The Height-Velocity diagram or H/V curve is a graph charting the safe/unsafe flight profiles relevant to a specific helicopter. As operation outside the safe area of the chart can be fatal in the event of a power or transmission failure it is sometimes referred to as the dead man's curve or Coffin Corner by helicopter pilots.
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- The Height-Velocity diagram or H/V curve is a graph charting the safe/unsafe flight profiles relevant to a specific helicopter. As operation outside the safe area of the chart can be fatal in the event of a power or transmission failure it is sometimes referred to as the dead man's curve or Coffin Corner by helicopter pilots. In the simplest explanation, the H/V curve is a diagram where the shaded areas should be avoided, as the average pilot may be unable to complete an autorotation landing without damage. The H/V curve will usually contain a take-off profile, where the diagram can be traversed from 0 height and 0 speed to cruise, without entering the shaded areas or with minimum exposure to shaded areas. The portion in the upper left of this diagram demonstrates a flight profile which will likely not allow the pilot to successfully complete an autorotation, primarily due to having insufficient airspeed to enter an autorotative profile in time to avoid a crash. The shaded area on the lower right is dangerous due to the airspeed and proximity to the ground resulting in dramatically reduced reaction time for the pilot in the case of mechanical failure, or other in-flight emergencies. This shaded area at the lower right is not portrayed in H/V curves for multiengine helicopters capable of safely hovering and flying with a single engine failure. The following examples further illustrate the relevance of the H/V curve to a single engine helicopter. At low heights with low airspeed, such as a hover taxi, the pilot can simply cushion the landing with collective, converting rotational inertia to lift. The aircraft is in a safe part of the H/V curve. At the extreme end of the scale (say a three-foot hover taxi at walking pace) even a complete failure to recognise the power loss resulting in an un-cushioned landing would probably be survivable. As the airspeed increases without an increase in height, there comes a point where the pilot's reaction time would be insufficient to react with a flare in time to prevent a high-speed, and thus probably fatal, ground impact. Even small increases in height give the pilot much greater time to react, thus the bottom right part of the H/V curve is usually a shallow gradient. If above ideal autorotation speed, the pilot's instinct is usually to flare to convert speed to height and increase rotor RPM through coning; which also immediately gets them out of the dead man's curve. Conversely, an increase in height without a corresponding increase in airspeed will put the aircraft above a survivable un-cushioned impact height, and eventually above a height where rotor inertia can be converted to sufficient lift to enable a survivable landing. This occurs abruptly with airspeeds much below the ideal autorotative speed. The pilot must have enough time to accelerate to autorotation speed in order to be able to successfully autorotate; this directly relates to a requirement for height. Above a certain height the pilot can achieve autorotation speed even from a 0-knot start, thus putting "high hovers" outside the curve. The typical safe takeoff profile will involve initiation of forward flight from a low hover, only gaining height as airspeed approaches a safe autorotative speed but keeping above the lower right area of the H/V curve.
- Höjd-hastighetsdiagrammet (engelska H/V-Diagram) för en helikopter visar de flygtillstånd från vilka piloten kan utföra respektive inte utföra en säker autorotationslandning vid motorbortfall. På den vertikala axeln återfinns flyghöjden, på den horisontella hastigheten. För att kunna genomföra en autorotationslandning behövs tillräcklig energi i rotorsystemet för att kunna utföra en så kallad ”flare” för en kontrollerad landning. Man får här göra skillnad på kinetisk energi på grund av helikopterns hastighet och potentiell energi bestående av dess höjd över den tänkta landningsplatsen. Om helikoptern har en hög hastighet kan vid motorbortfall rotorn hållas i rörelse och lyftkraften bibehållas genom att piloten minskar hastigheten hos helikoptern och konverterar rörelseenergin hos helikoptern till rotationsenergi hos rotorn i stället. Om helikoptern har hög höjd kan helikopterns potentiella energi konverteras till rotationsenergi hos rotorn då helikoptern sjunker, vilket ger tillräcklig lyftkraft för en säker landning. Diagrammet visar de två områden som utgör risker. Det streckade området till vänster motsvarar ett område där den totala energin (kinetisk energi plus potentiell energi) hos helikoptern inte är tillräcklig för att konverteras till rörelseenergi hos rotorn som räcker för en säker landning, vilket med största sannolikhet resulterar i ett mer eller mindre allvarligt haveri. Området nere till höger är också farligt därför att det utgör en stor risk att landa i höga farter. Innan en pilot hinner reagera på ett plötsligt motorbortfall kan helikoptern förlora höjd och kollidera med marken.
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- The Height-Velocity diagram or H/V curve is a graph charting the safe/unsafe flight profiles relevant to a specific helicopter. As operation outside the safe area of the chart can be fatal in the event of a power or transmission failure it is sometimes referred to as the dead man's curve or Coffin Corner by helicopter pilots.
- Höjd-hastighetsdiagrammet (engelska H/V-Diagram) för en helikopter visar de flygtillstånd från vilka piloten kan utföra respektive inte utföra en säker autorotationslandning vid motorbortfall. På den vertikala axeln återfinns flyghöjden, på den horisontella hastigheten. För att kunna genomföra en autorotationslandning behövs tillräcklig energi i rotorsystemet för att kunna utföra en så kallad ”flare” för en kontrollerad landning.
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- Height-velocity diagram
- Höjd-hastighetsdiagram
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