Railfan_Bill wrote:
When I was in the navy, I was stationed in a helicopter squadron, HS-@ out of Ream Field, San Diego. We were in the ASW game and out "choppers" were the SH-3A by Sikorsky. Our planes were powered by two T-58 Turbo-thrust engines. These engines were controlled by a variable load sensor on the rotors through the main gearbox. When we set the throttles, we placed it at 100% power setting. We could go to 117% power, but for only 5 minutes. The engines were then controlled by load factors as stated before. This is a large bird, but the smaller choppers do have a throttle control on the collective stick. This stick is on the left side of the pilot and it changes the pitch of all rotor bledes. Sensor keep the RPMs up, so the pilot must add fuel to maintain rotor speed. Hope this explains what large helicopters do to regulate fuel. RFB
When I was in the navy, I was stationed in a helic... (
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Even the smaller turbine powered helicopters maintained rpm via the load sensors on the engine. All the throttle control on the endofthe colledtive did was open the throttle to start position, then flight idle position, then 100%. The load sensors did all the rest. I'm talking about the Hughes OH-6A and the Bell OH-58A. I flew the Bell Jet Ranger 206 also worked that way. Now, the birds I learned on and instructed in, the Hiller 12E/OH-23, Bell OH-13 and Hughes TH-55/Hughes 300 had recip engines and throttle control was managed manually by the pilot manipulating the throttle control on the collective pitch lever. Took awhile to get that down pat. Once we learned that, we wondered why we couldn't do that before. Sort of like learning to drive in a car with a manual shift. Great fun.