F2C Seminar 13/07/2014 NOISE REDUCTION STANDARD FUEL

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Presentation transcript:

F2C Seminar 13/07/2014 NOISE REDUCTION STANDARD FUEL HOW TO ENCOURAGE GREATER PARTICIPATION?

F2C Noise reduction CIAM rule –Section 4C, part 1,1.2 b) states:- Noise limits shall be applied to powered model aircraft, with 96dB(A) at 3 metres for any category which does not have approval for any other noise rule. For many years we have used the latter part of this rule with our deflector shields and restricted exhaust outlet area.

F2C Noise reduction The Alternative Plan. From 01/01/2015 Step 1 b) The motor shall be naturally aspirated via a single round venturi with a maximum diameter of 3 mm. The venturi diameter shall be checked with a simple no-go plug gauge :Dia. 3,02 mm * 1,0 mm c) Any interconnecting chamber between the air intake and the induction port of the motor shall have a maximum volume of 1,25 cm3. No leakage is allowed between the venturi and the crankcase. d) There shall be no supplementary air induction except for sub piston induction to a maximum height of 0.6 mm at the exhaust port. THE CLEAR INTENT OF THIS IS TO ALLOW THE CONTINUED USE OF EXISTING MODELS AND ENGINES.

F2C Noise reduction Step 2 Experimental period – 2015 and 2016 contest seasons, noise tests at selected worldwide events, in races or preferably demonstration flights. record the noise levels and how achieved. Measurements taken at the center of the circle (pilot shoulder) and at 50 meters from the center of the circle,(these then used to calculate the noise level at 3 meters). It is not mandatory to use a 3mm venturi in demonstration flights (i.e. outside of competition flights). It is the responsibility of competitors to initiate the various experiments. It is essential part that the various results are widely communicated -to enable the work to progress rapidly (via F2 working group)

F2C Noise reduction Step 3 The F2 Committee shall present a proposal to 2016/ 2017 Plenary of the appropriate noise limit for F2C. Factors to be considered are site locations, the restricted operating area, height and duration of flights. Plus any other factors which mitigate the spread of noise. The agreed F2C noise limit will be circulated widely to assist the experimental work.

F2C Noise reduction Step 4 F2 Committee shall consider if it believes that further progress to the agreed F2C limit can be achieved by any of the experimentation route(s) so far demonstrated. If the answer is YES, the F2 Committee will present appropriate rules to the 2018 Plenary for implementation from 1st January 2019. If the answer is NO, the F2 Committee will present silencer based rules to the 2018 Plenary for implementation from 1st January 2019. The F2 Committee shall ensure that any such silencer solution rules are only drafted after open consultation with competitors and engine manufacturers on the preferred detail of that silencer rule.

Experiments so far 1 & 2 Volodymyr Fulitka ZALP engine.  Reduced exhaust period to135 degrees. Noise down by 4 dB to 93 dB at pilot in circle. Speed +0.2 secs.   YUGOV & SOSNOVSKI Kiev 2013 Venturi 3.0 mm Noise at pilot in circle 94dB(A) Flight speed18.3 – 18.9 (+1.3 – 1.8) for 42-44 laps 7

Experiments so far 3 & 4 Rob Metkemeijer PROFI, engine open exhaust Venturi 3.0 mm Noise at pilot in circle 92.2 dB (A) (-2.7) Flight speed 18.7 (+1.2) Profi engine with side resonant mini pipe. Venturi 4.85 mm Piston induction 0 mm Exhaust period ? Noise at pilot in circle 80 dB(A) (-14) Flight speed 18.4 (+1.1) 8

Experiments so far 5 & 6 Yugov Engine engine with side resonant mini pipe. Venturi 4.85 mm Piston induction 0 mm Exhaust period ? Noise at pilot in circle 82.1 dB(A) (-14) Flight speed 18.1 (+1.1) Rob Fitzgerald, Lerner Engine Open exhaust. Venturi 4.5 mm Piston induction 0.4mm Exhaust period ? Noise at pilot in circle 93.0 dB(A) Flight speed 16.9 for 33 laps. 9

Experiments so far 7 & 8 Rob Fitzgerald, Lerner Engine Venturi 3.0 mm Piston induction 0.4mm Exhaust period ? Noise at pilot in circle 88.0 dB(A) (-5) Flight speed 18.9 for 50 laps. Lerner engine with moulded bubble to duct the exhaust (hopefully more details to come) Noise at pilot in circle 85dB(A) Speed --no loss of speed. 10

Experiments so far 9 & 10 Lillo Condello Zalp Engine Venturi 4.5mm Noise at 3 metres 98.1 dB(A) Noise at 50 metres 74.4 dB(A) Noise at pilot in circle 89.3 dB(A) Flight speed 18.3 / 10. Lillo Condello Zalp engine Venturi 3 mm Noise at 3 metres 89.1dB(A) Noise at 50 metres 73.5 dB(A) Noise at pilot in circle 89.1 dB(A) Flight speed 19.4 / 10. 11

F2C Noise reduction Experiment summary @3meter @ pilot Exhaust in Exhaust out @pilot Exhaust front/rear fitted silencer @ 50 meters From centre. CIAM rule 96 85 80 82 72 1 Reduced exhaust period 93 2 3mm venturi 94 3 92.2 4 4.85mm venturi + mini pipe 5 4.85mm venturi +side resonant pipe 82.1 6 4.5mm venturi 84 7 88 81 8 external moulded exhaust bubble 9 98.1 89.3 74.4 10 89.1 73.5

Standard Fuel The F2 committee was tasked with reporting back to Plenary by 2016 on the viability of having a standard fuel in f2C. Proposal from Holland

HOW TO ENCOURAGE GREATER PARTICIPATION? Why are entries to World cup events declining? Why are there so few juniors in F2C? In 2013 world cup 46 juniors in F2D --Only 6 in F2C! Is the event losing its appeal?

How to make F2C more appealing? Would removing some of the expense and complication of F2C such as retracting undercarriage, multi fuels help? Would a minimum weight simplify construction so widening the appeal of the class? Do we need a different class to bridge the gap between F2C and F2F?