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AIRPORT PAVEMENT DESIGN

AIRPORT PAVEMENT DESIGN

COURSE NOTES

COURSE NOTES

(2)

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.

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AIRPORT PAVEMENT DESIGN:

AIRPORT PAVEMENT DESIGN:

CONTENTS

CONTENTS

Types of facilities

Types of facilities

Types of airports

Types of airports

Aircraft characteristics

Aircraft characteristics

Design loading

Design loading

Specific concepts

Specific concepts

Design procedures

Design procedures

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TYPES OF FACILITIES

TYPES OF FACILITIES

Runway

Runway

Taxiway

Taxiway

Apron

Apron

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TYPES OF AIRPORTS

TYPES OF AIRPORTS

International:International: BOEING 767 TO 747 BOEING 767 TO 747 CONCORDE CONCORDE AIRBUS 300 & 320 AIRBUS 300 & 320 DC DC -- 10, 1110, 11

Regional:Regional: BOEING 737 TO 707 BOEING 737 TO 707 AIRBUS AIRBUS BA 146 BA 146 DASH 7 DASH 7 F27, F28 F27, F28

Local:Local: CESSNA CESSNA DC DC -- 33 BEECHCRAFT BEECHCRAFT PIPER PIPER

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AIRCRAFT

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

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DESIGN LOADING

DESIGN LOADING

Wheel load

Wheel load

Tyre

Tyre

pressure

pressure

Wander:

Wander:

runwayrunway

taxiwaytaxiway

Forces:

Forces:

verticalvertical

horizontalhorizontal

Example

Example

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SPECIFIC CONCEPTS

SPECIFIC CONCEPTS

Load classification number (LCN)Load classification number (LCN)

Based on plate loadingBased on plate loading

Calculated from Benkelman Beam /FWDCalculated from Benkelman Beam /FWD

For flexible or rigidFor flexible or rigid

Aircraft classification number (ACN) and Pavement Aircraft classification number (ACN) and Pavement classification number (PCN)

classification number (PCN)

Include: pavement typeInclude: pavement type subgrade

subgrade strengthstrength tyre

tyre pressurepressure

method of calculation method of calculation

Used since 1983Used since 1983

Single wheel load (kg/500) with same performance as Single wheel load (kg/500) with same performance as group

group

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PCN

PCN

DESCRIPTIONDESCRIPTION

PCN numberPCN number

Type of pavementType of pavement R = rigid

R = rigid

F = flexible

F = flexible

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)

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PCN

PCN

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))

Evaluation methodEvaluation method T = technical

T = technical

U = experience

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PCN (CONT)

PCN (CONT)

Example: 30/F/C/W/TExample: 30/F/C/W/T

CalculationCalculation

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

Flexible: 10 000 repetitionsFlexible: 10 000 repetitions p = 1.25

p = 1.25 MpaMpa CBR or

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ICAOICAO

CanadianCanadian

FrenchFrench

UKUK

FAA (USA)FAA (USA)

BritishBritish

FAAFAA

US CORPSUS CORPS

CBRCBR

Asphalt InstituteAsphalt Institute

DESIGN PROCEDURES

DESIGN PROCEDURES

(13)

PCA

PCA

Graphs

Graphs

AIRPAV (Westergaard)

AIRPAV (Westergaard)

Mechanistic

Mechanistic

South African

South African

DESIGN PROCEDURES (CONT)

DESIGN PROCEDURES (CONT)

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FAA METHOD

FAA METHOD

Design aircraft Design aircraft -- largest thicknesslargest thickness

Convert all aircraft to designConvert all aircraft to design

Adjust annual departuresAdjust annual departures

SubgradeSubgrade -- CBR, kCBR, k

Critical on nonCritical on non--critical areascritical areas

Wide bodies (> 45 500 kg): Wide bodies (> 45 500 kg): stabilisestabilise base and base and subbase

subbase

Graphs (departures, gross mass, CBR)Graphs (departures, gross mass, CBR)

Total thicknessTotal thickness

(15)

FlexibleFlexible

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

RigidRigid

WastergaardWastergaard, edge loading, edge loading

SubbaseSubbase, any type, any type

Panel sizePanel size

FAA METHOD

FAA METHOD

(cont)

(16)

Design ACN: highest ACNDesign ACN: highest ACN mixed traffic

mixed traffic

Design life: 20 Design life: 20 -- 30 years30 years

Frequency: low Frequency: low -- 10 000 over life10 000 over life medium

medium -- 10 00010 000 high

high-- 250 000250 000

Traffic patternsTraffic patterns

CoveragesCoverages and Pass and Pass -- to to -- Coverage ratioCoverage ratio

BRITISH METHOD

BRITISH METHOD

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Design curves (ACN, CBR, Traffic, PQC)Design curves (ACN, CBR, Traffic, PQC)

FlexibleFlexible

Surfacing: 100 mm or 0.33 x DLCSurfacing: 100 mm or 0.33 x DLC

Base: bound (DLC, AC), Base: bound (DLC, AC), stabilisedstabilised, granular , granular (CBR > 30%)

(CBR > 30%)

SubbaseSubbase: granular (CBR > 30%): granular (CBR > 30%)

RigidRigid

Failure: 50% crackingFailure: 50% cracking

SubbaseSubbase: DLC, : DLC, stabilisedstabilised or granularor granular

Temperature warping (+ 10%)Temperature warping (+ 10%)

Joints/slab size (type, aggregate)Joints/slab size (type, aggregate)

BRITISH METHOD

BRITISH METHOD

(18)

EXAMPLES

EXAMPLES

(19)

EXAMPLE

EXAMPLE

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 year

LAYER 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

References

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