high tire pressure and temperature effects on hot mix asphalt concrete permanent deformation using...
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HIGH TIRE PRESSURE AND TEMPERATURE EFFECTS ON HOT MIX ASPHALT CONCRETE PERMANENT DEFORMATION
USING CUSTOMIZED ASPHALT PAVEMENT ANALYZER
April 22, 2010
Injun Song, Ph.D.
SRA International, Inc.
2010 FAA WORLDWIDE AIRPORT TECHNOLOGY TRANSFER CONFERENCE
ATLANTIC CITY, NEW JERSEY, USA
AUTHORS
Injun Song, Ph.D.
SRA International, Inc.
Phone: (609) 601-6800; Fax: (609) [email protected]
Navneet Garg, Ph.D.
FAA William J. Hughes Technical Center
Phone: (609) 485-4483; Fax: (609) [email protected]
OBJECTIVES
• High tire pressure / temperature effects on Hot Mix Asphalt (HMA) permanent deformation using Asphalt Pavement Analyzer (APA).
• Conducting research into the design of HMA to resist damage from high pressure aircraft tires. Test results will be compared with the FAA’s full scale test data.
ICAO ANNEX 14
• Annex 14 - Aerodromes. Volume I - Aerodrome Design and Operations.
2.6 Strength of pavements
2.6.6 Information on pavement type for ACN-PCN…
a) Pavement type for ACN-PCN determination:…
b) Subgrade strength category:…
c) Maximum allowable tire pressure category:
Code• no pressure limit W• pressure limited to 1.50 MPa X• pressure limited to 1.00 MPa Y• pressure limited to 0.50 MPa Z
FAA CUSTOMIZED APA
• The 100 psi (0.69 MPa) and 104°F (40°C) are adopted for APA test conditions. Simulating highway traffic (load) and environment conditions.
• FAA customized APA that is capable of applying tire pressures representative of a heavy commercial aircraft (250 psi +).
FAA CUSTOMIZED APA
APA TEST CONDITIONS
• Three test conditions are selected to simulate effects from high tire pressures and high pavement temperatures in airport pavements.
• All tests conducted in dry condition. • Pneumatic cylinders applied 100 lbf load at 60 Hz
frequency.• Contact Pressure, psi / Temperature, °F
– 100 / 140 (= 0.69 MPa / 60°C) – 250 / 70 (= 1.72 MPa / 21°C) – 250 / 140 (= 1.72 MPa / 60°C)
TEST SPECIMENS
• High Tire Pressure (HTP) pavement test area at the FAA’s National Airport Pavement Test Facility (NAPTF).
• 6-inch diameter by 3-inch high cylindrical samples are used for APA testing after cored from HTP area. The top 3-inch (76 mm) from 6-inch high core was used for the testing.
• FAA’s P401 specification based on Marshall mix design procedure was used for the HMA mix design. PG 64-22 is selected and used for the HTP test area construction.
P-401 GRADATION
0
10
20
30
40
50
60
70
80
90
100
Sieve Size, mm
Perc
en
t P
assin
g,
%
Gradation
Max. Density
1912.5 4.752.31.180.075
DATA ANALYSIS
• Direct comparisons of rut depth, rut depth slope, and rut rate respectively.
• Adopted VESYS method (pavement structure) to predict permanent deformation for extended APA stroke numbers. Effects from high tire pressures and temperatures are relatively compared.
RUT DEPTH COMPARISONS
• Temperatures effects under high contact pressure of 250 psi (1.72 MPa): 70°F (21°C) and 140°F (60°C).
• Contact pressure effects under high test temperature of 140°F (60°C): 100 psi (0.69 MPa) and 250 psi (1.72 MPa).
• Manual rut depth measurements shows about ±0.25 mm differences from APA monitored rut depth.
TEMPERATURE EFFECTS ON HMA RUT DEPTH
0
1
2
3
4
5
6
7
8
9
10
0 1000 2000 3000 4000 5000 6000
Pass Number
Ru
t D
epth
, m
m
250psi@70F
250psi@140F
100psi@140F
CONTACT PRESSURE EFFECTS ON HMA RUT DEPTH
0
1
2
3
4
5
6
7
8
9
10
0 1000 2000 3000 4000 5000 6000
Pass Number
Ru
t D
epth
, m
m
100psi@140F
250psi@140F
250psi@70F
RUT SLOPE COMPARISONS
• Rut slope changes at different APA test conditions.
• Rut slope is computed by (rut depth) / (pass number).
• Significant effects by high contact pressure and temperatures.
RUT SLOPE CHANGES
at DIFFERENT APA TEST CONDITIONS
-0.002
0
0.002
0.004
0.006
0.008
0.01
0.012
0.014
0 1000 2000 3000 4000 5000 6000
Pass Number
Ru
t S
lop
e, m
m/c
ycle
100psi@140F
250psi@70F
250psi@140F
RUT RATE COMPARISONS(at Steady State)
Pressure, psi Temperature, °FRut Rate
(between 1500 and 5000 passes), mm/pass number
100 (0.69 MPa) 140 (60°C) 0.000475
250 (1.72 MPa) 70 (21°C) 0.000294
250 (1.72 MPa) 140 (60°C) 0.000622*
*The rut rate would be 0.000275 mm/pass with the secondary stage
RUTTING STAGES USING APA TEST DATA
y = 0.0003x + 7.4405
y = 0.0008x + 5.5027
0
1
2
3
4
5
6
7
8
9
10
0 1000 2000 3000 4000 5000 6000
Pass Number
Ru
t D
epth
, m
m
250psi@140F
SecondaryPrimary Tertiary
VESYS METHOD
• VESYS method (pavement structure) was adopted to predict permanent deformation for extended APA stroke numbers.
• Effects from high tire pressures and temperatures are relatively compared.
• System rutting formulation considering the pavement system as a whole structure including all the layers as shown in following equation
2
1
N
N
sys dNNURD sys
VESYS METHOD (continued)
• Permanent deformation was predicted for extended APA stroke numbers until 15000 passes.
• Assumed the sublayers are all metal plates (no permanent deformation during the APA testing) to simulate APA test conditions.
CONCLUSIONS
• FAA customized APA equipment is capable of applying tire pressure representative of a heavy commercial aircraft.
• APA tests at high tire pressures and temperatures were conducted and the acquired data was analyzed. These test results will be used to augment the full scale testing program at the NAPTF.
• Rut depth increased significantly with higher contact pressures and temperatures.
• The permanent deformation was more sensitive to temperature than to the contact pressure changes.