Helipaddy 2022 Wrapped Quiz
Each answer is final, so choose carefully! Refresh the page to restart the quiz.
#1. Can birds fly “IMC” in clouds?
#2. What is the minimum altitude you are permitted to fly in the English Channel?
The answer depends on which side of the English Channel you are. There is a line through the middle of it, the FIR boundary, where airspace on one side belongs to the UK and on the other side to Europe.
Assuming no weather or visibility issues, the UK side of the FIR permits flying at zero feet, whereas on the European side the minimum is 500 feet. So, when flying to Europe, you may have to do a rapid climb at some invisible point halfway across – even if there is a cloud there!
#3. Would a helicopter take off on the moon?
Gravity on the moon is 1.6m/s/s (Earth is 10) so that’s great for flying machines. However, the moon has a total of 25 tonnes of air on the whole planet! This is more or less nothing so it is impossible for helicopter engines to function unless they carried their own air to mix with the fuel. Unfortunately, even such a helicopter would not be able to fly as the rotor blades would not have any air to work against. Helipaddy landing sites on the moon are therefore zilch.
Air density on Earth is 1.2 kg/m3. Visualise a cubic meter of air in front of you that has a surprisingly huge mass of more than a bag of sugar. Next time you fly through a windy valley, that’s probably several million tonnes of air sloshing about – it’s pretty heavy stuff.
#4. What is the highest number of main rotor blades of any operational helicopter?
Slight catch question because a chinook has two rotors each with three blades, so people may say 6. However, the appallingly named The Sikorsky CH-53E Super Stallion has 7 blades.
But… the Mil Mi-26, a Russian heavy transport helicopter, and the largest and most powerful helicopter to have ever gone into serial production, wins with EIGHT blades.
It’s notable that the highest theoretical lifting efficiency is achieved with the fewest blades and experiments have been done with single-blade rotors (with a counterweight – there were vibration problems that couldn’t be resolved).
So in practical terms, the most lift for the least power is achieved with a 2 blade rotor, but the need to absorb more power with a limited desirable disc diameter forces you to add more blades (or you may want a smaller rotor with lots of blades for manoeuvrability or other reasons, but it’s sub-optimal from a horsepower efficiency standpoint).
We don’t count the prototype with 20 blades – the Pescara Model 3 Helicopter.
#5. In the UK, are you allowed to fly through or land inside an ATZ without permission when it is closed?
The short answer is YES.
An ATZ at a civil aerodrome does not exist outside the notified hours of operation of the A/G, AFISO or ATC Unit. At a Government aerodrome, an ATZ will remain active during such times as are notified, regardless of the operational status of its ATS unit (UK AIP section ENR 2.2 and, where appropriate, certain section AD 2 items 2.17 refer). However, pilots are reminded that flying may take place outside of the published aerodrome operating hours and should therefore exercise caution when flying in the vicinity.
Details of ATZs, including hours of ATZ activation, will be published in the UK AIP at UK AIP ENR 2.2 OTHER REGULATED AIRSPACE ATZs and also in individual AD2 aerodrome entries at AD2.18, and for heliports in AD3 at AD3.16.
Reference to specific ATZ’s can be found in the ENR section 2-2-2-1/5 of the AIP.
#6. In the UK, are you ever allowed to fly through active danger areas?
The danger area is to caution pilots that it is necessary for them to assess the dangers in relation to their responsibility for the safety of their aircraft.
Be careful of the broader legislation though because the pilot is ultimately responsible for flight safety and must comply with the Air Navigation Order (ANO) 2016 articles 240 and 241 relating to endangerment:
- Article 240 – Endangering safety of an aircraft – a person must not recklessly or negligently act in a manner likely to endanger an aircraft, or any person in an aircraft.
- Article 241 – Endangering safety of any person or property – a person must not recklessly or negligently cause or permit an aircraft to endanger any person or property.
You cannot ever enter Prohibited as a civil pilot. You can enter Restricted with specific permission.
#7. Which is the only instrument that requires both the pitot tube and the static port?
Airspeed. So a faulty airspeed reading could be due to either device – more on this in our blog article here.
#8. At what point, during flight, is the airflow through the disc neither upward nor downward?
During autorotation, airflow is upwards and the aircraft is being slowed down by the air mass. During powered flight, airflow is downwards. So just at the point when transitioning into an autorotation, you will be in between the two for a brief moment.
During powered flight, in vortex ring conditions, the airflow will be down through the main rotor disc but will sweep around and mess with the clean air. Pilots are taught the Vuichard recovery technique to avoid this.
#9. The LOW FUEL test panel light has a delay - what is the reason?
To give the fuel a chance to settle in the tank. If the fuel had sloshed over and above the fuel sensor just at the point of pressing the button, then it might not detect low fuel.
If the fuel light comes in immediately during the test, it indicates a fault.
#10. The four forces acting on a helicopter in flight are:
Drag is actually composed of three types : profile, induced, and parasitic.
Profile drag develops from the frictional resistance of the blades passing through the air. It does not change significantly with the airfoil’s AOA but increases moderately when airspeed increases. Profile drag is composed of form drag and skin friction (from the paint). Form drag results from the turbulent wake caused by the separation of airflow from the surface of a structure.
Induced drag is generated by the airflow circulation around the rotor blade as it creates lift. The high-pressure area beneath the blade joins the low-pressure area above the blade at the trailing edge and at the rotor tips. This causes a spiral, or vortex, which trails behind each blade whenever lift is being produced. These vortices deflect the airstream downward in the vicinity of the blade, creating an increase in downwash. The component of lift that is acting in a rearward direction is induced drag.
Parasitic drag is caused by non-lifting components of the helicopter, such as the cabin, rotor mast, tail, and landing gear. Any loss of momentum by the airstream, due to such things as openings for engine cooling, creates additional parasitic drag.
The answer is A, drag is one of the forces.
#11. What is the most aerodynamic nose shape for a helicopter?
The droplet shape is the best for lowish speeds of helicopters. For transonic and supersonic the best shape is the sears-Haack body, like a nose cone. At low speeds, the shape of a tear minimizes the detachment of the flow from the surface that would generate drag due to turbulence. Flow detachment is caused by a condition called “adverse pressure gradient”.
So the droplet is the shape that minimizes this adverse pressure gradient.
The Hughes Model 369 had a distinctive teardrop-shaped fuselage that had strong crashworthiness properties and provided excellent external visibility. Customer preference and other design constraints ultimately led manufacturers to eschew the shape for one less aerodynamically efficient.
#12. In a modern turbine engine, how much of the airflow is used for cooling the engine versus used for combustion?
The burning process in a gas turbine engine is continuous, and nearly all of the cooling air must be passed through the inside of the engine. If only enough air were admitted to the engine to provide an ideal (stoichiometric) air/fuel ratio of 15:1, internal temperatures would increase to more than 2,000 °C. In practice, a large amount of air in excess of the ideal ratio is admitted to the engine. The large surplus of air cools the hot sections of the engine to acceptable temperatures ranging from 800° to 1,200 °C.
The air that comes from the compressor stages divides into three – Primary, Secondary and Tertiary. Out of these, only the Primary air enters directly into the chamber for combustion and only 25% of the air that comes from the compressor is this Primary air.
With thanks to Simon at Rolls Royce who helped with the answer to this question.
Wow, you are truly a Helipaddy Supremo!
Show everyone you’re a heli expert! Share your Helipaddy 2022 Wrapped Quiz results with your friends below.
Congrats! You successfully completed the Helipaddy 2022 Wrapped Quiz.
Share your result with your heli friends!