Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 23-Oct-2018

(see Svenska Flygmotor AB and Volvo Flygmotor AB).

Svenska Flygmotor AB is known in most cases as "Flygmotor" although the correct name is the complete reference.

-The company was founded in 1930 as "Nohab Flygmotor Fabriken AB" building the Bristol Pegasus I as model "My VI".

-In 1941 the company was renamed "Svenska Flygmotor" being AB Volvo its largest shareholder.

-During WWII they made radial engines (see Volvo) from American interned aircraft that entered Swedish territory.

-The engine that is discussed is the Pratt & Whitney R-1830, version S1C3-G. The Twin Wasp.

Flygmotor STW-C3
"Flygmotor STW-C3"

-It also had 14 cylinders in two coupled rows of 7 cylinders, with gear and supercharger.

-The main text explains how this engine was made in Sweden.

-Hereafter the DH Ghost-45 was made for the Saab 29 aircraft.

-The Saab32A Lansen plane was powered by RM-5 engines, which was none other than the Rolls-Royce Avon RA.7R.

Flygmotor RM-6
"RM-6"

-It had an afterburner and was also mounted on the Draken, Saab-35A, B and C, a curious supersonic fighter aircraft with double delta wing.

-The Avon 300 series were manufactured as RM-6C for the Draken-35D, E and F.

-The RM-8 was a Pratt & Whitney JT8D-22 intended for the Viggen planes.

-The RM-8 had afterburner, variable nozzle, thrust reversers, and reached 12,000 Kgs (26,400 lbs.) of thrust with these heavy attachments.

-From the RM-8 there are the A and B versions.

Flygmotor RM-8
"RM-8"

-The RM-12 was the GE F-404 turbofan built under license for the Grippen aircraft.

-With GE it intervenes in the CF-6 engine for airline aircraft.

Flygmotor RM-12
"RM-12"

-With Garrett, Flygmotor developed the TFE-1042, the TFE-731-5 and the TPE-331 turboprop.

-Formerly in 1957 and in collaboration with the Bristol, ramjets were manufactured: the RRX-1, RR-2, etc.

Flygmotor VR-3
"VR-3"

-The VR-3 engine for liquid fuels used simple aviation gasoline and hydrogen peroxide as an oxidant -comburent-.

-It had controllable thrust with its maximum in the range of 4,800 lbf.

Flygmotor VR-35
"VR-35"

-The VR-35 with its fuels and oxidizers already preloaded for immediate use, used nitric acid and Hydyne as propellants, with the advantage of not leaving smoke or signs on its trajectory.

Hybrid-fuel rocket engine
"Hybrid-fuel rocket engine"

-As it is natural, like Onera, SEPR, GE, UTC, etc, Svenska Flygmotor has tested proposals for rocket engines of all kinds: solids, liquids and litergol hybrids, that is, liquid comburent (nitric acid fuming) and solid propellants with hypergolic properties such as the amines of the aromatic series - triethylamine or xylidine - but not with polymers.

-SFA Volvo is currently building the Ariane 4 engines, within the large European consortium.

From Appendix 6: See Svenska Flygmotor as well.

-The horizontally-opposed four-cylinder engine was presented at the 1941 Paris Air Show and was intended to be mounted on the Saab Saphir training aircraft. It delivered 140/150 CV of power.

Flygmotor F-451-A
"Flygmotor F-451-A"

Engines of FLYGMOTOR

Model: DH Ghost-45 (Lic.)

Arquitecture:
Cooling:
Total Displacement:
Bore / Stroke: x
Power:
Weight:

Other details:
Model: F-451A, 140/150 HP. 4 cyl. boxer

Arquitecture:
Cooling:
Total Displacement:
Bore / Stroke: x
Power:
Weight:

Other details:
Model: HR-4, motor cohete

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: My-VI, My XXIV (Bristol Pegasus I, Lic.)

Arquitecture:
Cooling:
Total Displacement:
Bore / Stroke: x
Power:
Weight:

Other details:
Model: PW, R-1830 (Lic.)

Arquitecture:
Cooling:
Total Displacement:
Bore / Stroke: x
Power:
Weight:

Other details:
Model: RM-12, (GE F-404, Lic.)

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:

Other details:
Model: RM-5 (RR-Avon RA7C, Lic.)

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:

Other details:
Model: RM-6C (RR-Avon serie 300, Lic.)

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:

Other details:
Model: RM-8 ((PW, JT8D-22, Lic.)

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:

Other details:
Model: RR-2, estatoreactor

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: RR-5, estatoreactor

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: RRX-1, estatoreactor

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: TF-1042 Col. con Garrett)

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: VR-3/35 motor cohete

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
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