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tulip valve<br />

burner at fuel pressure not high enough to atomize continuous<br />

film but too high for it to converge as bubble.<br />

tulip valve Piston-engine exhaust valve shaped in side<br />

elevation like tulip.<br />

Tumav Tactical unmanned multirole air vehicle.<br />

tumble 1 To rotate about lateral axis, ie end over end;<br />

rare in aircraft but not uncommon in spacecraft.<br />

2 To rotate metal parts in drum, often with powder<br />

abrasive, to remove flash or burrs and obtain polished<br />

surface.<br />

3 Of gyro wheel, to precess to limit after toppling.<br />

tumblehome Distance measured parallel to transverse<br />

axis from vertical line through widest extremity of<br />

seaplane or flying-boat hull to any point on skin above.<br />

tumblehome line Abrupt change of curvature of mould<br />

line, buttock line or water-level contour at end of contour<br />

[marine aircraft].<br />

tumble limit Angular displacement in pitch or roll at<br />

which traditional gyro instrument is on gimbal stops.<br />

tumbler Drum in which metal parts are tumbled (2).<br />

tumbler switch Snap-action electrical switch with short<br />

operating lever.<br />

tumbling To tumble (1, 2, 3); to be in that condition.<br />

tunable beam approach Pre-ILS landing system (BABS,<br />

SBA) in which pilot tuned receiver to particular airfield<br />

(arch.).<br />

tundra tyre Low-pressure tyre suitable for operations<br />

from snow.<br />

tuned-bandpass transformer Typically, primary winding<br />

forms anode load of one stage and secondary drives grid<br />

of succeeding stage.<br />

tuned circuit Oscillatory circuit with capacitance and<br />

inductance selected or tuned to resonate at frequency of<br />

applied signal.<br />

tuned-grid circuit Parallel resonant circuit linking grid<br />

and cathode with maximum response at resonant<br />

frequency; similar resonant response for tuned anode<br />

circuit.<br />

tuner Subcircuit or device in RF receiver which selects<br />

desired frequency and rejects all others.<br />

tungsten Silver-grey metal, symbol W, density 19.3, MPt<br />

3,407°C; one of densest, hardest, strongest and most<br />

refractory metals known.<br />

tungsten inert-gas welding DC current is passed through<br />

cathode of 4% thoriated tungsten and through workpiece<br />

with high-purity argon fed to both sides of weld and to<br />

form gas lens from torch.<br />

Tungum Corrosion-resistant alloy of copper with 14.6%<br />

zinc and small amounts of other metals.<br />

tuning 1 Fine adjustment over continuous analog range<br />

of values to obtain that desired, eg RF frequency/wavelength<br />

or optimum operating condition of engine or other<br />

device.<br />

2 See airframe *.<br />

tunnel 1 See wind tunnel.<br />

2 Axial fairing along body, eg to cover pipes, cables and<br />

other lines routed outside skin.<br />

3 Channel along which baggage passes through<br />

screener.<br />

tunnel diode Semiconductor device having single p-n<br />

junction across which electrons flow by quantum<br />

tunnelling; when biased to centre of a negative-resistance<br />

mode can operate as amplifier, oscillator or switch.<br />

tunnel shock That occurring immediately downstream<br />

turbine temperatures<br />

of supersonic working section in wind tunnel when Mach<br />

number falls below unity; intense if no second throat.<br />

tunnel vision Inability to perceive anything outside an<br />

extremely small angular range of FOV, as if one were in a<br />

tunnel; caused by disease or high g.<br />

TUP Technology utilization program (NASA, technology<br />

transfer).<br />

turb, TURBC Turbulence (ICAO).<br />

turbidity Any condition of atmosphere which reduces its<br />

transparency to radiation, esp. optical; term normally<br />

applied to cloud-free sky where * is caused by suspended<br />

matter, scintillation and other effects.<br />

turbine 1 Gas-turbine shaft power, ie turboshaft or<br />

turboprop; eg helicopter can be said to have * power.<br />

2 Prime mover whose power is obtained by action of<br />

working fluid (water, steam, cold or hot gas, etc) to give<br />

tangential circumferential forces reacting on blades or<br />

shaped passages which rotate a shaft. At redline speed a<br />

modern turbofan blade can move at 460 m (1,500 ft) s -1 ,<br />

under 60,000 g. One or more are source of power in all gas-<br />

* engines and in turbochargers, turbopumps and many<br />

other rotary machines.<br />

turbine-airscrew unit See turboprop.<br />

turbine bearing Bearing supporting turbine shaft.<br />

turbine blade Radial aerofoil mounted in edge of turbine<br />

disc whose tangential force rotates turbine rotor. Each<br />

turbine stage has many blades, occasionally fabricated in<br />

groups of two or more. Called bucket in US. Inwardsradial<br />

turbine does not have *.<br />

turbine disc Central member upon which turbine rotor<br />

blades are mounted; in some modern engines the blades<br />

and disc are monolithic. In many multistage turbines there<br />

are no flat discs, first and last stages being conical and<br />

intervening stages being rings gripped between them.<br />

turbine entry temperature See turbine temperatures.<br />

turbine gas temperature See turbine temperatures.<br />

turbine rotor Complete turbine rotating assembly with<br />

1–6 stages; stators are excluded.<br />

turbine shroud Shroud around periphery of turbine<br />

rotor stage, formed by * section on tip of each blade.<br />

turbine stage Single turbine disc or ring with inserted<br />

blades; for completeness should be associated with<br />

preceding stator (IGV) stage.<br />

turbine stator Ring of fixed blades, also called inlet guide<br />

vanes, upstream of each turbine rotor stage, on to whose<br />

blades ** directs gas with optimum distribution of V and<br />

pressure for maximum turbine work and efficiency (eg<br />

changes radial pressure/V, previously uniform, so that<br />

with increasing radius pressure increases while V falls).<br />

turbine temperatures This entry describes temperatures<br />

in gas-turbine engines. Alphabetically, these are: CET,<br />

CIT, COT, EGT, RIT, SOT, TDT, TET, TGT and TIT.<br />

Following a particle through an engine, CIT is<br />

compressor inlet temperature, which is that of the ambient<br />

atmosphere corrected for any ram effect. COT is<br />

compressor outlet temperature, measured immediately<br />

behind the final stage of compression. CET, combustor<br />

exit temperature (also called combustion chamber outlet<br />

temperature, giving a second meaning for COT) is the<br />

temperature of the gas at the entry to the first-stage<br />

turbine stator. SOT is stator (first-stage) outlet temperature.<br />

The gas is then cooled 20°–120°C by injection of<br />

cooling air from the turbine disc (whose temperature TDT<br />

is cooled by the airflow) and other sources to give the RIT<br />

726

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