MakarovSuites
English
EnglishDeutschРусскийУкраїнськаFrançaisEspañolItalianoPolski
Contact & licences

Engineering

Aerial rescue ladder

At night before a burning house a fire truck stands on its four outriggers and raises its turntable ladder to a window on the top floor. The four telescopic sections bend as a stepped cantilever whose closed-form deflection agrees with the unit-load integral, and the ladder is drawn bent by it, magnified. When a second person steps into the cage the tip drops by m g cos θ/k and overshoots, then sways at the first bending frequency sqrt(k/m_eff)/2π, dying away with the logarithmic decrement 2πζ; a gust sets it swaying too. Draw the outriggers in and the pads share the load ever more unevenly - at 1.5 m one lifts while the cage sways, at 1.2 m the truck would tip. The load chart gives the safe load against the reach, and the work of the loads is followed into the sway and the damping.

Aerial rescue ladder — Actual application image
Actual application image

What happens

A turntable ladder of four telescopic sections, each 6.8 m long, on a truck of 12 t with a 3.2 t turntable. The sections extend together, each protruding 0.6 to 5.8 m beyond the one below, so the ladder is 8.6 to 24.2 m long; their bending stiffnesses are 1.0·10^8, 5.5·10^7, 3.0·10^7 and 1.5·10^7 N·m² and their masses 1100, 800, 560 and 380 kg. Where sections overlap their stiffnesses and weights add: a stepped cantilever, clamped at the turntable. Its weight and the 180 kg cage with its load, resolved across the axis (cos θ), bend it; the deflection is integrated in closed form on every segment (the moment is a quadratic there) and agrees with the unit-load integral of M m/EI to 10^-12. The first bending mode is a Rayleigh oscillator of the tip: k from the deflection under a unit tip force, m_eff = cage + the weight per metre times the square of that shape, damping ratio 3 %. A person of 90 kg stepping in is a step load with a mass jump (momentum kept); a gust of 18 m/s pushes with a drag rising as sin² over 2 s. Implicit midpoint steps of 1 ms keep the ledger exact. The truck is a rigid chassis on four equal pad springs at 1.6 and −3.9 m along it and ±1.2 to ±2.4 m across: a pad that would pull lifts and three carry the load; with the resultant outside the pads the truck would tip. The loads at which a pad lifts, at which the truck tips, and the safe load (stabilising moment 1.5 times the overturning one, at most 270 kg) follow in closed form from the moments about the pads’ edges.

Try this

Watch the tip drop and sway when the second person steps in, and read the sway frequency against the closed form; add a gust; draw the outriggers in to 1.5 m and watch a pad lift during the sway, to 1.2 m and the truck would tip; extend the ladder fully and lower it to see the safe load fall with the reach.

The model and its limits

A linear beam in its plane only, without axial shortening, twist or sideways sway; one bending mode; a rigid chassis on equal pad springs; the cage at the tip, statics on the undeflected geometry. Loads and limits are those of this idealized truck, not an operating table.

Equations used in the module
Equations
EI(s)·d²w/ds² = M(s) = F·(L − s) + Σ q_j·∫(t − s) dt,  δ = ∫ M·(L − s)/EI ds
k = 1/w_1(L),  m_eff = m_c + ∫ μ·(w_1/w_1(L))² ds,  f = √(k/m_eff)/2π
m_eff·a + c·v + k·y = k·δ_s(t),  c = 2ζ·√(k·m_eff),  Λ = 2πζ/√(1 − ζ²)
R_i = W/4 + B·(x_i − x_c) + C·z_i,  P_tip = Σ m_j·a_j/(−a_c),  P_safe = (M_s/1.5 − M_o)/(−a_c)

Related experiments

Back to catalogue
Lifeboat launching — Actual application image

Engineering

Lifeboat launching

Release an enclosed free-fall lifeboat from the stern ramp of a supply vessel at dusk. It slides down the skids with Coulomb friction and leaves them at exactly sqrt(2 g L (sin theta - mu cos theta)), tips nose-down over the lip until the contact lets go, falls along a parabola and meets the dark sea where the closed form says, at the speed energy gives. It dives two metres deep, the buoyancy of its hull - nearly five times its weight - turns it up, it surfaces and the propeller drives it away while the pitch and heave die out. Read the loads at the bow, midship and stern seats: a higher drop enters faster and loads harder, a steeper ramp enters better aligned, trim by the stern lowers the lip. Every joule is followed into friction, drag, slamming and the water.

Deployable bridge — Actual application image

Engineering

Deployable bridge

At first light an olive-green launcher stands at the edge of a foggy river gorge with an 18 m steel scissor bridge folded on its hull. One hydraulic drive lifts it on the launch arm, raises it through the vertical and opens the scissor until the far end glides level over the water, x = −2a cos φ, and lands on the far bank; the hydraulic work is followed into the bridge’s height, its motion and the friction to the joule. Raise the stabiliser blade and the outstretched 9 t bridge outweighs the launcher about its front tracks: it would tip at 152.7°, where the closed form puts it; above 11.8 t the relief valve cannot lift the bridge at all. Then a 24 t truck comes out of the fog and crosses: the span sags a further 45 mm, drawn magnified, its stress and safety against yield follow the influence lines, and without damping the ringing it leaves behind follows the closed form - at 36 km/h the two axles all but cancel.

Thermal soaring — Actual application image

Engineering

Thermal soaring

Soar a white 15 m sailplane over a broad alpine valley on a strong summer afternoon: circle in a thermal under its cumulus, climb toward cloud base, then glide to the next cloud and climb again. The speed polar a V³ + b/V gives the minimum-sink and best-glide speeds and a best glide of 40; in a Gaussian thermal the bank that climbs best is a closed form through Lambert’s W - too shallow and the circle lies outside the core, too steep and the circling sink eats the lift. Between thermals MacCready’s speed to fly is the tangent from the expected climb to the polar, and the measured cross-country speed follows V c/(c + w_s). Switch the centring off and an off-centre circle sinks out of the lift; weaken the thermal and the sailplane lands in a field. Every joule of height and speed is followed from the rising air into the drag.