Carden-Baynes Bee

The Carden Baynes Air¬craft Company Ltd built the twin pusher, side by side two-seater, designed by L.E. Baynes, at Heston, Middlesex, UK. It was fitted with two totally-enclosed pusher Carden Ford S.P.1 modified car engines.

Of all wooden construction, the wings pivoted about the centre-line of the aircraft, the aft fuselage top decking folded down to enable the wings to pass over the top.

The undercarriage had twin mainwheels of fixed centre, mounted inside the fuselage, and a tail skid.

Only one Bee was built, c/n 1 G-AEWC. First flown on 3 April 1937, at Heston.

It was broken up and scrapped in 1939.

Engines: 2 x Carden Ford S.P.1, 10 hp
Wingspan: 9.09 m / 29 ft 10 in
Wing area: 13.10 sq.m / 141 sq.ft
Length: 7.01 m / 23 ft 0 in
Empty weight: 400 kg / 880 lb
AUW: 612.35 kg / 1350 lb
Wing loading: 46.62 kg/sq.m / 9.55 lb/sq.ft
Max speed: 177 kph / 110 mph
Cruise: 161 kph / 100 mph
Stall: 64 kph / 40 mph
ROC: 213 m/min / 700 fpm
Endurance: 3 hr

Carden-Baynes Aircraft Co Ltd

Sir John Carden was associated with British light aviation after designing the 750 cc ultralight engine for the Gloucestershire Gannet in the early 1920s. Went into partnership with L. E. Baynes in 1930 to produce a one-off single-seat powered glider.

Baynes and Carden then planned a two-seat twin-enged light aircraft and decided to set up a new company to produce this aircraft which was known as the Bee. In spite of the death of Carden in an air crash near Croyden, the new company Carden-Baynes Aircraft Ltd was formed in 1936 at Heston Airport, Middlesex. However, three successive partners, including the Duke of Grafton, also died one after the other but the Bee eventually flew at Heston on 3 April 1937 as a small two- seat high-wing monoplane with two Carden Ford S.P.1 modified car engines.

Development of three-seat B-3 halted by war.

Financial difficulties followed. An agreement was eventually reached with Major Shaw for a development of the Bee to be manufactured by Slingsby Sailplanes Ltd.

Caquot Balloon

Caquot Type R

At the start of World War I observation balloons, the use of which was discontinued in France in 1912, were needed on the battlefield, and the Germans used them in large quantities called Drachen. The French who did not have any in their boxes therefore began to copy these German balloons.

While he was mobilized on 1st August 1914 to command the 21th company of balloonists, Albert Caquot performed some aerial observations in a spherical ball type from 1880, then found that the information given by the observers are not reliable due to the instability of the aerostats which makes them sick even in light winds. He then designed a new balloon stabilized by three inflatable rear lobes arranged at 120°. He then sent his plans and calculations to the Atelier de Chalais-Meudon in October 1914 and was received by the director of the establishment in November; but he is not convinced by his idea. Despite everything, he decides to entrust the realization of Caquot’s plans to a team of designers from his design office, they are carried out in a week. In the meantime General Hirschauer, who is in charge of aviation at the Ministry of War, orders that a test be carried out. Caquot then obtained authorization to build a prototype, which was done in February 1915.

The Caquot type L balloon is then compared to a spherical balloon and a copy of Drachen. It immediately proves to be more efficient, its hull offering minimum resistance to the wind. It managed to withstand winds of 90 km / h against only 54 km / h and 36 km / h for the Drachen and the spherical balloon. Its performance is due to the ovoid shape of the balloon which allows less aerodynamic resistance, and above all to its three inflatable tail units at the rear but based on an internal structure fixing them rigidly to the hull at an angle of 120°. This makes it possible to avoid the pendulum movement of the balloon during gusts of wind, which made observers sick.

Despite these conclusive tests, series production is not launched. However, an English naval officer, who attended the prototype tests, told Caquot that the British navy was trying to equip its fleet with captive balloons, but that they could not withstand bad weather. He then asks her to help them. By examining the constraints, Caquot realizes that the aerostats must resist winds of 125 km / h since in addition to the wind is added the speed of the ship. He then designed a specific braked winch that allowed the balloon to be carried away by too strong gusts and then return once the gust was over.

A French Caquot type observation balloon in 1915.

This ability proved itself in an account of a “free balloon” flight taken by Capt. F. H. Cleaver, commanding officer of the RFC’s No. 1 Kite Balloon Section on October 27, 1915:

The speed and direction of the wind was tested and found to be 15 m.p.h. by the air meter. The balloon was then let up and marched for 300 yards to the winch; it was easily controlled by the balloon party. The winch was shackled on and I and Lieut. Beaufort ascended; the wind appeared to be increasing, the speed was again taken from the balloon and found to be 30 m.p.h. The guy of the right sail carried away, which caused the balloon to oscillate considerably, thus increasing the strain on the cable and rigging. On this an order was immediately given to haul down. The winch, whose power is only 6 horse failed; the wind was rapidly increasing in strength and on again being tested the speed was found to be 40 m.p.h. Fortunately for the occupants of the balloon the cable then parted, had it not done so the rigging most certainly would have gone. The valve rope was immediately pulled and as soon as the end of the cable or any part of it touched the ground, the balloon in spite of the loss of gas naturally was lightened owing to being relieved of the weight of a portion of the cable, and ceased to descend and at times rose; this coupled with the heat of the sun causing the gas to expand and the balloon to become still lighter, was responsible for what might appear to be a long flight, which owing to the speed of the wind was carried out at 40 m.p.h. A perfect landing was effected in 45 minutes without any damage to the balloon, occupants and instruments.

These qualities quickly proved the Caquot to be the best balloon design on the Western Front and all the combatant nations eventually adopted it.

In June 1915, Albert Caquot became director of the mechanical aerostation workshop at Chalais-Meudon, where he had new aerostats built in large series according to his plans. On July 10, 1916, the British Aviation Inspector requested M type balloons from the War Department. Between July and the end of November 1916, 46 M type balloons were built in Chalais-Meudon for the British, subsequently ‘others are built in the UK. Three types of balloons with a capacity of 750 cu.m, 820 cu.m and 1000 cu.m. The first equip small ships used for the research of submarines, they are served by two men from an altitude of 500 m; the larger ones are used aboard squadron ships for the adjustment of fire and are served by a crew of three observers at 500 m altitude or two at 1000 m. This use of Caquot balloons allows the British Navy to reduce its losses. In 1917, the French navy, noting that its losses due to torpedoing were becoming higher than those of the British, then decided to adopt the Caquot balloons as well. The French Navy uses types P and P2 on its smaller units for protection against U-boat attacks, and the Type R to direct the fire of its larger ships. In July 1918, it had nearly 200 balloons and 24 units designed to work with them.

The French Army, for its part, trained 76 units during the war equipped with Caquot balloons. These balloons are used for artillery tuning and general observation of the battlefield.

In 1917, when the Germans began to bombard Paris with aircraft, Albert Caquot proposed to make barrages with low volume balloons, the cables of which would force the bombers to climb higher and reduce their load. This idea is taken up by the British in September 1917. At the end of the war, there are Caquot type of balloons, mainly with M 900 cu.m and R 1000 cu.m.

The Caquot balloon entered service in other Allied armies and then in others including the new Polish army.

In France, the production of balloons was 319 units per month in 1919. The first models are of type L and M, and finally the Caquot balloons are produced in four different formats:

P – 750 m³ (capacity – two observers at the height of 500 m)
P2 – 820 m³
M2 – 930 m³
R – 1000 m³ (capacity – two observers at the height of 1000 m or three at 500 m)

During the war, one of the British Caquot balloons fell into the hands of the Germans who made a copy called Ae 800 for Achthundert english 800 which was a reference to the cubic meter capacity.

Type Ae

General Ernst von Hoeppner, commander of the German Luftstreitkräfte freely admitted that German balloons put in service after 1916 were patterned after a captured British example. Caquots and their German copies eventually served on all fronts and with naval forces operating in the Atlantic and Mediterranean. The improved Caquot could ride higher, and fly in higher winds than the Parseval-Sigsfeld, so it quickly replaced the Drachen, even among the Luftschiffertruppen.

During the war, France was from 1915 the leading power in the field of ballooning and built nearly 4,200 captive balloons: 1,700 observation balloons and 2,500 barrage balloons.

The Caquot balloon was manufactured in large numbers, including a thousand in the United States between 1918 and 1919.

Caquot Type R at the National Museum of the United States Air Force

The United Kingdom built others during World War II where they were used until the 1960s to test parachutes, for non-combat aerial observation and photography.

A type R Caquot on the Arcadia Balloon School of the United States Army Air Service in the city of Arcadia (California) in 1921.

Gallery

P
Capacity: 50 m³
Payload: two observers
Altitude: 500 m

P2
Capacity: 820 m³

M2
Capacity: 930 m³

R
Capacity: 1000 m³ / 32,200 cu.ft
Payload: two observers to 1000 m / three observers to 500 m
Length: 92 ft
Diameter: 32 ft
Cruising speed: 75 km / h
Max wind speed: 70 mph

Caquot, Albert

Albert Caquot, in a dark jacket in the foreground (the 2 nd from the right), in the premises of the École Polytechnique

Albert Irénée Caquot, born on 1st July 1881 in Vouziers (Ardennes) and died on November 28, 1976 in Paris at 95, was considered “the greatest of living French engineers” for half a century.

Albert Caquot Article

Large landowners, his parents, Paul Auguste Ondrine Caquot and Marie Irma Cousinard 2 , wife Caquot, “run a large family farm, adjoining a mill on the banks of the Aisne”, in Vouziers in the Ardennes. His father opened this farm to modernism, installing electricity and telephones in his home in 1890.

Just one year after leaving the high school Reims, eighteen years, Albert Caquot received 29 e the entrance exam to the Ecole Polytechnique (class of 1899) which he graduated ranked 15th, and enters the body of bridges and roads.

From 1905 to 1912, he was a bridge and road engineer in Aube, in Troyes, and stood out for the important sanitation measures he developed. These saved many human lives and protected the city from the great flooding of the Seine in 1910.

In 1912, he joined the reinforced concrete design office of Armand Consideration as a partner, where he gave free rein to his talent as a designer of civil engineering structures. In 1914, after the death of Armand Considere, the office became “Pelnard-Considerere & Caquot”. It was in this same context that he worked from 1919 to 1928, from 1934 to 1938, then from 1940.

During his life, Albert Caquot taught for a long time the resistance of materials at the Ecole Nationale Superieure des Mines in Paris, the Ecole Nationale des Bridges et Chaussées and the Ecole Nationale Supérieure de l’Aéronautique.

During his career he produced more than three hundred civil engineering works of all kinds, several of which were then world records.

Two achievements contribute to its international reputation:

The internal reinforced concrete structure of the large statue of Christ the Redeemer on Mount Corcovado (1931, height 30 m and weight 1,145 t), in Rio de Janeiro, the work of French sculptor Paul Landowski and, for the head of Christ, by Romanian sculptor Gheorghe Leonida.

The George V Bridge in Glasgow (Scotland) on the Clyde for which Scottish engineers are asking for help.

The Christ of Corcovado whose internal structure is due to Caquot.

He devoted his life to aeronautics and civil engineering in alternating periods at the pace imposed by the First and Second World Wars. Albert Caquot’s contributions to aeronautics are invaluable, from the development of the propeller engine and the opening up of the Air Ministry to technical innovations, to the founding of the first institutes of fluid mechanics. Marcel Dassault, who was commissioned by Albert Caquot to build a prototype of the postal three-engine program, wrote of him: “He is one of the best technicians that aviation has ever known. He was a visionary who, in all areas, looked to the future. He was ahead of everyone.”

From 1901 he carried out his military service in a battalion of balloonists. At the start of the Great War, he found a battalion of balloonists from Toul as captain. For a wind speed greater than 22 km/h, it highlights the great instability of the spherical balloon with which the units are equipped. In 1915, he produced a tapered tethered balloon model equipped with rear stabilizers on the Drachen principle developed by the German August von Parseval, allowing observation by winds of 90 km/h. The Chalais-Meudon aerostatic workshop then began to manufacture “Caquot balloons” for all the Allied armies. The winch with constant braking torque that it creates allows it to adapt its balloons to the Allied fleets (fire control and detection of submarines) and to make them withstand winds of up to 125 km/h. Also called a “sausage”, this captive balloon gives France and its Allies a major strategic advantage. In January 1918, Clemenceau appointed him technical director of military aviation.

A French Caquot type observation balloon in 1915.

In 1919, Albert Caquot was behind the creation of the French Air Museum, today the Air and Space Museum at Le Bourget. It is the oldest aeronautical museum in the world.

In 1935, he built a double canopy hangar 120 m long, 60 m wide by 9 m free height and its annexes for around 10,000 m2 at Fréjus on the naval air base.

In 1928, he became the technical director general of the newly created Air Ministry. It practices a policy of research, prototypes and mass production which gives France back the industry it deserves.

In 1934 he preferred to retire and devote himself again to civil engineering. In 1938, under the threat of war, Albert Caquot was recalled to assume the joint presidency of all the national aeronautical companies. In July 1939, he also took over the role of technical director general of the Air Ministry but, although he had spectacularly turned around the production of aircraft, the obstacles he encountered on the part of the staff and the management of the control led him to submit his resignation in 1940.

Numerous honorary distinctions from all countries that have been awarded to him, including the dignity of Grand Cross of the Legion of Honour in 1951.

He chaired many French scientific organizations for more than twenty years, such as the National Council of French Engineers and the Société d’Enouragement pour l’Industrie Nationale. He was also a director of Electricité de France for more than ten years.

He served 41 years in the Academy of Sciences and was its president in 1952.

In 1961, at the age of eighty, Albert Caquot voluntarily resigned from all the presidencies that he had always provided on a voluntary basis.

His name was given to an amphitheatre of the School of Bridges and Roads located in no 28 of the rue des Saints-Peres in Paris May 25, 1977. The new occupant of the premises, the Institut d’études politiques de Paris, renamed it in honour of Simone Veil on March 8, 2018.

The July 2, 2001, a stamp of CHF 4.50 and 0.69 € is issued for the 120th anniversary of the birth and the 25th anniversary of the death of Albert Caquot. Designed and engraved by Claude Andréotto, the stamp is printed in intaglio on sheets of forty and is distributed in 4.37 million copies.

Since 1989, the Albert-Caquot Prize has been awarded each year by the French Association of Civil Engineering (AFGC) to an engineer.

The 7th promotion of the National School of Engineers Military Infrastructure (ENSIM) was christened Albert Caquot to honour his contribution to the military works.

Distinctions:

Distinguished Service Order
Officer of the Order of the Crown of Italy
Commander of the Order of Leopold
Grand Officer of the Order of the Crown of Romania
Order of the White Eagle
Order of the Rising Sun
Order of Saint Michael and Saint -Georges
Croix de guerre 1914-1918
Distinguished Service Medal
Honorary fellow American Institute of Aeronautics and Astronautics (1937)
Grand Cross of the Legion of Honour (1951)
Wilhelm Exner Medal (1962)

Caproni Ca.311 / Ca.312 / SABCA S.48

The Ca 311 differed from its predecessor in having the “stepped” windscreen replaced by a more extensively glazed Blenheim I-style dose section (although the second production series, the Ca 311M (Modificato) reverted to a stepped canopy rather like that later adopted for the Ca 314), and the Ca 312 was a version with 630-h.p. Piaggio P.XVI R.C.35 radials.

Caproni Ca.311M

Defensive armament was a Caproni Lanciani turret with a single 7.7mm machine-gun, and one machine-gun in the port wing root and another firing aft through a ventral hatch.

Caproni Ca.311

The Ca 312M possessed a similar nose to that of the Ca 311, the Ca 312bis was a twin-float seaplane variant, and the Ca 312-1S was an experimental torpedo floatplane. The Ca 313 was a further development of the Ca 311 with two 650-h.p. Isotta-Fraschini Delta R.C.35 engines which was used in limited numbers on the Russian Front.

(SABCA) made a marketing agreement with the Italian company Caproni, with SABCA selling some of Caproni’s military aircraft in certain markets, including the Caproni Ca.135, Ca.310 and the Ca.312, which were to be designated SABCA S.45bis, S.46 and S.48 respectively.

Ca.311
Engines: 2 x Piaggio P.VIII C.35, 470 hp

Caproni Ca.310 / SABCA S.46

Developed in parallel with the Ca.309 Ghibli, the Ca.310 Libeccio (south west wind) reconnaissance / transport aircraft was structurally similar, but had retractable landing gear and was powered by two 460hp/350kW Piaggio P.VII C.35 radial engines.
Export deliveries went to Norway, Peru and Yugoslavia. Yugoslavia also acquired 12 more under the designation Ca.310bis; this variant differed primarily by having an unstepped extensively glazed nose.
The Caproni C.310 World War 2 to be retired by the Italians in 1948.
The prototype of the Ca.310bis served as a development aircraft for the following Ca.311.

(SABCA) made a marketing agreement with the Italian company Caproni, with SABCA selling some of Caproni’s military aircraft in certain markets, including the Caproni Ca.135, Ca.310 and the Ca.312, which were to be designated SABCA S.45bis, S.46 and S.48 respectively.

Caproni Ca.310 (Libeccio)
Engines: 2 x Piaggio P.VIII C.35, 470 hp
Length: 40.03ft (12.2m)
Width: 53.15ft (16.20m)
Height: 11.55ft (3.52m)
Maximum Speed: 227mph (365kmh; 197kts)
Maximum Range: 1,050miles (1,690km)
Service Ceiling: 22,966ft (7,000m; 4.3miles)
Armament:
1 x 7.7mm Breda SAFAT machine gun in dorsal turret.
2 x 7.7mm Breda SAFAT machine guns in fixed-firing forward wingroot locations.
Up to 992lbs of internal ordnance.
Accommodation: 3
Hardpoints: 0
Empty Weight: 6,724lbs (3,050kg)
Maximum Take-Off Weight: 10,251lbs (4,650kg)

Caproni Ca.306 Borea / Ca.309      

Caproni Ca.309 Series V Ghibli

The prototype of the six-passenger low-wing transport Caproni Bergamaschi Ca.306 Borea (north wind) appeared at the 1935 Milan Exhibition. The Borea was first of a range of light twin-engine aircraft manufactured for a variety of roles.

The first of these was the mixed wood and metal construction Ca.309 Ghibli (desert wind) of 1936, 78 of which were built for use in Libya. The military versions were used as light transports or reconnaissance bombers with a lengthened glazed nose, bomb racks, cameras, and with armament comprising three 7.7mm machine-guns. Powered by two Alfa Romeo 115 in-line engines, of 185hp each and having a fixed, spatted undercarriage, the Ghibli had a maximum speed of about 150mph.

Caproni Ca.309 Ghibli

Seven squadrons equipped with Ghiblis were operational when Italy entered the war in 1940. The Ghibli was used for police duties by the Aviazione Presidio Coloniale and the Aviozione Sahariana as a light reconnaissance-bomber and transport (carrying two crew members and six passengers).

Several production series were produced, the final versions of the Ghibli to Ibe produced in quantity being the Series V and VI, the latter having a forward-firing 20-mm. cannon mounted in the nose.

Caproni Bergamaschi Ca 309 Ghibli
Engine: 2 x 200hp Alfa Romeo 115-II
Max take-off weight: 2695 kg / 5941 lb
Empty weight: 1745 kg / 3847 lb
Wing load: 14.35 lb/sq.ft / 70.00 kg/sq.m
Wingspan: 16.20 m / 53 ft 2 in
Length: 13.30 m / 43 ft 8 in
Height: 3.25 m / 10 ft 8 in
Wing area: 38.70 sq.m / 416.56 sq ft
Max. speed: 250 km/h / 155 mph
Cruise speed: 210 km/h / 130 mph
Service ceiling: 14764 ft / 4500 m
Range: 670 km / 416 miles
Armament: 3x MG 7,7mm, 335kg Bomb.
Undercarriage: fixed.

Caproni Ca.164

The Caproni Ca.164 was produced by Aeronautic Pedappio S.A., a division of the Caproni Group in 1937.

Powered by a 185 hp Alfa 115-1 engine, the Ca,164 was employed by the Regia Aeronautica during the war years.

Engine: 185 hp Alfa 115-1
Wingspan: 30 ft 10 in
Length: 22 ft 10 in
Height: 8 ft 6 in
Empty weight: 1873 lb
Loaded weight: 2600 lb
Max speed: 13 mph
Cruising speed: 115 mph
Range: 330 mi
Seats: 2