Gnome-Rhône Lambda / Gnome 7 Lambda / Gnome 14 Lambda-Lambda / Oberursel U.0 / Oberursel U.III

Oberursel U.III

The Gnome 7 Lambda was a French designed, seven-cylinder, air-cooled rotary aero engine that was produced under license in Britain and Germany. Powering several World War I era aircraft types it was claimed to produce 80 horsepower (60 kW) from its capacity of 12 litres (720 cubic inches) although recorded figures are lower.

Gnome 7 Lambda

Just under 1,000 units were produced in Britain, the majority (967) by the Daimler Company of Coventry. A 14-cylinder variant was known as the Gnome 14 Lambda-Lambda.

In Germany Motorenfabrik Oberursel license-built the seven-cylinder engine as the Oberursel U.0 and later copied the 14-cylinder design and designated it as the Oberursel U.III.

Gnome 7 Lambda

Variants:
Gnome 7 Lambda
Seven-cylinder, single-row rotary engine.
Gnome 7 Lambda (long stroke)
Increased stroke of 145 mm (5.7 in) to raise the compression ratio to 3.87:1, and total displacement to 12.26 litres.
Gnome 14 Lambda-Lambda
14-cylinder, two-row rotary engine using Lambda cylinders. 160 hp (120 kW).
Motorenfabrik Oberursel U.0
German production of the Gnome 7 Lambda – had a 124mm cylinder bore and 140mm piston stroke for a total displacement of 11.52 litres, external diameter of 1.020 meters.

Applications:

Gnome 7 Lambda
Avro 504
Blackburn Type I
Blériot Parasol
Blériot XI
Bristol Boxkite
Bristol Gordon England G.E.3
Bristol-Coanda Monoplanes
Bristol Coanda T.B.8
Bristol Coanda P.B.8
Bristol Scout
Caudron G.III
Deperdussin Type B
Dunne D.8
Henry Farman F.20
Grahame-White G.W.15
L & P 4
Lowe Marlburian
Nieuport IVG
Nieuport 10
Radley-England Waterplane
Royal Aircraft Factory B.E.3
Royal Aircraft Factory B.E.4
Royal Aircraft Factory B.E.8
Royal Aircraft Factory B.S.1
Royal Aircraft Factory S.E.2
Royal Aircraft Factory S.E.2
Royal Aircraft Factory S.E.4
Short S.37
Short S.38
Short S.41
Short S.60
Short S.70
Sopwith Gordon Bennett Racer
Sopwith Pup
Sopwith Sociable
Sopwith Tabloid
Sopwith Three-Seater
Vickers No.8 Monoplane

Gnome 14 Lambda-Lambda
Avro 510
Royal Aircraft Factory S.E.4
Deperdussin Monocoque
Short S.63
Short S.64
Short S.70
Short S.74
Short S.80
Short S.81
Short S.82

Specifications:

Gnome 7 Lambda
Type: 7-cylinder, single-row, rotary engine
Bore: 124 mm (4.9 in)
Stroke: 140 mm (5.5 in)
Displacement: 11.8 L (721.2 cu in)
Length: 112 cm (44 in)
Diameter: 93 cm (36.6 in)
Dry weight: 96 kg (212 lb)
Valvetrain: Automatic centre-piston inlet valve, overhead exhaust valve (one each per cylinder)
Cooling system: Air-cooled
Reduction gear: Direct drive, right-hand tractor, left-hand pusher
Power output: 50.3 kW (67.5 hp) at 1,250 rpm (maximum power)
Compression ratio: 3.75:1

Gnome-Rhône 7 Gamma / 14 Gamma-Gamma

The Gnome 7 Gamma was a French designed, seven-cylinder, air-cooled rotary aero engine. Powering several pre-World War I era aircraft types it produced 70 horsepower (52 kW) from its capacity of 12 litres (680 cubic inches).

March 1909

A 14-cylinder variant was known as the Gnome 14 Gamma-Gamma.

Variants:
Gnome 7 Gamma
Seven-cylinder, single-row rotary engine.
Weight: 165 lb
Output: 50 hp

Gnome 14 Gamma-Gamma
14-cylinder, two-row rotary engine using Gamma cylinders. 140 hp (104 kW).

Applications:

Gnome 7 Gamma
Blériot XXI
Bristol Biplane Type T
Bristol Prier-Dickson
Henry Farman Biplane
Grahame-White Passenger Biplane VIIc
Handley Page H.P.3
Morane-Borel seaplane
Nieuport Monoplane
Paulhan Biplane
Royal Aircraft Factory B.E.3
Royal Aircraft Factory B.E.4
Short School Biplane
Short S.32
Short S.36
Short S.38
Short S.45
Sopwith Three-Seater
Vickers No.6 Monoplane
Vickers No.8 Monoplane

Gnome 14 Gamma-Gamma
Royal Aircraft Factory B.E.7
Short S.41

Specifications:
Gnome 7 Gamma
Type: 7-cylinder, single-row, rotary engine
Bore: 120 mm (4.7 in)
Stroke: 130 mm (5.1 in)
Displacement: 11.14 L (679.84 cu in)
Length: 112.7 cm (44.4 in)
Diameter: 86.9 cm (34.2 in)
Valvetrain: Automatic centre-piston inlet valve, overhead exhaust valve (one each per cylinder)
Cooling system: Air-cooled
Reduction gear: Direct drive, right-hand tractor, left-hand pusher
Power output: 52.2 kW (70 hp) at 1,200 rpm

Gnome-Rhône

Société des Moteurs Gnôme was founded in 1905 by Louis Seguin. In 1915, this firm merged with the Société des Moteurs Le Rhône, founded three years earlier by Louis Verdet, to form Gnôme & Rhône. While Gnôme had continued to produce rotary engines in the 50 to 100 horsepower range, Rhône had refined its fixed-cylinder engines to produce 200 horsepower. However, both these lines of engines were being outclassed in terms of reliability, economy, or power by several contemporary engine manufacturers.

Seguin brothers of Gnome-Rhone Article

Nevertheless, the two merged companies were quite successful commercially, thanks to licensed production in Great Britain, Russia, the United States, Sweden, Germany, and Japan, as well as joint ventures in Italy and elsewhere.

A number of factors hit Gnôme & Rhône (G&R) hard after the war. A huge tax burden was levied based on the firm’s previous international success. At the same time, a mass of war surplus engines glutted the market.

Unlike its other domestic rivals, Gnôme & Rhône lacked experience in areas apart from aero engines, a market now glutted by thousands of surplus motors. A variety of schemes, from making sewing machines to engines for farm tractors or cars, all failed. In constant francs, the company’s sales in 1921 were almost half those of 1913, though the factories were five times larger, notes one scholar in the journal Entreprise et Histoire. In that year, the already legendary company reduced its employment from 6500 workers to 1200.

Production of motorcycles under the Gnôme & Rhône was one area that produced quite satisfactory results in the marketplace; in fact these machines gained a devoted following. In 1922 the English firm Bristol licensed to G&R the right to produce its powerful air-cooled radial engines producing up to 450 horsepower, as well as the freedom to sell them anywhere in the world except for the United States and the territories of the British Empire. With the support of its banks, G&R was able to retool its workshops to build engines, including the new Jupiter introduced in 1923. At the time, G&R had also taken a significant holding in a French-Romanian airline, which helped establish its engines in Eastern Europe.

Between 1924 and 1928, sales increased more than sixfold. At the same time, the air, sea, and land branches of the French military were deciding their outdated equipment was in need of replacement, hence, another blossoming market at home. Expanding commercial fleets produced still more demand. The radial Jupiter engines earned a reputation for being simple to run and easy to fix, even if in-line and V-8 engines made by Hispano-Suiza and Lorraine-Dietrich were more powerful. A novel program, instituted in 1924, allowed for the lease of the engines for a given number of flight-hours, which relieved designers and manufacturers some of the financial strain associated with bringing out new models of aircraft. The popular Jupiter engine was subsequently licensed for production in several European countries as well as the Soviet Union and Japan.

G&R introduced its K family of engines in 1928. In terms of power, this series culminated in the 750 horsepower 14K licensed to a Soviet factory for eventual use in Antonov transports. G&R’s designers evolved L, M, and N families of engines by 1939; one of the latter achieved 1150 horsepower.

Air power played a determining role World War II, and G&R engines had a significant part to play. The Soviet Union’s Molotov factory was producing 300 licensed G&R engines a month in 1940 for use in biplanes and Sukhoi fighters. In Japan, Mitsui illegally copied the 850 h.p. 14K engine, producing the “Suizei” powerplant found in the Mitsubishi Zeroes that attacked Pearl Harbor. During the Nazi occupation of France, G&R became a subsidiary of BMW. Emmanuel Chadeau writes in Entreprises et Histoire that G&R thereby influenced 16 manufacturers in 14 countries during the war; this off-shore production nearly equalled G&R’s own output of 8,000 motors a year, together accounting for a quarter of the worldwide market.

The high share price that G&R commanded prevented it from being nationalized before the war. However, this did come to pass after the Liberation. SNECMA, la Société nationale d’étude et de construction de moteurs d’aviation, was thus created on May 29, 1945. The company was an amalgamation of diverse design bureaus and workshops; it inherited a work force of 10,000 mostly part-time employees. Along with G&R, Snecma was given some of the factories of the Société des moteurs et automobiles Lorraine, formerly Lorraine-Dietrich, which had been nationalized as la Société nationale des moteurs and had been relegated to making parts for tanks. Some of Snecma’s other facilities had been devoted to the production of German Junkers engines by the thousands during the Nazi occupation. G&R also owned a factory of the Aéroplanes Voisin firm, which had gone bankrupt in 1938.

GM V90

Cycle: 4 stroke
No cylinders: Vee 2
Bore: 97 mm
Stroke: 76 mm
Compression: 8.5
Displacement: 1122 cc
Cooling: air / oil
Ignition: electronic
Reduction: Poly-V belt 2.3/1
Weight: 57 kg
Max pwr: 70 hp at 5800 rpm
Max torque: 131 Nm at 4200 rpm
Price 1998: 89 000 000 L

Gluhareff EMG-300

Mr. Gluhareff pioneered the use of liquid propane as a fuel for jet engines and a series of ultra-light portable one-man-helicopters, MEG-1X, MEG-2X and MEG-3X which were designed and built by his own company, Gluhareff Helicopters Corporation. All of which were powered by the G8-2 Pressure Jet Engine on the blade tip and test flown by Eugene M. Gluhareff.
In 1972 Mr. Gluhareff returned to research and design under his own company name of EMG Engineering in Gardena, California. There he continued his work on the G8-2 Pressure Jet Engines which ranged from five pounds of thrust to 700 pounds of thrust.
Mr. Gluhareff designed, built and tested his own one-man tip jet helicopter, the EMG-300 in the early 90’s. Its successful test flight marked the realization of Mr. Gluhareff’s lifelong dream to design what he called a “Flying Motorcycle”.
The EMG-300 was his last design before his death in 1994, it had completed an initial series of test flights, but was not completely tested at the time of his death.

EMG-300
Engine: 2 x G8-2-20H jet engines 10kg of thrust each
Fuel: liquid propane
Fuel capacity: 70 litres
Rotor diameter: 7.3m
Fuselage length: 4.57m
Height: 2.1m
Empty weight: 109kg
Take-off weight: 208kg
Maximum speed without canopy (est.): 112km/h
Maximum speed with canopy (est.): 193km/h
Range: 280km
Endurance: 2.5hr

Gluhareff MEG-3X

Mr. Gluhareff pioneered the use of liquid propane as a fuel for jet engines and a series of ultra-light portable one-man-helicopters, MEG-1X, MEG-2X and MEG-3X which were designed and built by his own company, Gluhareff Helicopters Corporation. All of which were powered by the G8-2 Pressure Jet Engine on the blade tip and test flown by Eugene M. Gluhareff.
Eugene Gluhareffs tip-mounted G8-2 engine MEG-3X was based on a dish-shaped platform on which the pilot would stand and a two-blade rotor revolving underneath the platform. No commercial development was undertaken.

Gluhareff MEG-2X

Mr. Gluhareff pioneered the use of liquid propane as a fuel for jet engines and a series of ultra-light portable one-man-helicopters, MEG-1X, MEG-2X and MEG-3X which were designed and built by his own company, Gluhareff Helicopters Corporation. All of which were powered by the G8-2 Pressure Jet Engine on the blade tip and test flown by Eugene M. Gluhareff.
The MEG-1X personal strap-on helicopter rig with a tip-mounted G8-2 engine was followed by the MEG-2X which had a two-blade rotor. No commercial development was undertaken.

Gluhareff MEG-1X

Eugene Gluhareff established a development company in 1952 to carry out research into pressure-jet powered light helicopters. Mr. Gluhareff pioneered the use of liquid propane as a fuel for jet engines and a series of ultra-light portable one-man-helicopters, MEG-1X, MEG-2X and MEG-3X which were designed and built by his own company, Gluhareff Helicopters Corporation. All of which were powered by the G8-2 Pressure Jet Engine on the blade tip and test flown by Eugene M. Gluhareff.
He built the MEG-1X personal strap-on helicopter rig which used a single-blade rotor with a tip-mounted G8-2 engine and followed this with the MEG-2X which had a two-blade rotor. No commercial development was undertaken.

MEG-1x
Take-off weight: 104kg
Max speed: 88.5km/h
Hovering ceiling: 1500m
Endurance: 14-18min