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    • 9. 发明专利
    • Improvements in and relating to aircraft
    • GB461170A
    • 1937-02-11
    • GB1796736
    • 1936-06-29
    • JOSEF KOENIGJAN KADLEC
    • B64C27/04
    • 461,170. Helicopters. KONIG, J., and KADLEC, J. June 29, 1936, No. 17967. Convention date, June 29, 1935. [Class 4] A helicopter, Fig. 1, has oppositely rotated superposed helical screws 1, 2, respectively secured to shafts 3, 5, which together with driving engines 7 and fuel tanks 16, are mounted in a casing 13 closed by a cover 14 and connected to a nacelle 12 bv trunnion bearings 15, Fig. 3, and adjustable relative thereto in the fore and aft plane. The adjusting means comprise a toothed segment 19 secured to casing 13 with which meshes a pilotoperated worm 20. The helical screws each consist of curved rods or tubes fitted into hubs keyed to the shafts and successively angularly displaced in such manner that when fabric is secured to the rib elements, helical surfaces are produced. A thrust bearing 27 is interposed between the two screws and shaft 3 carries a retaining nut 28. Shaft 3 is fitted with a pinion 4, Fig. 4, at its lower end and shaft 5 with an internally toothed gear ring 6. Gears 4 and 6 are engaged by pinions 8, 9 secured to driving shafts of motors 7.