at the time.

Engines of NARKIEWICZ

Model: WN-1

Arquitecture: 4-cylinder Horizontally opposed
Cooling:
Total Displacement:
Bore / Stroke:
Power: 65 CV
Weight:

Other details:
Model: WN-3

Arquitecture: 7-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power: 340 CV @ 2500 rpm
Weight:

Other details:
Model: WN-5

Arquitecture: 7-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power: 450 CV
Weight:

Other details:
Model: WN-6

Arquitecture: 6-cylinder Horizontally opposed
Cooling:
Total Displacement:
Bore / Stroke:
Power: 220 CV @ 3500 rpm
Weight:

Other details:
Model: WN-7, -7R

Arquitecture: 4-cylinder Horizontally opposed
Cooling:
Total Displacement:
Bore / Stroke:
Power: 125 CV
Weight:

Other details:

The author of this edition of Aeroengines AtoZ, through Aeroteca, collaborated on Version 2 of this video, which is presented here.

To understand the operation of the connecting rods, the 1929 Continental R 670 single-cylinder engine was chosen.

A demonstration of Version 3, improved at the author's suggestion, is also available on YouTube at a later date. This version shows bronze valve guides, improved valve spring movement, and the split crankshaft counterweights and front bearing balls also move.

The design is from Juan Soler, Sant Cugat, Barcelona

Below we show a flash of version 3

Counting also with the coloboration of JMC of Enginys Mecanics in Mataro, Barcelona