Boeing XF5B-1

     
Název:
Name:
Boeing XF5B-1 Boeing XF5B-1
Originální název:
Original Name:
Boeing XF5B-1
Kategorie:
Category:
stíhací-bombardovací letoun fighter-bomber aeroplane
Výrobce:
Producer:
DD.MM.1930-DD.MM.1930 Boeing Aircraft Division, United Aircraft & Transport Corp., Seattle, Washington
Období výroby:
Production Period:
DD.MM.1930-DD.MM.1930
Vyrobeno kusů:
Number of Produced:
1
První vzlet:
Maiden Flight:
09.02.1930
Osádka:
Crew:
1
Základní charakteristika:
Basic Characteristics:
 
Vzlet a přistání:
Take-off and Landing:
CTOL - konvenční vzlet a přistání CTOL - conventional take-off and landing
Uspořádání křídla:
Arrangement of Wing:
jednoplošník monoplane
Uspořádání letounu:
Aircraft Concept:
klasické conventional
Podvozek:
Undercarriage:
pevný fixed
Přistávací zařízení:
Landing Gear:
kola wheels
Technické údaje:
Technical Data:
 
Hmotnost prázdného letounu:
Empty Weight:
935 kg 2062 lb
Vzletová hmotnost:
Take-off Weight:
1274 kg 2808 lb
Maximální vzletová hmotnost:
Maximum Take-off Weight:
? kg ? lb
Rozpětí:
Wingspan:
9.3 m 30ft 6in
Délka:
Length:
6.4 m 21ft
Výška:
Height:
2.84 m 9ft 4in
Plocha křídla:
Wing Area:
14.61 m2 157.3 ft2
Plošné zatížení:
Wing Loading:
? kg/m2 ? lb/ft2
Pohon:
Propulsion:
 
Kategorie:
Category:
pístový piston
Počet motorů:
Number of Engines:
1
Typ:
Type:
Pratt & Whitney R-1340B nebo C o výkonu 361 kW v 2438 m
dvoulistá kovová vrtule Hamilton Standard
Pratt & Whitney R-1340B or C, power 485 hp at 8000 ft
Hamilton Standard two-blade metal propeller
Objem palivových nádrží:
Fuel Tank Capacity:
500 l 132 US gal
Výkony:
Performance:
 
Maximální rychlost:
Maximum Speed:
294.5 km/h v 2438 m 183 mph in 8000 ft
Cestovní rychlost:
Cruise Speed:
233.4 km/h v ? m 145 mph in ? ft
Rychlost stoupání:
Climb Rate:
9.4 m/s 1850 ft/min
Čas výstupu na výšku:
Time to Climb to:
10 min do 4877 m 10 min to 16000 ft
Operační dostup:
Service Ceiling:
8047 m 26400 ft
Dolet:
Range:
627.6 km 390 mi
Maximální dolet:
Maximum Range:
? km ? mi
Výzbroj:
Armament:
1x 7,62mm a 1x 12,7mm kulomet Browning

5x 11kg bomba nebo
1x 227kg bomba
1x fixed .30 and 1x .50 Browning machine gun

5x 25 lb bomb or
1x 500 lb bomb
Uživatelské státy:
User States:
Poznámka:
Note:
- -
Zdroje:
Sources:
Bowers, Peter M. Boeing Aircraft since 1916. London, Putnam 1989. ISBN 0-85177-804-6.
Swanborough, F. G.; Bowers, P. M. US Navy Aircraft Since 1912, Putnam Aeronautical Books, London 1990. ISBN 0-85177-838-0.
Pelletier, Alain. Boeing - The Complete Story. Haynes Publishing, Yeovil 2010. ISBN 978-1-84425-703-4.
Matt, Paul R. United States Navy and Marine Corps Fighters 1918-1962. Harleyford Publications, Los Angeles 1962.
http://www.airwar.ru/enc/fww1/f5b.html

Boeing XF5B-1 - XF5B-1 v původní podobě, zvnějšku odlišitelný od XP-15 jen podle přistávacího háku.

XF5B-1 v původní podobě, zvnějšku odlišitelný od XP-15 jen podle přistávacího háku.
URL : https://www.valka.cz/Boeing-XF5B-1-t121984#417210 Version : 0
Model 205 was a double of the Model 202, or XP-15, but was intended as a carrier-based fighter-bomber, of which were based on changes in the internal structure and the resulting weight. From the outside initially looked basically like trapping a hook-equipped XP-15, high-wing with poloskořepinovým hull, roughly in the shapes of its direct dvouplošného predecessor F4B-1, slightly larger wing has the same outline as in F4B, however, it was all-metal, from the ground and a covering of duralumin and with the profile of the Boeing 106. It should also be waterproof and help from sinking in the event of landing on water. Because the XP-15 were carried out the same adjustments, soon looked both machines again almost the same.

Factory tests have not been carried - Boeing has already tested the XP-15 and assumed sufficiently identical characteristics. 9. February 1930. loaned to the navy, 14. February flown to Anacostie. Until June has been tested on NAS Anacostia and NAS Norfolk, have been tested two engines, the R-1340B and R-1340C, with different ratios of compression, later with a motor ring type Townend and also two different on the ground adjustable metal propeller company, Hamilton Standard, with a diameter of 2,74 m and 2,64 m. Was praised maneuverability, but had too long a runway, and three times failed tail wheel. Because of the improved stability soon got a new higher round rudder coated by corrugated sheets.

10. may the 1930s was the Model 205 the navy repurchased, with the official designation XF5B-1. Yet he was operated with civil registrations X271V and in civil coloring - hull was in the "Boeingově green", wing top orange and the bottom light gray, gray, were also the tail surfaces and struts, now got a standard coloring of the navy. Shortly after the tests were completed with the fact that after a little editing would go on a machine suitable for operation on aircraft carriers, but he was not recommended as the serial type. Instead, the navy ordered a new dvouplošnou version, F4B-2, but she used some of the elements developed for the XF5B-1, as a tail wheel and a ring Townend, and the corporate prototype Model 208 used even poloskořepinový fuselage and tail surfaces, which from him took the serial F4B-3 and P-12E. Only all-metal wing is not used, it was the last of the sea dvouplošníků, XF6B-1. XF5B-1 then served to the experiments and his career ended in October 1933, when it was destroyed in static tests.

Source:
Bowers, Peter M. Boeing Aircraft since 1916. London, Putnam 1989. ISBN 0-85177-804-6.
Swanborough, F. G.; Bowers, P. M. US Navy Aircraft Since 1912, Putnam Aeronautical Books, London 1990. ISBN 0-85177-838-0.
Pelletier, Alain. Boeing - The Complete Story. Haynes Publishing, Yeovil 2010. ISBN 978-1-84425-703-4.
Matt, Paul R. The United States Navy and Marine Corps Fighters 1918-1962. Harleyford Publications, Los Angeles, 1962.
https://www.airwar.ru/enc/fww1/f5b.html
.
Boeing XF5B-1 - Finální podoba

Finální podoba
Boeing XF5B-1 -


URL : https://www.valka.cz/Boeing-XF5B-1-t121984#417328 Version : 0
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