Linke-Hofmann R.I
| Linke-Hofmann R.I | |
|---|---|
 |
|
| The second Linke-Hofmann R.I, 40/16 | |
| Role | Heavy bomber |
| National origin |
 German Empire
|
| Manufacturer | Linke-Hofmann |
| Designer | Paul Stumpf |
| First flight | spring 1917 |
| Number built | 4 |
The Linke-Hofmann R.I was a heavy bomber aircraft designed and built by the German company Linke-Hofmann during World War 1. Only four were built and the type never saw service with the Luftstreitkräfte (Imperial German Air Service).
Linke-Hofmann was one of a number of German manufacturers who competed to build Riesenflugzeug (giant aircraft) for the German air service during World War 1. This was despite the fact that Linke-Hofmann being principally a manufacturer of railway rolling stock, with little aeronautical experience.
Linke-Hofmann designed the fuselage of the R.I to completely fill the interplane gap of the widely separated biplane wings. Encouraging data from tests at the MLStG Laboratory at Göttingen suggested there would be advantages in this configuration.
The capacious fuselage housed the crew compartments as well as the four engines and their clutches and combining gearboxes. This configuration offered the advantage that the engines could be accessed in-flight for adjustment or minor repairs. However, there were serious problems during development with engine cooling and vibration.
Construction of the R.I was largely of wood covered by transparent Cellon (Cellulose acetate) in the first prototype, R.I number 8/15, and lozenge camouflage fabric in the second aircraft, 40/16.
Cellon was used with the intention of making the aircraft partially transparent and so less visible; however, the Cellon reflected sunlight, making the aircraft more visible, before quickly yellowing due to the effect of ultra violet radiation. It also shrank and stretched due to in-flight temperature changes, with detrimental effect on trim.
The forward section of the fuselage was divided into three levels. The top deck housed the pilots and wireless station, the middle the engine compartment and the lower the bombardiers, fuel tanks and payload. It has to be noted that this configuration would have made the aircraft top heavy when, after expending its fuel and weapon payload, it eventually landed.
The Linke-Hofmann R.I was powered by four in-board Mercedes D.IVa engines, rated at 260 hp (194 kW), coupled to a gear-box assembly which transferred power through shafts to two tractor propellers mounted between the wings, giving the aircraft a maximum speed of 140 km/h (87 mph).
...
Wikipedia