LFG Roland D.XIV
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The Luft-Fahrzeug-Gesellschaft (LFG) Roland D.VII was a German single seat, single engine
biplane A biplane is a fixed-wing aircraft with two main wings stacked one above the other. The first powered, controlled aeroplane to fly, the Wright Flyer, used a biplane wing arrangement, as did many aircraft in the early years of aviation. While ...
fighter aircraft Fighter aircraft are fixed-wing military aircraft designed primarily for air-to-air combat. In military conflict, the role of fighter aircraft is to establish air superiority of the battlespace. Domination of the airspace above a battlefield ...
built during
World War I World War I (28 July 1914 11 November 1918), often abbreviated as WWI, was one of the deadliest global conflicts in history. Belligerents included much of Europe, the Russian Empire, the United States, and the Ottoman Empire, with fightin ...
. Problems with its underdeveloped
V-8 engine A V8 engine is an eight-cylinder (engine), cylinder piston engine in which two banks of four cylinders share a common crankshaft and are arranged in a V engine, V configuration. The first V8 engine was produced by the French Antoinette_(manuf ...
prevented its production.


Design and development

The D.VII was a response by LFG to continued criticism of the pilot's limited forward and downward view from its fighters. The D.V and D.VI had attempted to address this problem though not very successfully. Since the height of the
Mercedes D.III The Mercedes D.III, or F1466 as it was known internally, was a six-cylinder SOHC valvetrain liquid-cooled inline aircraft engine built by Daimler and used on a wide variety of German aircraft during World War I. The initial versions were introd ...
and Benz Bz.IIIa inline engines used in these two designs were part of the problem, LFG decided to install the new 60° V-8
Benz Bz.III The Benz Bz.III was a six-cylinder, water-cooled, inline engine developed in Germany for use in aircraft in 1914. Developing 112 kW (150 hp) at 1,400 rpm from 14.3 L (875 cu in),Smith 1981, p.53. it powered many German military aircraft ...
b, lowering the cylinders and providing a gap between them. Apart from its engine, the D.VII had much in common with the D.VI, particularly with the original D.VIa variant. It was a single bay biplane with pairs of near-parallel
interplane strut In aeronautics, bracing comprises additional structural members which stiffen the functional airframe to give it rigidity and strength under load. Bracing may be applied both internally and externally, and may take the form of strut, which act in ...
s and blunt-tipped wings of almost constant chord, though less staggered than on the D.VI. The upper wing was carried above the fuselage by a cabane; only this wing-mounted
aileron An aileron (French for "little wing" or "fin") is a hinged flight control surface usually forming part of the trailing edge of each wing of a fixed-wing aircraft. Ailerons are used in pairs to control the aircraft in roll (or movement around ...
s. A small cut-out in its
trailing edge The trailing edge of an aerodynamic surface such as a wing is its rear edge, where the airflow separated by the leading edge meets.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', page 521. Aviation Supplies & Academics, 1997. ...
above the cockpit enhanced the pilot's view. The vertical tail was rounded, with a deep, wide chord
rudder A rudder is a primary control surface used to steer a ship, boat, submarine, hovercraft, aircraft, or other vehicle that moves through a fluid medium (generally aircraft, air or watercraft, water). On an aircraft the rudder is used primarily to ...
that extended below the fuselage to meet a small
ventral Standard anatomical terms of location are used to unambiguously describe the anatomy of animals, including humans. The terms, typically derived from Latin or Greek language, Greek roots, describe something in its standard anatomical position. Th ...
fin A fin is a thin component or appendage attached to a larger body or structure. Fins typically function as foils that produce lift or thrust, or provide the ability to steer or stabilize motion while traveling in water, air, or other fluids. Fin ...
. Both types had ''Klinkerrumpf'',
clinker built Clinker built (also known as lapstrake) is a method of boat building where the edges of hull planks overlap each other. Where necessary in larger craft, shorter planks can be joined end to end, creating a longer strake or hull plank. The techniq ...
fuselage The fuselage (; from the French ''fuselé'' "spindle-shaped") is an aircraft's main body section. It holds crew, passengers, or cargo. In single-engine aircraft, it will usually contain an engine as well, although in some amphibious aircraft t ...
s,
monocoque Monocoque ( ), also called structural skin, is a structural system in which loads are supported by an object's external skin, in a manner similar to an egg shell. The word ''monocoque'' is a French term for "single shell". First used for boats, ...
s constructed with thin overlapping spruce strips over a light wooden internal framework and oval in cross-section. The engine was totally enclosed in the nose, driving a two-blade
propeller A propeller (colloquially often called a screw if on a ship or an airscrew if on an aircraft) is a device with a rotating hub and radiating blades that are set at a pitch to form a helical spiral which, when rotated, exerts linear thrust upon ...
. The D.VII's
conventional undercarriage Conventional landing gear, or tailwheel-type landing gear, is an aircraft undercarriage consisting of two main wheels forward of the center of gravity and a small wheel or skid to support the tail.Crane, Dale: ''Dictionary of Aeronautical Term ...
had mainwheels on a single axle, supported by long V-struts to the lower fuselage and a tail skid on the
leading edge The leading edge of an airfoil surface such as a wing is its foremost edge and is therefore the part which first meets the oncoming air.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', page 305. Aviation Supplies & Academics, ...
of the ventral fin. Pilots agreed that the revised forward profile changed the view from poor on the D.VI to excellent on the D.VII. During development, the D.VII acquired some of the features of the D.VIb, most noticeably overhung, balanced ailerons. The empennage was also modified to a form close to that of the D.VIb, with a small, lower, and broader
fin A fin is a thin component or appendage attached to a larger body or structure. Fins typically function as foils that produce lift or thrust, or provide the ability to steer or stabilize motion while traveling in water, air, or other fluids. Fin ...
and broad chord
balanced rudder Balanced rudders are used by both ships and aircraft. Both may indicate a portion of the rudder surface ahead of the hinge, placed to lower the control loads needed to turn the rudder. For aircraft the method can also be applied to elevators and ...
. The tailplane was lowered from the top of the fuselage to its midpoint. Development of the D.VII was interrupted by problems with the Benz engine, itself still under development. Nonetheless, the D.VII took part in the second D. competition (for fighter types) held in May 1918. In the end, the recurrent engine problems led to development being abandoned. LFG fitted a second aircraft with a geared version of the Benz engine, a
Benz Bz.IIIb The Benz Bz.IIIb was an eight-cylinder, water cooling, water-cooled, V-engine developed in Germany for use in aircraft in 1918 in aviation, 1918. Design and development Inspired by the Hispano-Suiza 8, some of which were captured and tested, the ...
m, redesignating it as the LFG Roland D.VIII; this also attended the second D. competition. Its report marked it unfit for series production; the reasons are not recorded, but it is known this geared engine, again in early development, suffered from severe vibration.


Variants

;D.VII: direct drive, Benz Bz.IIIbo. One built. ;D.VIII: geared drive, Benz Bz.IIIbm. One built. ;D.XIII: D.VII based but with a Körting Kg.III water-cooled
V-8 engine A V8 engine is an eight-cylinder (engine), cylinder piston engine in which two banks of four cylinders share a common crankshaft and are arranged in a V engine, V configuration. The first V8 engine was produced by the French Antoinette_(manuf ...
. The sole example was first flown in May 1918. Flight tests proved the engine unsatisfactory and it was returned to Körting for modification, with the intention of refitting it. However, the engineless D.XIII was destroyed in a hangar fire that July. One built. ;D.XIV: As D.XIII, but with a Goebel Goe.III 11-cylinder
rotary engine The rotary engine is an early type of internal combustion engine, usually designed with an odd number of cylinders per row in a radial configuration. The engine's crankshaft remained stationary in operation, while the entire crankcase and i ...
. It took part in the second D competition of May 1918 but its unreliable engine denied it production status. One built.


Specifications (D.VII)


References


Bibliography

* {{Idflieg D-class designations Biplanes 1910s German fighter aircraft
LFG Roland D.VII The Luft-Fahrzeug-Gesellschaft (LFG) Roland D.VII was a German single seat, single engine biplane fighter aircraft built during World War I. Problems with its underdeveloped V-8 engine prevented its production. Design and development The D.VII ...
Aircraft first flown in 1918