AIRPORT PAVEMENT DESIGN
AIRPORT PAVEMENT DESIGN
COURSE NOTES
COURSE NOTES
AIRPORT PAVEMENT DESIGN:
AIRPORT PAVEMENT DESIGN:
COURSE NOTES
COURSE NOTES
1.
1. Pavement design conceptsPavement design concepts 2.
2. Copies of transparenciesCopies of transparencies 3.
3. Copies of additional informationCopies of additional information A.
A. Typical layoutTypical layout B.
B. Aircraft characteristicsAircraft characteristics C.
C. FAA design curves and adjustments forFAA design curves and adjustments for flexible and rigid
flexible and rigid
D.
D. British procedureBritish procedure E.
E. Typical concrete slab layoutTypical concrete slab layout F.
F. Typical pavement structures for SouthTypical pavement structures for South African airports
African airports
G.
G. ReferencesReferences H.
AIRPORT PAVEMENT DESIGN:
AIRPORT PAVEMENT DESIGN:
CONTENTS
CONTENTS
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Types of facilities
Types of facilities
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Types of airports
Types of airports
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Aircraft characteristics
Aircraft characteristics
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Design loading
Design loading
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Specific concepts
Specific concepts
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Design procedures
Design procedures
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TYPES OF FACILITIES
TYPES OF FACILITIES
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Runway
Runway
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Taxiway
Taxiway
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Apron
Apron
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TYPES OF AIRPORTS
TYPES OF AIRPORTS
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International:International: BOEING 767 TO 747 BOEING 767 TO 747 CONCORDE CONCORDE AIRBUS 300 & 320 AIRBUS 300 & 320 DC DC -- 10, 1110, 11•
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Regional:Regional: BOEING 737 TO 707 BOEING 737 TO 707 AIRBUS AIRBUS BA 146 BA 146 DASH 7 DASH 7 F27, F28 F27, F28•
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Local:Local: CESSNA CESSNA DC DC -- 33 BEECHCRAFT BEECHCRAFT PIPER PIPERAIRCRAFT
AIRCRAFT
CHARACTERISTICS
CHARACTERISTICS
TYPE
TYPE TOTAL LOADTOTAL LOAD (
(kNkN))
NO OF WHEELS
NO OF WHEELS LOAD/WHEELLOAD/WHEEL ( (kNkN)) PRESSURE PRESSURE ( (MPaMPa)) ACN / @ 10 F ACN / @ 10 F CONCORDE
CONCORDE 18151815 8 8 --Dual tandemDual tandem 218218 1.261.26 7272 B767
B767 --300300 1 5661 566 8 8 --Dual tandemDual tandem 186186 1.211.21 4646 B747
B747 --400400 3 7963 796 16 16 --Dual tandemDual tandem 223223 1.381.38 4545 V737
V737 --300300 603603 4 4 --DualDual 138138 1.141.14 3131 B727
B727 --200 Advanced200 Advanced 934934 4 4 --DualDual 215215 1.151.15 4646 A300
A300 --C4C4 1 6291 629 8 8 --Dual tandemDual tandem 189189 1.241.24 5151 A310
A310 --300300 1 5101 510 8 8 --Dual tandemDual tandem 178178 1.401.40 4646 F27 Mk 400
F27 Mk 400 194194 4 4 --DualDual 4646 0.540.54 1010 BAe146
BAe146 --200200 400400 4 4 --DualDual 9494 1.141.14 2121 DASH 7
DESIGN LOADING
DESIGN LOADING
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Wheel load
Wheel load
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Tyre
Tyre
pressure
pressure
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Wander:
Wander:
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runwayrunway•
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taxiwaytaxiway•
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Forces:
Forces:
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verticalvertical•
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horizontalhorizontal•
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Example
Example
SPECIFIC CONCEPTS
SPECIFIC CONCEPTS
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Load classification number (LCN)Load classification number (LCN)–
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Based on plate loadingBased on plate loading–
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Calculated from Benkelman Beam /FWDCalculated from Benkelman Beam /FWD–
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For flexible or rigidFor flexible or rigid•
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Aircraft classification number (ACN) and Pavement Aircraft classification number (ACN) and Pavement classification number (PCN)classification number (PCN)
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Include: pavement typeInclude: pavement type subgradesubgrade strengthstrength tyre
tyre pressurepressure
method of calculation method of calculation
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Used since 1983Used since 1983–
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Single wheel load (kg/500) with same performance as Single wheel load (kg/500) with same performance as groupgroup
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PCN
PCN
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DESCRIPTIONDESCRIPTION–
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PCN numberPCN number–
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Type of pavementType of pavement R = rigidR = rigid
F = flexible
F = flexible
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Pavement Pavement subgradesubgrade categorycategory A = High (CBR = 15) A = High (CBR = 15) B = Medium (CBR = 10) B = Medium (CBR = 10) C = Low (CBR = 6) C = Low (CBR = 6) D = Ultra low (CBR = 3) D = Ultra low (CBR = 3)PCN
PCN
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Maximum Maximum tyretyre pressurepressure W = high (no limit)W = high (no limit)
X = medium (< 1 500
X = medium (< 1 500 kPakPa))
Z = very low (< 500
Z = very low (< 500 kPakPa))
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Evaluation methodEvaluation method T = technicalT = technical
U = experience
PCN (CONT)
PCN (CONT)
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Example: 30/F/C/W/TExample: 30/F/C/W/T•
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CalculationCalculation–
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Rigid Max Flexural stress = 2.75 Rigid Max Flexural stress = 2.75 MpaMpa Ec Ec = 27.6 = 27.6 GpaGpa Poisson = 0.15 Poisson = 0.15 p = 1.25 p = 1.25 MpaMpa Westergaard Westergaard–
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Flexible: 10 000 repetitionsFlexible: 10 000 repetitions p = 1.25p = 1.25 MpaMpa CBR or
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ICAOICAO–
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CanadianCanadian–
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FrenchFrench–
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UKUK–
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FAA (USA)FAA (USA)•
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BritishBritish•
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FAAFAA•
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US CORPSUS CORPS–
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CBRCBR•
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Asphalt InstituteAsphalt InstituteDESIGN PROCEDURES
DESIGN PROCEDURES
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PCA
PCA
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Graphs
Graphs
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AIRPAV (Westergaard)
AIRPAV (Westergaard)
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Mechanistic
Mechanistic
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South African
South African
DESIGN PROCEDURES (CONT)
DESIGN PROCEDURES (CONT)
FAA METHOD
FAA METHOD
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Design aircraft Design aircraft -- largest thicknesslargest thickness•
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Convert all aircraft to designConvert all aircraft to design•
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Adjust annual departuresAdjust annual departures•
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SubgradeSubgrade -- CBR, kCBR, k•
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Critical on nonCritical on non--critical areascritical areas•
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Wide bodies (> 45 500 kg): Wide bodies (> 45 500 kg): stabilisestabilise base and base and subbasesubbase
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Graphs (departures, gross mass, CBR)Graphs (departures, gross mass, CBR)–
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Total thicknessTotal thickness–
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• FlexibleFlexible
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– SubbaseSubbase: CBR > 35, any type: CBR > 35, any type –
– Base: CBR > 100, any typeBase: CBR > 100, any type –
– Surfacing: 100 mm ACSurfacing: 100 mm AC
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• RigidRigid
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– WastergaardWastergaard, edge loading, edge loading –
– SubbaseSubbase, any type, any type –
– Panel sizePanel size
FAA METHOD
FAA METHOD
(cont)
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Design ACN: highest ACNDesign ACN: highest ACN mixed trafficmixed traffic
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Design life: 20 Design life: 20 -- 30 years30 years•
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Frequency: low Frequency: low -- 10 000 over life10 000 over life mediummedium -- 10 00010 000 high
high-- 250 000250 000
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Traffic patternsTraffic patterns•
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CoveragesCoverages and Pass and Pass -- to to -- Coverage ratioCoverage ratioBRITISH METHOD
BRITISH METHOD
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Design curves (ACN, CBR, Traffic, PQC)Design curves (ACN, CBR, Traffic, PQC)•
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FlexibleFlexible–
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Surfacing: 100 mm or 0.33 x DLCSurfacing: 100 mm or 0.33 x DLC–
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Base: bound (DLC, AC), Base: bound (DLC, AC), stabilisedstabilised, granular , granular (CBR > 30%)(CBR > 30%)
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SubbaseSubbase: granular (CBR > 30%): granular (CBR > 30%)•
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RigidRigid–
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Failure: 50% crackingFailure: 50% cracking–
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SubbaseSubbase: DLC, : DLC, stabilisedstabilised or granularor granular–
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Temperature warping (+ 10%)Temperature warping (+ 10%)–
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Joints/slab size (type, aggregate)Joints/slab size (type, aggregate)BRITISH METHOD
BRITISH METHOD
EXAMPLES
EXAMPLES
EXAMPLE
EXAMPLE
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Aircraft:Aircraft: B747 -B747 - 200 F (380 000 kg)200 F (380 000 kg) CBR = 10 CBR = 10 ACN = 58 ACN = 58 100 000 total rep 100 000 total rep 4 000 rep per year 4 000 rep per yearLAYER BRITISH FAA SA 1 SA 2 AC Surfacing 100 100 75 75 Base 500 BBM 250 Stab 100 G 200 WM
Subbase - 175 Stab 450 C 300 G Total 600 525 625 575