1.7.21 · Physics › Thermodynamics
Carnot cycle sabse zyada efficient heat engine hai jo do temperatures ke beech kaam karta hai. Yeh ek idealized, poori tarah reversible cycle hai. Iski efficiency sirf do reservoir temperatures par depend karti hai — working substance par nahi, pressures par nahi, kisi aur cheez par nahi. Yeh ek akela fact 2nd law aur absolute temperature ka beej hai.
Ek reversible cycle jo chaar strokes se bana hota hai, ek ideal gas use karta hai jo hot reservoir T H aur cold reservoir T C ke beech kaam karta hai:
Isothermal expansion at T H (heat Q H absorb karo)
Adiabatic expansion (T H → T C , koi heat exchange nahi)
Isothermal compression at T C (heat Q C reject karo)
Adiabatic compression (T C → T H , wapas shuru pe)
Intuition Exactly yeh chaar steps kyun?
Heat transfer ke time isothermal kyun? Heat ko reversibly transfer karne ke liye, gas ka temperature reservoir ke temperature ke (essentially) barabar hona chahiye — warna heat ek finite temperature gap cross karti hai, jo irreversible hota hai aur potential work waste karta hai.
Dono temperatures ke beech adiabatic kyun? Gas ko T H se T C tak bina kisi intermediate temperature ke reservoir ko touch kiye le jaana hai (woh phir se irreversible hota). Use insulate karo aur use apna temperature khud change karne ke liye work karne/absorb karne do.
Toh: heat exchange = isothermal; temperature change = adiabatic. Yeh combination ek hi tarika hai har step ko reversible rakhne ka.
Hum 1 mole ideal gas use karte hain: P V = R T , internal energy U = U ( T ) sirf.
General efficiency definition. Ek poore cycle mein Δ U = 0 , toh first law se net heat, net work ke barabar hoti hai:
η = Q H W net = Q H Q H − Q C = 1 − Q H Q C
Ab hum Q H aur Q C compute karte hain.
Kyunki T constant hai, Δ U = 0 , toh Q H = W 1 → 2 .
W 1 → 2 = ∫ V 1 V 2 P d V = ∫ V 1 V 2 V R T H d V = R T H ln V 1 V 2
Yeh step kyun? Ideal gas law se P = R T H / V use kiya aur integrate kiya; log isliye aaya kyunki ∫ d V / V = ln V .
Q H = R T H ln V 1 V 2
Same logic, heat reject hoti hai (gas compress hoti hai, V 4 < V 3 ):
Q C = − W 3 → 4 = R T C ln V 4 V 3
Sign kyun? Hum Q C ko heat released (positive number) define karte hain, toh magnitude lete hain. Kyunki V 3 > V 4 , ln ( V 3 / V 4 ) > 0 . ✓
Ek ideal gas ki reversible adiabatic ke liye, T V γ − 1 = const .
Step 2 (T H , V 2 → T C , V 3 ) aur step 4 (T C , V 4 → T H , V 1 ) par apply karo:
T H V 2 γ − 1 = T C V 3 γ − 1 , T H V 1 γ − 1 = T C V 4 γ − 1
Dono equations divide karo:
V 1 γ − 1 V 2 γ − 1 = V 4 γ − 1 V 3 γ − 1 ⇒ V 1 V 2 = V 4 V 3
Yeh key trick kyun hai? Q H aur Q C mein aane wale dono volume ratios equal hain! Yahi wajah hai ki log terms cancel ho jaati hain.
Q H Q C = R T H l n ( V 2 / V 1 ) R T C l n ( V 3 / V 4 ) = T H T C ⋅ = 1 ln ( V 2 / V 1 ) ln ( V 3 / V 4 ) = T H T C
Worked example Example 1 — Steam-to-river engine
T H = 600 K , T C = 300 K . η nikalo.
η = 1 − 600 300 = 0.5 = 50%
Yeh step kyun? Direct plug-in; temperatures pehle se kelvin mein hain. Absorb ki gayi heat ka aadha hissa work ban jaata hai — baaki cold reservoir mein dump karna hi padta hai .
Worked example Example 2 — Heat rejected
Same engine Q H = 2000 J absorb karta hai. W aur Q C nikalo.
W = η Q H = 0.5 × 2000 = 1000 J
Q C = Q H − W = 1000 J (check: Q C = Q H T C / T H = 2000 ⋅ 2 1 = 1000 ✓ )
Dono checks kyun? Confirm karta hai ki first law aur reversible relation dono agree karte hain.
Worked example Example 3 — Forecast-then-verify
Forecast: Agar T H ko 600 K se 900 K tak raise karo (T C = 300 rakhte hue), toh kya η zyada badhega ya T C ko 0 tak drop karne se?
Verify: T H raise karna: η = 1 − 300/900 = 0.667 . T C → 0 drop karna: η = 1 − 0 = 1 . Toh in values ke paas T C kam karna zyada powerful hai har degree ke liye, lekin T C = 0 achieve karna impossible hai (3rd law). Isliye real engines T H raise karne ki koshish karte hain.
Common mistake Kelvin ki jagah Celsius use karna
Kyun sahi lagta hai: Tum zyattar temperature differences calculate karte ho, jahan °C aur K same number dete hain. Trap: efficiency ek ratio T C / T H use karti hai, aur ratios zero point ke saath bilkul badal jaate hain. Fix: T C / T H banane se pehle hamesha kelvin mein convert karo.
Common mistake Yeh sochna ki sirf hot source
η → 1 kar deta hai
Kyun sahi lagta hai: bada T H sach mein η badhata hai. Trap: η = 1 − T C / T H < 1 hamesha, kyunki T C > 0 . Tum cycle mein kabhi saari heat ko work mein convert nahi kar sakte. Fix: 2nd law yaad rakho — kuch heat reject karni hi padti hai.
Common mistake Volume ratios cancel hona bhool jaana
Kyun sahi lagta hai: chaar volumes independent lagte hain. Trap: adiabatic relations force karte hain V 2 / V 1 = V 3 / V 4 . Yeh skip karo toh Q C / Q H ko T C / T H tak reduce nahi kar sakte. Fix: hamesha dono adiabatic conditions ko pair karo aur divide karo.
Common mistake Yeh claim karna ki koi bhi engine
T H , T C ke beech Carnot ko beat kar sakta hai
Kyun sahi lagta hai: clever engineering unbounded lagti hai. Trap: Carnot's theorem — do reservoirs ke beech koi bhi engine reversible engine se zyada efficient nahi ho sakta. Use beat karna tumhe second kind ki perpetual motion machine banane dega. Fix: η any ≤ 1 − T C / T H .
Recall Feynman: ek 12-saal ke bacche ko explain karo
Socho ek bouncy gas ek cylinder mein hai. Tum use ek hot stove se touch karne do, aur woh dhire-dhire piston push karti hai hot rehte hue (woh heat grab karti hai aur work karti hai). Phir tum use ek blanket mein wrap karte ho taaki koi heat andar-bahar na jaye, aur woh push karte-karte thandi ho jaati hai. Ab tum use ek cold ice block ke saath press karte ho, use dheere squeeze karte ho taaki woh bacha khucha heat dump kar sake. Aakhir mein tum use phir blanket karte ho aur squeeze karke start pe le aate ho, use garam karte hue. Ghoomta-ghoomta yeh heat ko useful pushing mein convert karta hai. Pakad: jitna thanda tumhara ice aur jitna garam tumhara stove, utna zyada useful work milta hai — lekin tum kabhi 100% nahi pa sakte, kyunki kuch warmth hamesha ice mein jaani hi padti hai.
Mnemonic Cycle ka order yaad rakho
"I Adam Is Adam" — I sothermal hot, A diabatic down, I sothermal cold, A diabatic up.
Efficiency ke liye: "One minus Cold-over-Hot" → 1 − T C / T H (Cold upar isliye kyunki woh heat hai jo tum lose karte ho).
Carnot cycle ke chaar steps order mein kya hain? Isothermal expansion (at T H ), adiabatic expansion, isothermal compression (at T C ), adiabatic compression.
Heat transfer steps isothermal kyun hone chahiye? Unhe reversible rakhne ke liye — gas reservoir ke temperature par rehti hai toh heat koi finite temperature gap cross nahi karti.
Carnot efficiency formula kya hai? η = 1 − T C / T H , temperatures kelvin mein.
Step 1 (isothermal at T H ) mein kitni heat absorb hoti hai? Q H = R T H ln ( V 2 / V 1 ) , kyunki Δ U = 0 toh Q = W .
Adiabats volumes ke beech kya relation force karte hain? V 2 / V 1 = V 3 / V 4 , dono adiabatics par T V γ − 1 = const se.
Efficiency working substance par kyun depend nahi karti? Volume-ratio logs cancel ho jaate hain, sirf temperature ratio T C / T H bachta hai.
Heats ko link karne wali reversible identity kya hai? Q H / T H = Q C / T C , yaani ∮ d Q r e v / T = 0 — entropy ka aadhar.
Carnot's theorem bolo. Do reservoirs ke beech kaam karne wala koi bhi engine, unhi reservoirs ke beech ek reversible (Carnot) engine se zyada efficient nahi ho sakta.
η = 1 kyun nahi ho sakta?Iske liye T C = 0 K chahiye hoga (pahuncha nahi ja sakta, 3rd law); kuch heat hamesha reject karni hi padti hai (2nd law).
Common kelvin mistake kya hai? T C / T H mein Celsius use karna — ratios zero point par depend karte hain, toh kelvin use karna zaroori hai.
Isothermal at reservoir T