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The Boeing T50 (company designation Model 502) was a small turboshaft engine produced by Boeing. Based on Boeing's earlier Model 500 gas generator, the T50's main application was in the QH-50 DASH helicopter drone of the 1950s. An up-rated version designated Model 550 was developed to power the QH-50D and was given the military designation T50-BO-12. ==Variants== ;T50-BO-4: at 6,000 output rpm, military rating turboprop. ;T50-BO-6: ;T50-BO-8: at 5,950 output rpm, revised reduction gear ratio, fuelsystem and other changes.〔 ;T50-BO-8A: ;T50-BO-10: at 6,000 output rpm〔 ;T50-BO-12: ;502-2E:Turboprop, at 2,900 output rpm max. continuous at sea level. ;502-7B:Compressed air generator.〔 ;502-8A:Turboshaft.〔 ;502-8B:Turboprop, at 37,500 compressor rpm for take-off.〔 ;502-10B:Turboprop, at 37,500 compressor rpm for take-off.〔 ;502-10C: ;502-10V: (T50-BO-4) ;502-10VB: at 3,000 output rpm, variant of -10V / T50-B0-4 with revised reduction gear ratio.〔 ;502-10VC: (T50-BO-8) ;502-11:Compressed air generator.〔 ;502-12B: ;502-W ;502-14: (T50-BO-10) ;550-1: (T50-BO-12) 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Boeing T50」の詳細全文を読む スポンサード リンク
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