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throttle back<br />

admission to engine of either air, fuel or (piston engine<br />

only) mixture.<br />

4 To reduce power of engine, also called to * back.<br />

5 To constrict fluid flow path and thus reduce mass<br />

flow.<br />

throttle back To reduce power.<br />

throttle friction Pilot-operated device which greatly<br />

increases resistance of throttle lever(s) to movement,<br />

effectively locking them in set position; also called friction<br />

lock.<br />

throttle icing Ice accretion in carburettor near or on<br />

partially closed throttle (3).<br />

throttle lock See throttle friction.<br />

throttle push Pilot action to increase power.<br />

throttle sensitivity Change in thrust or power per unit<br />

movement of throttle lever.<br />

throttle tension Locking resistance value of friction lock.<br />

throttling capability Range of thrust expressed as<br />

percentage to 100, over which liquid rocket (occasionally<br />

other type of engine or propulsion) is designed to operate.<br />

through-deck ship Generally, one with flight deck unobstructed<br />

by any full-width superstructure, even though<br />

not necessarily extending to bow.<br />

through hardening Heat treatment or other procedure<br />

which increases hardness through the entire piece of metal<br />

[see case hardening].<br />

through-stick feedback Characteristic of some autopilots<br />

that, when engaged, pilots flight controls move.<br />

through-thickness pinning Repair of major damage to<br />

composite structure in which numerous fine pins are<br />

collapsed by a foam carrier.<br />

throw 1 Part of crankshaft to which conrod attached,<br />

comprising webs and crankpin.<br />

2 Loose measurement of distance to which ECS freshair<br />

inlet projects, in absence of bulk cabin air movement.<br />

thrower ring Flange on rotating shaft which flings off<br />

leakage oil or other fluid.<br />

throw-off clutch Mechanical shaft drive which automatically<br />

disconnects as a particular condition is reached [in<br />

starting an engine, when torque falls to zero].<br />

throw weight Total mass of payload carried by ballistic<br />

missile, in case of ICBM including warheads, RVs, decoys<br />

and other penaids, post-boost propulsion and terminal<br />

guidance systems.<br />

THRP Port throttle (caption).<br />

THRS Starboard throttle (caption).<br />

THRU, Thru 1 Through.<br />

2 I am switching you to ...<br />

thrust Force, esp. that imparting propulsion, SI unit is<br />

newton (N), conveniently multiplied in kN = 224.80 lb st;<br />

1 lb st = 4.44483 N [see force for other conversions].<br />

Useful * of turbofan or turbojet is resultant of all * generated<br />

by fan (positive), front of combustor (positive),<br />

turbines (negative) and nozzles (negative),<br />

* at each location being AP + ––––<br />

WV<br />

g<br />

where A<br />

is area of flow cross section, P is pressure, W is mass flow<br />

W(V<br />

and V flow velocity. Overall net * is A (P-Po) + –––––––– j V)<br />

g<br />

where P is static pressure at nozzle, Po local atmospheric<br />

pressure, V j is jet velocity and V velocity of aircraft.<br />

thrust angle 1 Acute angle between axis of nozzle of<br />

canted solid motor and centreline axis of vehicle,<br />

measured in plane passing through both axes if possible.<br />

thrust/frontal area<br />

2 See propeller angle of attack.<br />

thrust augmentation Usually means afterburning, but<br />

also applied to water injection, and to piston engine<br />

ejector-exhaust schemes.<br />

thrust-augmented wing Aeroplane wing in which<br />

enhancement of circulation by powered-lift system also<br />

gives significant additional thrust (many arrangements,<br />

but augmentation of thrust invariably secondary<br />

objective).<br />

thrust axis Axis along which resultant propulsive thrust<br />

acts. With a turbofan this is resultant of fan and core jets,<br />

and with a turboprop that of propeller and (probably<br />

angled) jet. In multiengined aircraft * can oscillate<br />

because of engines outboard on flexible wing.<br />

thrust bearing Bearing, usually tapered roller, needle or<br />

ball, that resists axial shaft load due to propeller thrust.<br />

thrust buildup Sequence of programmed events in large<br />

rocket engine between ignition and liftoff.<br />

thrust bump Sudden uncommanded change [especially<br />

increase] in thrust.<br />

thrust chamber Complete thrust-producing portion of<br />

liquid rocket engine comprising combustion chamber and<br />

nozzle, often mounted on gimbals; not applicable to other<br />

types of engine.<br />

thrust coefficient 1 For propeller, basic performance<br />

calculation method based on Drzwiecki method of plotting<br />

grading curve of thrust against blade radius, yielding<br />

value k T , constant for each value of advance ratio J; **<br />

then equals k T J 2 and has symbol C T . This is also measured<br />

thrust divided by ρ n 2 D 4 where ρ is density, n rpm and D<br />

diameter.<br />

2 For rocket motor, measured ** is thrust: time integral<br />

over action-time interval divided by product of average<br />

throat area and integral of chamber pressure: time over<br />

action-time interval, symbol C f .<br />

3 For CC/BLC blowing slit, T/qS.<br />

thrust component In propeller theory (Drzwiecki), force<br />

on one element parallel to axis of rotation, T c ; convenient<br />

to plot T c as ordinate against blade radius, area under<br />

curve being measure of total thrust, T = N½ρV 2 ∫ r o T c dr<br />

where N is number of blades, ½ρV 2 dynamic head and T c<br />

integrated between axis of rotation (or, in practice,<br />

spinner diameter) and tip radius r.<br />

thrust control computer AFCS computer providing<br />

control of engine N 1 and thrust, computation of engine<br />

limit parameters, and autothrottle.<br />

thrust cutoff See cutoff.<br />

thrust decay Gradual falloff in thrust of solid motor,<br />

usually a slow fall from peak to cutoff or burnout<br />

followed by rapid ** over 2 to 8 s and to zero after perhaps<br />

10–12 s.<br />

thrust-decay system Idle-area reset (turbofan).<br />

thrust deflector Various schemes for V/STOL or<br />

STOVL, see four-poster, switch-in deflector, vectored<br />

thrust, etc.<br />

thrust equivalent horsepower See thrust horsepower.<br />

thruster Small propulsor, normally any of many kinds<br />

of rocket, used for spacecraft attitude control or fine<br />

adjustment of velocity.<br />

thrust face Side of propeller blade corresponding to<br />

underside of aerofoil.<br />

thrust/frontal area Jet-engine thrust divided by engine’s<br />

nominal or published frontal area; fair criterion in early<br />

days of jet propulsion but today meaningless. Important<br />

699

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