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Pratt & Whitney Canada JT15D

 

PW-JT15D

 

The Pratt & Whitney Canada JT15D is a small turbofan engine built by Pratt & Whitney Canada and first run in 1966. It was introduced in 1971 at 2,200 lbf (9,800 N) thrust, and has since undergone a series of upgrades to just over 3,000 lbf (13 kN) thrust in the latest versions. It is the primary powerplant for a wide variety of smaller jet aircraft, notably business jets. Over 6,000 JT15D's have been delivered since the 1970s, with over 30 million hours of operation.

The JT15D is rare among modern turbofans in that it uses a centrifugal compressor as its main high-pressure system. This was a common feature of early jet engines, but was quickly replaced by axial compressors in most roles due to its large frontal size. In the turbofan role most of the jet thrust is generated by the cold air blown past the engine, and the internal "jet" portion is quite small. In this role the high single-stage compression of the centrifugal design has advantages, and the main reason most small turbofans don't use them is that they are often developments of previous turbojet designs.

In the JT15D the fan blows about 70% of the air into the bypass duct, producing most of the overall thrust. On JT15D-4 models and above there is a small "booster" axial stage just behind the fan which is running at the same speed as the fan and directing the remaining 30% of the airflow into the engine core. This air is further compressed by the centrifugal stage, and burned in a reverse-flow annular combustor. The hot gases flow through a "high-pressure" turbine that drives the centrifugal stage, and then two more turbines driving the fan and booster.

The first model, the JT15D-1, was introduced to power the Cessna Citation I, then known as the Fanjet 500. Deliveries started in 1972, and eventually on 1,417 -1s were delivered. The JT15D-4 was introduced the next year, improving thrust to 2,500 lbf (11,000 N). The -4 was the primary engine for the Cessna Citation II, and went on to find use on the Mitsubishi Diamond 1A, Aerospatiale Corvette and SIAI Marchetti S.211. Eventually 2,195 engines of the -4 series were delivered.

The next major model was the JT15D-5, certified in 1983. The first versions delivered 2,900 lbf (13,000 N) and were used on the Beechjet 400A and Cessna T-47A. Several minor versions were introduced, the -5A for the Cessna Citation V, while the -5B powered the Beechcraft T-1A Jayhawk, the -5C the DASA Ranger 2000 and S-211A.

A more major upgrade was the JT15D-5D, which was certified in 1993. It increased thrust again, this time to 3,045 lbf (13,540 N). The -5D is used on the Cessna UC-35A and Cessna Citation Ultra.

 

The D-5 of 2965 lb take-off rating was produced for the Diamond II/Beech 400A. The JT15D-5R is a later development, identical in all respects to the -5 except for changes to the fuel and oil systems associated with the elimination of the Fuel System Icing Inhibitor (FSII) additive.

 

Applications:
Aérospatiale Corvette
Alenia Aermacchi M-311
Beechcraft Beechjet 400
Cessna Citation I
Cessna Citation II
Cessna Citation V/Ultra
Hawker 400
Mitsubishi MU-300 Diamond
Raytheon T-1 Jayhawk
Rockwell Ranger 2000
SIAI Marchetti S.211/Aermacchi S-211
Sport Jet II
Boeing Bird of Prey

 

Specifications:

 

JT15D-1
Takeoff thrust: 9,8 kN / 2200 lb
Continuous thrust: 9,3 kN
Length: 1506 mm
Diameter: 691 mm
Dry weight: 223,5 kg
Bypass ratio: 3,3
 
JT15D-4
Takeoff thrust: 11,12 kN / 2500 lb
Continuous thrust: 10,56 kN
Length: 1600 mm
Diameter: 686 mm
Dry weight: 253 kg
Bypass ratio: 2,6

 

JT15D-4C
Takeoff thrust: 11,12 kN
Continuous thrust: 10,56 kN
Length: 1600 mm
Diameter: 686 mm
Dry weight: 261 kg
Bypass ratio: 2,6

 

JT15D-5
Takeoff thrust: 12,92 kN
Length: 1600 mm
Dry weight: 287 kg
Bypass ratio: 2

 

JT15D-5A
Takeoff thrust: 12,92 kN
Length: 1600 mm
Dry weight: 287 kg
Bypass ratio: 2

 

JT15D-5B
Takeoff thrust: 12,92 kN
Length: 1600 mm
Dry weight: 292 kg
Bypass ratio: 2

 

JT15D-5C
Takeoff thrust: 14,21 kN
Length: 1600 mm
Dry weight: 302 kg
Bypass ratio: 2

 

JT15D-5D
Type: Turbofan
Length: 60.5 in / 1531 mm
Diameter: 27 inches
Dry weight: 630 lb / 292,6 kg
Compressor: Axial flow LP, centrifugal flow HP
Fan Diameter: 520 mm
Bypass ratio: 3,3
Maximum thrust: 3,050 pounds
Takeoff thrust: 13,56 kN
Specific fuel consumption: 0.562 at max, 0.552 at cruise (typ)
Thrust-to-weight ratio: 4.58/1 (approximation)

 

JT15D-5F
Takeoff thrust: 12,92 kN
Length: 1600 mm
Dry weight: 288 kg
Bypass ratio: 2

 

 

 

 

 

 


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