Monthly Archives: April 2021

Guidobaldi-front-left

Guidobaldi 1939 Tilting-Body Prototype Racer

By William Pearce

Francois Guidobaldi was born in 1888 and lived in Antibes, France, near Nice and the Italian boarder. In the early 1900s, Guidobaldi became a cycling champion and started to focus on mechanics and engineering. He filed around 28 patents over his lifetime, with a carburetor for automobiles being one of the first, awarded in 1912. In the late 1920s and early 1930s, Guidobaldi was a team mechanic for Benoît Falchetto, who drove Bugatti racers. During that same period, Guidobaldi either founded or worked for the Société anonyme, moteurs à explosion pour aviation, marine et automobiles (MEAMA / the Combustion Engines for Aviation, Marine and Automobiles Corporation), at which he designed and built an air-cooled, two-row, 10-cylinder aircraft engine.

Guidobaldi-front-left

Francois Guidobaldi started work on his race car in 1939, and it took two decades to finish. Looking similar to a late 1930s Auto Union Grand Prix racer, the car’s body hides its unusual suspension system that enabled the chassis to lean into turns and its custom two-stroke, air-cooled, eight-cylinder radial engine. (Cyril de Plater image)

After lengthy consideration and planning in the mid-1930s, Guidobaldi began work on a race car. Guidobaldi’s car would incorporate a number of his ideas on how to improve handling—namely, the body and wheels would tilt in toward the curve when the vehicle was in a turn. This lean would help minimize lateral g-forces and improve the vehicle’s stability. Work on Guidobaldi’s engine design and the car’s chassis development started around 1939. The car’s basic mid-engine layout was similar to that of the Auto Union Grand Prix racers that were very successful in the late 1930s. However, the outbreak of World War II and material shortages after the war caused Guidobaldi to make slow progress on his car, which at times was called the “Guidomobile.”

They chassis of Guidobaldi’s car consisted of two large tubular steel side rails connected by various cross members. Triangular structures at the front and rear of the chassis attached it to the vehicle’s independent suspension. The suspension consisted of a series of rubber dampers sandwiched between steel plates. The chassis mounting point near the top of the triangular suspension structure enabled the chassis to hang and swing like a pendulum from the mount. While in a turn, centrifugal force would swing the chassis and prevent the buildup of lateral g-forces. At the same time, the suspension was engineered so that it would articulate with the body and the steering so that the tires leaned into the turn. The net result of the design was that the car took turns somewhat like a motorcycle. Strong springs connecting the upper suspension links to the chassis centered the chassis when the vehicle was traveling in a straight line and helped moderate the centrifugal effect when in a curve.

Guidobaldi-1955

This picture appeared in a French newspaper in 1951. However, if Francois Guidobaldi is in the driver’s seat, he is much too young for the picture to have been taken in 1951. It is possible that the picture was taken much earlier and near the start of the car’s construction in 1939. Note the angle of the chassis and rear tires as they lean into the turn.

The driver sat in a low cockpit at the center of the car. The gas tank was located behind the cockpit and extended forward along both sides of the driver at the bottom of the cockpit. The engine was positioned between the fuel tank and the rear suspension mount. Mounts for the engine were clamped to the tubular frame rails. The three-speed transaxle with reverse gear was positioned under the rear suspension mount. At all four corners, the car had Bugatti knock-off wheels and Bugatti finned drum brakes.

Perhaps the only thing more unusual than the car’s leaning chassis was its engine. Guidobaldi designed, built, and installed into his car a two-stroke, eight-cylinder, air-cooled radial engine. The engine was placed horizontally (crankshaft was vertical) to get the car’s center of gravity as low as possible. From the drive side of the engine (under the car), a shaft extended forward to power two Roots-type superchargers built by Bugatti, and another shaft extended to the rear to power the transaxle. Two Guidobaldi-designed carburetors added the fuel. From the supercharger, the air and fuel mixture was delivered to the cylinders via intake manifolds under the car.

Guidobaldi-engine

The “Guidomobile’s” engine package being tested. Laying a radial engine flat provided a low center of gravity, but it also complicated the drive arrangement. The two Bugatti superchargers on the left were driven via a single shaft from the engine. Note the individual exhaust stacks above the frame rail.

Intake and exhaust ports were on the drive side of the engine, facing the ground. An intake valve was positioned in each cylinder head and controlled via a rocker and pushrod by a cam ring atop the engine. The exhaust port was located on the cylinder just below the intake port. The flow of exhaust was controlled by the piston uncovering and covering the port. Exhaust from each cylinder flowed into an exhaust stack, with four stacks exiting horizontally on each side of the car. Two magnetos were mounted horizontally on the top (non-drive) side of the engine. Each magneto fired one of the two spark plugs mounted in the cylinder and flanking the intake valve. The engine was started via a remote starter engaged through the transaxle at the rear of the car.

The engine’s exact displacement is a bit of a mystery. One publication lists the bore and stroke as 2.36 in (60 mm), which would give a displacement of 83 cu in (1.36 L). However, many other publications state the engine’s displacement was either 61 or 67 cu in (1.0 or 1.1 L), which would result in a bore and stroke of approximately 2.17 in (55 mm). The engine was later enlarged to 91 cu in (1.5 L). If the bore and stroke were originally 2.36 in (60 mm), the bore would have been increased to 2.48 in (63 mm) to achieve a total displacement of 91 cu in (1.5 L). However, if the bore and stroke were originally 2.17 in (55 mm), then the bore would need to be increased to 2.60 in (66 mm) to reach a displacement of 91 cu in (1.5 L). It seems more reasonable to increase the bore of the air-cooled cylinders by .12 in (3 mm) than it does by .43 in (11 mm). Regardless of its actual displacement, the engine produced 180 hp (132 kW) at 6,500 hp in its original form. The engine’s power rating at 91 cu in (1.5 L) has not been found, but was presumably around 200 hp (147 kW). At some point after 1960, the two Bugatti superchargers were replaced by a single Roots supercharger of Guidobaldi’s own design.

Guidobaldi-car-1956

The bodiless “Guidomobile” on display at the Exposition Automobile de Nice in 1956. An aged Francois Guidobaldi stands at center holding his hat. The triangular suspension structures are apparent, as is the low-mounted engine. The circular mounts near the top of the suspension structures are the pivot points for the chassis, allowing it to swing.

Guidobaldi built the car almost entirely by himself, even making wooden cores to create clay molds for casting parts. The main structure of the chassis was seemingly complete by 1951, and the unbodied car was displayed at the Exposition Automobile de Nice in 1956. Some sources state the Guidobaldi undertook test drives in the late 1950s on the winding roads in the Maritime Alps. There are accounts that the car gave an unsettling ride while traversing curvy roads. The chassis would rise and fall as the suspension leaned back and forth, subjecting driver to movement in all directions. It is not clear when the aluminum body was added to the car, and no pictures of the original body have been found. A new body was constructed in 2010 when the car was restored. The new body reportedly follows the aesthetics of the original body, which had been badly damaged over the years.

The aluminum body built in 2010 covers the entire chassis. Large cutouts are present by each wheel to allow room for the suspension’s travel. A number of inlets provide ample cooling air to the engine. Air from the from grille passes through the entire body. A large scoop on each side of the car, just behind the front wheels, delivers cooling air to the engine. Two smaller scoops atop the engine cowling provide further cooling. A number of louvers behind the engine help the heated air leave the engine compartment. During the 2010 restoration, the exhaust stacks were lengthened and turned up 90 degrees to exit the top of the car’s sides.

Guidobaldi-right-side

Side view of Guidobaldi’s restored car illustrates the cooling air scoops just behind the front wheel and on the side of the engine compartment. Note the numerous louvers and vertical exhaust stacks. The fuel filler cap is just behind the driver’s headrest. (Cyril de Plater image)

Guidobaldi had always planned to build a passenger car using the same leaning chassis concept, but no such car was ever built. In the 1960s, a number of automobile manufacturers had an interest in Guidobaldi’s car. Perhaps the most interested was Mercedes-Benz, but negotiations failed to yield any agreement. Guidobaldi predicted his race car could achieve a top speed of 174 mph (280 km/h) and had eyed Formula 1 as a testing ground, but a lack of funds curtailed his aspirations. The expenses of building the car and filing patents left Guidobaldi with little extra money. On 6 August 1971, Guidobaldi passed away. His car had already been locked away and nearly forgotten.

In 1980, Antoine Raffaelli purchased the car from Guidobaldi’s son, Virgile. The car was then sold to Adrien Maeght in 1984. Maeght displayed the car at the Musée de l’Automobile à Mougins until the museum closed in early 2009. At that time, Guidobaldi’s car was purchased by David Humbert, who ordered a total restoration. Luc Franza completed the restoration to running order in 2010, and the restored “Guidomobile” debuted at the 8th Avignon Motor Festival in March. The car was then displayed at the Monaco Motor Show in June 2010 and in March 2014 at the

Concours d’Elegance du Monaco, where it won first prize in the technology category. Starting in September 2014, the car was displayed at the Cité de l’Automobile – Musée National, Collection Schlumpf in Mulhouse, France. In late 2019, and still in perfect condition, the “Guidomobile” was offered for sale. The vehicle serves as a lasting tribute to all engineers who chase their dreams.

Guidobaldi-rear

Rear view of the “Guidomobile” shows the car with a slight lean into a right turn. Note the different angles of the left and right rear suspension arms. Just visible at the top of the car is the rubber damper system for the rear suspension. (Cyril de Plater image)

Sources:
– “Un mécanicien d’Antibes a réalisé cette monoplace de 180 Ch (Formule 1)” Supplement à l’Automobile N°107 (March 1955)
– “La voiture révolutionnaire de F, Guidobaldi” by Sven-Ake Nielsen, l’Automobile N°157 (March 1959)
– “The Leaning Car” by Sven-Ake Nielsen, Sportscar Graphic (April 1960)
– “Un rêve d’inventeur” by Dominique Pascal, Auto Passion N°6 (September 2006)
– “Un chef d’oeuvre ressuscité” by Philippe Loisel, La vie de l’Auto N°1424 (16 September 2010)
– “Road Vehicle Tilting Inwardly in Curves” US patent 2,791,440 by Francois Guidobaldi (granted 7 May 1957)
http://s512186177.onlinehome.fr/
https://www.hemmings.com/classifieds/cars-for-sale/classic/unspecified/2451178.html
https://drivetribe.com/p/swaying-superstar-1956-guidobaldi-Ye7EN33pQFuOvZInPejodQ?iid=Kft1piUOT7OEPjWpIiuEHA

Curtiss-XP-23-rear-left

Curtiss XP-23 / YP-23 Hawk Biplane Fighter

By William Pearce

On 8 July 1931, the United States Army Air Corps (AAC) issued production contract W535-ac-4434 to the Curtiss-Wright Corporation for the production of 46 P-6E Hawk fighter aircraft. The P-6E was one of many variants that had branched from the P-6 line, which originated in 1928. The basic P-6 was a refined P-1 equipped with a Curtiss V-1570 Conqueror engine; however, the 46th aircraft from contract W535-ac-4434 would not be finished as a P-6E. Rather, it would become the Model 63, which carried the AAC designation XP-23. In the early 1930s, the AAC was interested in exploring advancements with turbosuperchargers to create a fighter capable of high speeds at high altitudes, and the XP-23 was an opportunity to create just such an aircraft.

Curtiss-XP-23-front-left

The Curtiss XP-23 Hawk with an unidentified individual (contact us if you can ID). Visible is the large turbosupercharger, its intake, and the two exhaust pipes feeding the turbine. Note the engine coolant radiator between the main gear.

The Curtiss XP-23 was a single engine biplane with conventional fixed taildragger undercarriage. The only components the aircraft had in common with a P-6E were the wings, although some sources state that the wings had a spar and rib frame built of metal rather than wood. Whether it was made of wood or metal, the wing’s frame was covered in fabric. The upper wing had a 1.5-degree dihedral, was mounted 4 in (102 mm) higher than on the P-6E, and was positioned 28.5 in (724 mm) forward of the lower wing. The lower wing had no dihedral and was 5 ft 6 in (1.68 m) shorter in span. Ailerons were located on the upper wing only.

The aircraft’s monocoque fuselage and tail were of all-metal construction. The main and reserve fuel tanks were housed forward of the cockpit and held a total of 78 US gallons (65 Imp gal / 295 L). The oil tank held 11 US gallons (9 Imp gal / 42 L). A .30-cal machine gun was mounted on each side of the aircraft just forward of the cockpit. A long blast tube extended from each gun, through the engine bay under the exhaust, and exited just behind the spinner. Some sources indicate the armament was one .30-cal and one .50-cal machine gun, while other sources state two .30-cal and one .50-cal machine gun. It is not clear where the third gun would have been located, if indeed there was one. Aerodynamic fairings covered the main wheels except for their outer side.

Curtiss-XP-23-left

Side view of the XP-23 illustrated the aircraft’s rather smooth, all-metal finish. Note the machine gun port just under the engine’s exhaust and the left-handed (counterclockwise) propeller. The image was dated 12 April 1932, four days before the aircraft was accepted by the AAC.

The XP-23 was powered by a liquid-cooled Curtiss V-1570 Conqueror V-12 engine, which was equipped with a General Electric F-2C turbosupercharger. The turbosupercharger was externally mounted to the left side of the engine. Exhaust from the left cylinder bank was fed directly into the turbosupercharger, and exhaust from the right cylinder bank was ducted through the cowling just behind the engine and to the turbosupercharger. The intake was just forward of the turbosupercharger. The engine did not have a mechanically-driven supercharger or blower.

The turbosupercharger enabled the V-1570 engine to produced 600 hp (447 kW) at 2,400 rpm from sea level to 15,000 ft (4,572 m). The V-1570 had a 6.1 to 1 compression ratio and consumed 60 US gph (50 Imp gph / 227 L/h) at full throttle and 36 US gph (30 Imp gph / 136 L/h) at 2,100 rpm (cruise power / 88% throttle). At a .500 reduction, the engine turned a metal, three-blade, ground-adjustable Hamilton Standard propeller that was 9 ft 6 in (2.90 m) in diameter. Mounted under the engine and between the main gear was the radiator for the engine’s ethylene glycol cooling system.

Curtiss-XP-23-rear-left

The drag-inducing installation of the side mounted turbosupercharger is illustrated in this rear view of the XP-23. Note the reduced span of the lower wing.

The XP-23’s upper wing had a span of 31 ft 6 in (9.60 m), and its lower wing had a span of 26 ft (7.92 m). The aircraft had a length of 23 ft 9 in (7.24 m) and a height of 8 ft 9 in (2.67 m). The XP-23’s top speed was 223 mph (359 km/h) at 15,000 ft (4,572 m) and 178 mph (286 km/h) at sea level. The aircraft’s cruising speed was 192 mph (309 km/h) at 15,000 ft (4,572 m), and its stalling speed was 69 mph (111 km/h) at sea level. The XP-23 had an initial climb rate of 1,370 fpm (6.96 m/s), and its service ceiling was 32,000 ft (9,754 m). The aircraft’s range was 292 miles (470 km) at full throttle and 435 miles (700 km) at cruise power. The XP-23 had an empty weight of 3,142 lb (1,425 kg) and a gross weight of 4,032 lb (1,829 kg).

The XP-23 was allotted serial number 32-278 and built at the Curtiss Airplane Division Plant 1 on Kenmore Avenue in Buffalo, New York. The aircraft was accepted by the AAC on 16 April 1932 at a cost of $12,279.36. Although the XP-23’s performance met expectations, there is some indication that the turbosupercharger overheated and was unreliable. Regardless, the age of biplane fighters was at an end, and the XP-23 was the last biplane fighter accepted by the AAC. The Boeing P-26 Peashooter prototype was the AAC’s first monoplane fighter to enter service and made its first flight on 20 March 1932. The P-26 out-performed the XP-23 and showed that the monoplane type was the future.

Curtiss-YP-23-front-left-radiator

The YP-23 with the turbosupercharger removed and a two-blade propeller installed. It also appears that either a support was installed between the main wheels or that a fairing was installed over the existing brace wires.

Curtiss had proposed powering the XP-23 with a V-1800 Super Conqueror engine. The V-1800 had a mechanically-driven supercharger that eliminated the bulbous side-mounted turbosupercharger previously used on the XP-23 and resulted in a much cleaner cowling. The engine produced 800 hp (597 kW) at 2,400 rpm and turned a 10 ft (3.05 m) diameter, metal, three-blade, ground-adjustable Hamilton Standard propeller at a .714 reduction. With the V-1800, the XP-23 had an anticipated top speed of 234 mph (377 km/h) at 12,000 ft (3,658 m) and a cruise speed of 199 mph (320 km/h). At 23 ft 11 in (7.29 m) long and 3,227 lb (1,464 kg) empty, the aircraft was 2 in (51 mm) longer and 85 lb (39 kg) heavier than the V-1570-powered variant. Curtiss did note that the wing might need to be moved forward slightly to achieve a proper center of gravity. However, the V-1800 was never installed in the XP-23.

The sole XP-23 was modified by removing the turbosupercharger, but the V-1570 was retained. It is not clear if the modifications were in anticipation of further changes to incorporate the V-1800, or if it was done to compare the turbosupercharger setup to the normally-aspirated V-1570. With the turbosupercharger removed, the aircraft became commonly known as the YP-23. The engine’s air intake was positioned atop the cowling, a two-blade propeller was fitted, and its armament was removed. In this configuration, the YP-23 achieved 200 mph (322 km/h) at 15,000 ft (4,572 m).

Curtiss-YP-23-left-radiator

A new cowling was made for the YP-23 that did not incorporate gun ports below the engine’s exhaust stacks. Note the intake atop the cowling and the Wright “Arrowhead” painted on the fuselage. The aircraft as pictured is similar in appearance to the proposed V-1800-powered XP-23.

The YP-23 underwent one last round of modifications to explore the effects of radiator drag on high-speed aircraft. The coolant radiator was removed, the V-1570 engine was switched to a total-loss water cooling system, and the aircraft’s main fuel tank was used as a water reservoir. Using fuel from the reserve tank, cooling water flowed through the engine at a reduced rate from the main tank and was then vented overboard. The previous deletion of the turbosupercharger and the removal of the radiator gave the YP-23 an exceptionally clean appearance. Unfortunately, test results of these modifications have not been found. It is possible that thorough testing was never conducted since monoplanes offered higher performance. The YP-23 was disassembled, and its wings were reportedly used on the XF11C-1 Goshawk prototype fighter for the United States Navy.

Curtiss-YP-23-left-no-radiator

The YP-23 in its final form with the radiator removed and serving as the AAC’s last biplane fighter design. While the aircraft exhibits an exceptionally clean appearance, its flight endurance was very short with its total-loss cooling system.

Sources:
Curtiss Fighter Aircraft by Francis H. Dean and Dan Hagedorn (2007)
Curtiss Aircraft 1907–1947 by Peter M. Bowers (1987)
U.S. Fighters 1925 to 1980s by Lloyd S. Jones (1975)
American Combat Planes of the 20th Century by Ray Wagner (2004)
http://www.joebaugher.com/usaf_fighters/p23.html