The Nakajima Mamoru (護, Preserve) engine was a 14-cylinder, air-cooled, two-row radial engine of 1870 hp. The Nakajima model designation for this engine was NAK while it was an experimental project, in service it was known as the NK7, and known as the Ha-103 by the Army and "Mamori" or "Mamoru" by the Navy. According to unified designation code it was Ha-36. The meanings of these two Japanese words are very similar, Mamori translates as 'protection' and Mamoru, translates as 'to guard, protect, defend and obey'.[1]
At some 44.9 litres (2,740 in²) displacement, it was one of the largest-displacement 14-cylinder radial engines in the world, rivalling the similar configuration American 42.7 litre (2,600 in²) Wright R-2600 Twin Cyclone engine, of Soviet 41.2 litre (2,515 in²) Shvetsov ASh-82 engine of displacement levels, 53.6 L Bristol Centaurus, and was meant to compete with early 18-cyl engines.
Competing against the successful Mitsubishi Kasei engine, the Mamoru proved to be unreliable and was rarely able to operate near its design power. Designs based on the Mamoru were forced to use other engines, typically the less powerful Mitsubishi Kasei or the Nakajima Homare. Production of the Mamoru was ended by the Navy after only a few hundred production examples were built.
The Mamoru was Nakajima's seventh air-cooled design, which led to its designation: N for Nakajima, K for air-cooled, 7 for the 7th design, and A for the major model number. Two sub-models were built with minor changes, the Model 11 for the Navy, and the Model 12 for the Army. Both produced 1,850 hp
The first application of the Mamoru was on the first prototype of the Nakajima G5N1 Genzan. The G5N1 had been designed on the basis of the Douglas DC-4E as Japan's first four-engine bomber and proved to be a disappointment. These problems were compounded by the unreliability of the early Mamoru engines, which had to be de-tuned and left the G5N1 underpowered. The G5N1's maiden flight was on 10 April 1941, and a further four prototypes were built with the Mamoru. In an attempt to salvage the project, two additional airframes were fitted with 1,530 hp Mitsubishi MK4B 12 Kasei engines and redesignated G5N2s. Although the Mitsubishi engines were more reliable than the original Mamoru 11s, further development was halted. Of the six completed Shinzans, four of them (two G5N2s and two G5N1s re-engined with the Kasei 12) were relegated for use as long-range Navy transports under the designation Shinzan-Kai Model 12 Transport G5N2-L.
The Nakajima Mamoru was also used on the Nakajima B6NTenzan ('heavenly mountain') carrier based torpedo bomber aircraft. The Navy requested this aircraft based on the Kasei, but Nakajima's Kenichi Matsumara insisted on using their Mamoru. The B6N first flew on 14 March 1941, demonstrating several problems, notably the poor engine reliability. With the delay of 2 years, by 1943 the engine had improved to the point where serial production was allowed to start, but after only 133 B6N1s had been delivered the Navy ordered the switch to the 1,850 hp (1380 kW) Mitsubishi MK4T Kasei 25. The rest of the 1,268 B6N2s were Kasei powered.
Variantsedit
Mamoru 11 NK7A
1,870 horsepower (1,390 kW) at 2,600 rpm (take-off) 1,750 horsepower (1,300 kW), 2,500 rpm at 1,400 metres (4,600 ft) 1,600 horsepower (1,200 kW), 2,500 rpm at 4,900 metres (16,100 ft)
Mamoru 12 Ha-103
As NK7A
Applicationsedit
Nakajima B6N 1 X 1,870 hp (1395 kW) Nakajima NK7A Mamoru 11
Nakajima G5N 4 X 1,870 hp (1395 kW) Nakajima NK7A Mamoru 11
Francillon, Ph.D., René J. Japanese Aircraft of the Pacific War. London: Putnam & Company, 2nd edition 1979. ISBN0-370-30251-6. pg 425
Goodwin, Mike & Starkings, Peter (2017). Japanese Aero-Engines 1910-1945. Sandomierz, Poland: MMPBooks. ISBN978-83-65281-32-6.
External linksedit
Wikimedia Commons has media related to Nakajima Mamoru.
March 11, 2024
nakajima, mamoru, preserve, engine, cylinder, cooled, radial, engine, 1870, nakajima, model, designation, this, engine, while, experimental, project, service, known, known, army, mamori, mamoru, navy, according, unified, designation, code, meanings, these, jap. The Nakajima Mamoru 護 Preserve engine was a 14 cylinder air cooled two row radial engine of 1870 hp The Nakajima model designation for this engine was NAK while it was an experimental project in service it was known as the NK7 and known as the Ha 103 by the Army and Mamori or Mamoru by the Navy According to unified designation code it was Ha 36 The meanings of these two Japanese words are very similar Mamori translates as protection and Mamoru translates as to guard protect defend and obey 1 MamoruNakajima Mamoru engine at the National Air and Space MuseumType Piston aircraft engineManufacturer Nakajima Aircraft CompanyDesigner Kiyoshi TanakaFirst run 1941Major applications Nakajima G5N Nakajima B6NNumber built 200Developed from Nakajima HikariDeveloped into Ha 107 Ha 117 Ha 217At some 44 9 litres 2 740 in displacement it was one of the largest displacement 14 cylinder radial engines in the world rivalling the similar configuration American 42 7 litre 2 600 in Wright R 2600 Twin Cyclone engine of Soviet 41 2 litre 2 515 in Shvetsov ASh 82 engine of displacement levels 53 6 L Bristol Centaurus and was meant to compete with early 18 cyl engines Competing against the successful Mitsubishi Kasei engine the Mamoru proved to be unreliable and was rarely able to operate near its design power Designs based on the Mamoru were forced to use other engines typically the less powerful Mitsubishi Kasei or the Nakajima Homare Production of the Mamoru was ended by the Navy after only a few hundred production examples were built Contents 1 Design and development 2 Variants 3 Applications 4 Specifications Nakajima NK7A Mamoru type 11 12 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 References 6 1 Notes 6 2 Bibliography 7 External linksDesign and development editThe Mamoru was Nakajima s seventh air cooled design which led to its designation N for Nakajima K for air cooled 7 for the 7th design and A for the major model number Two sub models were built with minor changes the Model 11 for the Navy and the Model 12 for the Army Both produced 1 850 hpThe first application of the Mamoru was on the first prototype of the Nakajima G5N1 Genzan The G5N1 had been designed on the basis of the Douglas DC 4E as Japan s first four engine bomber and proved to be a disappointment These problems were compounded by the unreliability of the early Mamoru engines which had to be de tuned and left the G5N1 underpowered The G5N1 s maiden flight was on 10 April 1941 and a further four prototypes were built with the Mamoru In an attempt to salvage the project two additional airframes were fitted with 1 530 hp Mitsubishi MK4B 12 Kasei engines and redesignated G5N2s Although the Mitsubishi engines were more reliable than the original Mamoru 11s further development was halted Of the six completed Shinzans four of them two G5N2s and two G5N1s re engined with the Kasei 12 were relegated for use as long range Navy transports under the designation Shinzan Kai Model 12 Transport G5N2 L The Nakajima Mamoru was also used on the Nakajima B6N Tenzan heavenly mountain carrier based torpedo bomber aircraft The Navy requested this aircraft based on the Kasei but Nakajima s Kenichi Matsumara insisted on using their Mamoru The B6N first flew on 14 March 1941 demonstrating several problems notably the poor engine reliability With the delay of 2 years by 1943 the engine had improved to the point where serial production was allowed to start but after only 133 B6N1s had been delivered the Navy ordered the switch to the 1 850 hp 1380 kW Mitsubishi MK4T Kasei 25 The rest of the 1 268 B6N2s were Kasei powered Variants editMamoru 11 NK7A 1 870 horsepower 1 390 kW at 2 600 rpm take off 1 750 horsepower 1 300 kW 2 500 rpm at 1 400 metres 4 600 ft 1 600 horsepower 1 200 kW 2 500 rpm at 4 900 metres 16 100 ft Mamoru 12 Ha 103 As NK7AApplications editNakajima B6N 1 X 1 870 hp 1395 kW Nakajima NK7A Mamoru 11 Nakajima G5N 4 X 1 870 hp 1395 kW Nakajima NK7A Mamoru 11 Nakajima Ki 49 2 X 1 870 hp Nakajima Ha 103 Mitsubishi Ki 67 prototype 2 X 1 870 hp Nakajima Ha 103Specifications Nakajima NK7A Mamoru type 11 12 editData from Francillon p 433 General characteristics Type 14 cylinder supercharged air cooled two row radial piston engine Bore 155 mm 6 1 in Stroke 170 mm 6 7 in Displacement 44 9 L 2 740 cu in Diameter 1 380 mm 54 3 in Dry weight 870 903 kg 1 918 1 991 lb Components Valvetrain Pushrod operated overhead valve system with 4 valves per cylinder Supercharger Two speed single stage centrifugal Cooling system Air cooled Reduction gear 0 578Performance Power output takeoff 1 870 hp at 2 600 rpm cruise 1 750 hp at 2 500 rpm at 1 400 m Compression ratio 6 5See also editComparable engines BMW 801 Mitsubishi Kasei Pratt amp Whitney R 2800 Wright R 2600Related lists List of aircraft enginesReferences editNotes edit translated at eudict com Bibliography edit Francillon Ph D Rene J Japanese Aircraft of the Pacific War London Putnam amp Company 2nd edition 1979 ISBN 0 370 30251 6 pg 425 Goodwin Mike amp Starkings Peter 2017 Japanese Aero Engines 1910 1945 Sandomierz Poland MMPBooks ISBN 978 83 65281 32 6 External links edit nbsp Wikimedia Commons has media related to Nakajima Mamoru Retrieved from https en wikipedia org w index php title Nakajima Mamoru amp oldid 1193000418, wikipedia, wiki, book, books, library,
