Q5
(a) With the help of P-θ (pressure-crank angle) diagram, compare the knock in SI and CI engines. Explain that "the factors which tend to prevent knock in SI engines in fact promote knock in CI engines". (10 marks) (b) Describe the phenomenon of 'blowby losses'. What are the factors that increase the blowby losses? What are the effects of increased blowby losses on the engine performance? (10 marks) (c) What are the advantages and disadvantages of supercritical pressure boilers as compared to that of subcritical boilers? Also, draw the Rankine cycle (T-s diagram) for a steam power plant employing supercritical boiler with single stage of reheating. (10 marks) (d) Derive the expression as given below for draught h in mm of water column being created by a chimney of height H metre: h = 353H[1/T_a - ((m_a + 1)/m_a)(1/T_g)] where m_a is mass of air supplied per kg of fuel, and T_a and T_g are ambient air and hot gas temperatures in Kelvin, respectively. (10 marks) (e) What is the chemical name of R134a? Is R134a an ecofriendly refrigerant? Clarify. (10 marks)
हिंदी में प्रश्न पढ़ें
(a) P-θ (दाब-क्रैंक कोण) आरेख की सहायता से एस० आइ० तथा सी० आइ० इंजनों में अपस्फोट (नॉक) की तुलना कीजिये। व्याख्या कीजिये कि "वे कारक, जो एस० आइ० इंजनों में अपस्फोट को रोकने में मदद करते हैं, वास्तव में सी० आइ० इंजनों में अपस्फोट को बढ़ावा देते हैं"। (10 अंक) (b) 'आधात क्षरण (ब्लोबाई लॉस)' की प्रक्रिया का वर्णन कीजिये। वे कौन-से कारक हैं, जो आधात क्षरण को बढ़ाते हैं? बढ़े हुए आधात क्षरण का इंजन के निष्पादन (परफॉर्मेंस) पर क्या प्रभाव पड़ता है? (10 अंक) (c) अवकांतिक (सबक्रिटिकल) बॉयलरों की तुलना में अतिकांतिक (सुपरक्रिटिकल) दाब बॉयलरों के क्या लाभ और हानियाँ हैं? साथ ही एक भाप विद्युत संयंत्र के लिये अतिकांतिक बॉयलर का प्रयोग करते हुए रैंकाइन चक्र (T-s आरेख) बनाइये, जिसमें एकल चरण (सिंगल स्टेज) पुनःस्थापन (रिहीटिंग) हो। (10 अंक) (d) H मीटर ऊँचाई की एक चिमनी द्वारा बनाये गये जल स्तंभ (वाटर कॉलम) के h mm प्रवात (ड्राफ्ट) के लिये नीचे दिये गये व्यंजक (एक्सप्रेशन) को व्युत्पन्न कीजिये: h = 353H[1/T_a - ((m_a + 1)/m_a)(1/T_g)] जहाँ m_a प्रति किलोग्राम ईंधन के लिए आपूर्ति की गई वायु का द्रव्यमान है तथा T_a और T_g क्रमशः वातावरण की वायु और गर्म गैस के कैल्विन में तापमान हैं। (10 अंक) (e) R134a का रासायनिक नाम क्या है? क्या R134a पर्यावरण का एक अनुकूल प्रशीतक द्रव्य (रेफ्रिजरेंट) है? स्पष्ट कीजिये। (10 अंक)
Directive word: Derive
This question asks you to derive. The directive word signals the depth of analysis expected, the structure of your answer, and the weight of evidence you must bring.
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How this answer will be evaluated
Approach
Begin with part (a) by drawing and comparing P-θ diagrams for SI and CI knock, then explain the inverse relationship of factors. For (b), describe blowby mechanism before listing factors and effects. Part (c) requires a balanced comparison of supercritical vs subcritical boilers followed by the T-s diagram with supercritical Rankine cycle and reheat. Part (d) demands rigorous step-by-step derivation of the chimney draught formula using ideal gas assumptions and density relationships. Conclude with (e) by stating R134a's chemical name and critically evaluating its environmental impact through GWP and ODP analysis. Allocate approximately 20% time each to parts (a), (b), (c), (d), and (e) respectively.
Key points expected
- Part (a): P-θ diagram showing SI knock as sharp pressure spike near TDC vs CI knock as gradual pressure rise; explanation of how high compression ratio, high inlet temperature, and early injection prevent SI knock but promote CI knock
- Part (b): Definition of blowby as gas leakage past piston rings into crankcase; factors including worn rings, high cylinder pressure, low viscosity oil, poor honing; effects on power loss, oil contamination, increased blowby gas handling requirement
- Part (c): Advantages of supercritical boilers (higher efficiency ~45%, no drum, reduced fuel consumption, lower emissions) vs disadvantages (high capital cost, materials stress, water treatment criticality); T-s diagram showing supercritical heating, expansion, reheat, condensation with correct slopes and critical point marked
- Part (d): Derivation starting from hydrostatic pressure balance, ideal gas law for air and flue gas, density substitution ρ = P/RT, pressure difference ΔP = H(ρ_a - ρ_g)g, conversion to mm of water using ρ_w, final algebraic manipulation to given formula
- Part (e): Chemical name 1,1,1,2-tetrafluoroethane (CF3CH2F); evaluation as eco-friendly regarding zero ODP but high GWP of 1430 over 100 years, comparison with R12 and R22, mention of Kigali Amendment implications for India
- Part (d) numerical: Correct handling of temperature in Kelvin, proper unit conversion from Pa to mm of water (1 mm H2O = 9.81 Pa), recognition that 353 = 353 K·mm/Pa or equivalent constant derivation
Evaluation rubric
| Dimension | Weight | Max marks | Excellent | Average | Poor |
|---|---|---|---|---|---|
| Concept correctness | 20% | 10 | For (a), correctly identifies SI knock as pre-ignition/auto-ignition of end gas vs CI knock as ignition delay causing rapid pressure rise; for (b), accurately describes blowby as unburnt mixture/combustion gas past piston rings; for (c), correctly distinguishes supercritical (P>22.1 MPa, no phase change) from subcritical with phase change; for (e), correctly identifies R134a as HFC with zero ODP but significant GWP | Basic understanding of knock differences but confuses cause-effect relationships; blowby described vaguely as 'leakage' without specifying path; supercritical advantages listed but without clear thermodynamic reasoning; R134a identified correctly but environmental assessment superficial | Confuses SI and CI knock mechanisms entirely; describes blowby as valve leakage or exhaust blowback; treats supercritical as simply 'high pressure' without critical point significance; wrong chemical name or claims R134a is CFC/HCFC |
| Numerical accuracy | 15% | 7.5 | Part (d) derivation shows correct substitution of ρ_a = P/(RT_a) and ρ_g = P/(RT_g) with proper algebraic manipulation; constant 353 correctly derived as 353000/(g×ρ_w) or equivalent showing unit consistency; temperature strictly in Kelvin throughout | Final formula correct but intermediate steps skip unit conversions or assume 353 without derivation; minor algebraic errors that cancel out; temperature conversion errors that are partially corrected | Numerical errors in density expressions; uses Celsius in gas law without conversion; wrong constant derivation leading to incorrect final formula; order of magnitude errors in mm of water calculation |
| Diagram quality | 20% | 10 | Part (a) P-θ diagram shows two distinct curves: SI with smooth rise then sharp spike (detonation) vs CI with delayed ignition then steep rise; both with correct TDC reference and crank angle scale; Part (c) T-s diagram clearly shows supercritical region above critical point (22.1 MPa, 374°C), continuous heating line, expansion, reheat at intermediate pressure, second expansion, condensation below critical pressure; critical point marked, constant pressure lines correctly sloped | Diagrams drawn but lack precision: P-θ diagrams show pressure rise but knock characteristics not clearly distinguished; T-s diagram shows reheat but supercritical region not clearly marked or treated as simply high-pressure subcritical | Diagrams missing or incorrect: P-θ shows pressure vs volume or wrong axes; T-s diagram shows standard Rankine cycle without supercritical features or omits reheat; no labels or values indicated |
| Step-by-step derivation | 25% | 12.5 | Part (d) shows complete derivation: (1) pressure at chimney base due to air column Hρ_a g, (2) pressure due to gas column Hρ_g g, (3) draught pressure ΔP = Hg(ρ_a - ρ_g), (4) ideal gas substitution ρ = PM/RT with M_air ≈ 29, M_gas ≈ 29-30, (5) simplification using m_a relationship, (6) conversion to mm water; each step logically connected with assumptions stated | Key steps present but skips some algebraic manipulation or assumes relationships without proof; jumps from pressure difference to final formula with 'hence' or 'it can be shown'; partial derivation with correct final result | No derivation shown, only final formula stated; or derivation with fundamental errors (e.g., treating gases as incompressible, ignoring temperature effect, wrong molecular weight assumption); circular reasoning |
| Practical interpretation | 20% | 10 | For (a), explains practical implications: SI engines need high octane fuel, spark timing retard, combustion chamber design; CI engines need cetane number, injection timing advance, pre-chamber design; for (b), links blowby to Indian context: BS-VI emission norms requiring positive crankcase ventilation (PCV) and oil consumption limits; for (c), cites Indian supercritical plants like NTPC Kudgi (2×800 MW) or Mundra UMPP; for (e), discusses India's phase-down schedule under Kigali Amendment, transition to R1234yf or natural refrigerants | Mentions practical applications but generic: 'knock is bad for engines', 'blowby causes pollution', 'supercritical saves fuel'; no specific Indian examples or current regulatory context for R134a | No practical interpretation; treats all parts as purely theoretical; or gives incorrect practical implications (e.g., claims SI and CI can use same anti-knock strategies, suggests blowby increases power) |
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