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2. Make up meaningful sentences from the following words:

  1. is/ engines/ fighter/ to use/ the thrust-vectoring/ the S-37/ designed

  2. intake/ section/ large/ are located/ two/ fuselage/ auxiliary/ centre/doors/ on the

  3. canards/ side/ the Su-37/ intake/ has/ on the/ large/ mounted

  4. wave/ the airframe/ with/ absorbent/ is/ radio/ with

  5. the S-37 fighterussia`s/ it/ that/ to become/ fighter/ clear/ fifth/ now/ is/ is intended/ generation

Speaking

1. Work in pairs. Your authorities give you the task to introduce some improvements of aircraft Su-37. Cooperate and prove your point of view speaking on your improvements.

UNIT 4

Vertical Horizons

Preparing to read

  1. Read the title of the text and think of all possible terms that may relate to the topic.

  2. Work in pairs. Share the words and give your prediction about the content of the text.

Reading

1. Skim the text and try to guess and explain the meaning of the underlined words or word – combinations.

Vertical Horizons

A. People have dreamed of taking off and landing vertically for as long as they have dreamed about flying. But today the two classes of air vehicle remain fundamentally fixed-wing distinct: those that hover efficiently and those that fly efficiently. Closing the gap between rotary-wing and fixed-wing aircraft is the dream of vertical flight proponents, and designers are pursuing two paths: improving the efficiency of helicopters and perfecting new configurations.

B. The first “free” vertical flight was made by Frenchman Paul Cornu in 1907, barely four years after the Wright brother’s first flight, but the machine was impractical. Autogyros became quite sophisticated between the wars, but they were not true vertical take-off and landing (VTOL) machines. The first practical helicopters were the German side-by-side rotor Focke-Angelis Fa61 of 1936 and intermeshing-rotor Flettner Fl282 of 1941. But Igor Sikorsky’s VS300 defined the modern single-rotor helicopter when it first flew in 1939.

C. Despite all the technological progress since then, helicopters remain niche players in aviation. Compared with equivalent fixed-wing aircraft, they are still more expensive to buy and costly to operate; they are too noisy inside and out; and they vibrate too much for the comfort of their occupants or the longevity of their components. Yet helicopters are arguably the most versatile and useful of air vehicles.

Room for improvement

D. There is still considerable development potential in conventional helicopter, albeit incremental. Higher speeds, heavier payloads, less noise and vibration, and lower production and operating costs are possible. Typical industry goals for a 2020-timeframe helicopter include a 200kt (370km/h) cruise speed; 30% reductions in empty weight and fuel consumption; 60%lower external noise; fixed-wing levels of vibration and safety; 30-50% lower development, production, operation and maintenance costs; and all-weather operability.

E. The latest helicopters can cruise at up to 160kt, but this is an economical, rather than physical barrier. At 160kt the power required in forward flight is close to the power required in hover; to increase speed the power required in level flight has to be reduced. This will require lower-drag airframes, active rotor control and antitorque concepts. Eurocopter’s Dauphin-based DGV200 demonstrator has cruised at 195kt, and exceeded 200kt, proving that faster helicopters are possible.

F. More important than higher speed are lower noise and vibration, as both are barriers to the wider acceptance of helicopters. External noise is being tackled with rotor designs and operating procedures. The latest high-thrust blades allow the main rotor to be slowed in the cruise, reducing fly-over noise, and both passive and active means to reduce approach noise are being evaluated.

G. The main source of noise on the descent is blade vortex interaction (BVI) – the main rotor blades hitting the air shed by preceding blades. Among the mitigating technologies NASA has evaluated is the low-noise planform rotor. This has a “wavy” blade that distributes the shed air and reduces BVI noise. Another is the modulated rotor, in which the blades are spaced unevenly to generate a more random, less annoying noise.

H. A third concept for reducing BVI noise is the active twist rotor, in which the load distribution and spatial position of each blade is controlled individually. This reduces the strength of the wake and allows the blade to be “flown” away from the air shed by the preceding blade. The active twist rotor has shown substantial reduction in noise and vibration in NASA windtunnel testing.

I. Active rotor control is a feature of most advanced low-noise, high-speed helicopter designs, with advances in materials and electronics making individual blade control practical. Manufacturers are testing main rotor blades with active servo flaps driven by piezo-electric actuators. These are precursors to smart-material “morphing” blades that would allow elimination of the mechanical swashplate used to control blade pitch.

J. Smart, or active, structures also promise to reduce internal noise, as well as vibration. Passive vibration reduction has reached its limits, with the trend towards variable rotor RPM to reduce external noise requiring an adaptive antivibration system. Approaches being tested include acoustically active gearbox struts and cabin ceiling panels fitted with piezo-electric actuators that oscillate to cancel out noise and vibration.

K. Pushing helicopter speeds higher may require a new approach. One concept receiving attention is the reverse velocity rotor. This tackles the fundamental limit on the forward speed of a conventional helicopter, which is a result of the rotor flying sideways. As forward speed increases, airflow over the advancing blade gets faster while that over the retracting blade gets slower. Eventually the retreating blade begins to stall, setting the speed limit.

L. The reverse-velocity rotor (RVR) has a double-ended aerofoil that generates lift whichever way the air is flowing over the blade. As forward speed increases, the rotor is slowed until the retreating blade is immersed in reverse flow, but still producing lift. This requires a variable-speed transmission and auxiliary propulsion, as at high speed the rotor is autorotating and pitch and yaw control is provided by thrust vectoring.

M. Windtunnel testing indicates the reverse-velocity rotor is capable of cruise speeds exceeding 300kt, but it retains the simplicity of a helicopter with no reconfiguration required to transition from vertical to forward flight. Under NASA contract, Sikorsky has studied an 80-passenger RVR runway-independent aircraft, with three engines, an eight-blade rotor and ducted-fan propulsor on the tail. The baseline RVR has a 340kt cruise and 1,000km range. Compounding – adding a wing to offload the rotor in the cruise – results in a smaller aircraft for the same mission, but increases empty weight and hover download.