Alaska Aviation Museum - (unofficial)

Engines - Pratt & Whitney

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AAM - Pratt & Whitney Engines

1st
Run
Brand Name Model HP Weight Built
1925 P&W Wasp R-1340 450 to 600 930 34,966 Used on: Fairchild 71 - Black wood stand, NE corner Odom Hangar
1925 P&W Wasp R-1340 450 to 600 930 34,966 Used on: Noorduyn Norseman
1925 P&W Wasp R-1340 450 to 600 930 34,966 Used on: Pilgrim 100B
1925 P&W Wasp R-1340-C 450 930 34,966 On blue engine stand, ignition wires, no sign, ASM 92-21-14
Middle Hangar
1926 P&W Hornet R-1690 780 1,014 2,944 Used on: Sikorsky S-43
On blue engine stand,
sign that says it was used on Pilgrim
1926 P&W Hornet R-1690-B 780 1,014 2,944 Black engine mount, oil pan on pallet - Odom Hangar
1929 P&W Wasp Junior R-985 450 640 ≈39,000 Used on: Beechcraft Model 18
1929 P&W Wasp Junior R-985 450 640 ≈39,000 Used on: Grumman Goose
1929 P&W Wasp Junior R-985 450 640 ≈39,000 Used on: Travelair 6000B
1937 P&W Double Wasp R-2800 1,500 to 2,800 2,360 125,334 Used on: Douglas DC-6
1944 P&W Wasp Major R-4360 4,300 3,720 18,697 Used on: Fairchild C-119 Flying Boxcar
1960 P&W JT8D-17 SER 4,741 Used on: Boeing 737

Pratt & Whitney Engines

1st
Run
Name Model HP Weight Built
1925 Wasp R-1340 450 to 600 930 34,966 Used on: Fairchild 71, Noorduyn Norseman, Pilgrim 100B, Grumman Mallard
1926 Hornet R-1690 780 1,014 2,944 Larger version of the Wasp
Used on: Sikorsky S-43
1929 Wasp Junior R-985 450 640 ≈39,000 Smaller version of the Wasp
Used on: Beechcraft Model 18, Grumman Goose,
Travelair 6000B, DHC-2 Beaver, Stinson Reliant, Waco S3HD
1937 Double Wasp R-2800 1,500 to 2,800 2,360 125,334 Used on: Douglas DC-6
1944 P&W Wasp Major R-4360 4,300 3,720 18,697 Used on: Fairchild C-119 Flying Boxcar
1960   JT8D-17 SER 4,741 Used on: Boeing 737

(Wikipedia) - Pratt & Whitney

enginehistory.org Pratt & Whitney SingleRow

Pratt & Whitney R-1340 Wasp Engine

Pratt & Whitney's first engine was called the Wasp.

Completed on Christmas Eve of 1925, the Wasp was an air-cooled, radial piston engine with 1,340 cubic inches of displacement. It also featured a revolutionary design for the crankshaft and master rod, which eliminated what had proved to be a weak area in other engines. The new Wasp weighed less than 650 pounds.

The Wasp developed 425 horsepower on its third test run. It easily passed Navy qualification testing in March 1926, and by October of the same year, the Navy had ordered 200 engines. The Wasp demonstrated exceptional capabilities. It exhibited speed, rate of climb, performance at altitude and reliability that revolutionized American aviation, shattering one record after another. Soon it dominated Navy and Army Air Force fighter planes.

The Wasp also made its mark on early commercial aviation during the 1930s. Charles Lindbergh shattered the transcontinental speed record in 1930 with his Wasp-powered Lockheed Sirius. Jimmy Doolittle relied on his Wasp to take his Gee Bee aircraft to new speeds. And, Amelia Earhart made history with her Wasp-powered Lockheed Electra 10E.

(Wikipedia) - P & W R-1340 Wasp

Pratt & Whitney R-1340 Wasp

aviation-history.com - P & W R-1340

Pratt & Whitney R-1340-S1H1-G Wasp

First Run: 1925
Number Built: 34,966
General Characteristics
Type: Nine-cylinder single-row supercharged air-cooled radial engine
Bore: 5.75 in 146 mm
Stroke: 5.75 in 146 mm
Displacement: 1,344 cu in 22 L
Diameter: 51.75 in 1,314 mm
Dry weight: 930 lb 422 kg
Components
Valvetrain: 1 inlet and 1 exhaust valve per cylinder Pushrod-actuated
Supercharger: Single-speed centrifugal type supercharger, 1:10 step-up
Fuel system: Two-barrel Stromberg carburetor
Fuel type: 91 octane rating gasoline
Cooling system: Air-cooled
Reduction gear: 3:2
Performance
Power output: 600 hp at 2,250 rpm at 6,200 ft 447 kW (1,890 m)
740 hp at 2,250 rpm at 7,000 ft (2,135 m) 552 kW
Specific power: 0.45 hp/cu in 20.3 kW/l
Compression ratio: 6:1
Power-to-weight ratio: 0.65 hp/lb at cruising rpm 1.05 kW/kg
pw-wasp-r-1340-number1-nasm.jpg
Pratt & Whitney Wasp A Serial Number 1, (R-1340), Radial 9 Engine at the National Air and Space Museum. (NASM)
pw-pw-logo.jpg

Pratt & Whitney R-1340 Wasp - Fairchild 71

PW Wasp R-1340 Fairchild 71

This Pratt & Whitney R-1340 Wasp was removed from the Fairchild 71 owned by Bob Reeve.

Pratt & Whitney R-1340 Wasp - Norseman

Used on Noorduyn Norseman

N725E-engine

N725E-engine-right

N725E-engine-right-cyl

Pratt & Whitney R-1340 Wasp - Pilgrim

Pilgrim Engine Data Plate - Pratt & Whitney R-1340-AN-2
550 hp (410 kW), 3:2 geared prop shaft
N709Y Engine N709Y Engine 2 N709Y Engine 2012

Pratt & Whitney R-1340-C Wasp Engine

PW e01 front PW e01 logo pw-asm-92-21-14-tag pw-asm-92-21-14-data-plate-top

Tag numbers: TMA-76-17, ASM 92-21-14.

Data plate on right side of accessory case.

This is a single-row, 9-cylinder air-cooled radial design.

450 HP at 2,100 rpm

Pratt & Whitney R-1690 Hornet

2,944 were produced from 1926 through 1942. It is a single-row, 9-cylinder air-cooled radial design. The B model is rated at 575 hp.

(Wikipedia) - P & W R-1690 Hornet

Pratt & Whitney R-1690 Hornet

aviation-history.com - P & W Hornet

Pratt & Whitney R-1690 SIE-G

First Run: 1926
Number Built: 2,944
General Characteristics
Type: Nine-cylinder single-row supercharged air-cooled radial engine
Bore: 6 1⁄8 in 155 mm
Stroke: 6 3⁄8 in 161 mm
Displacement: 1,690 cu in 27.7 L
Length: 50.98 in 1,295 mm
Diameter: 54.41 in 1,382 mm
Dry weight: 1,014 lb 460 kg
Components
Valvetrain: 1 inlet and 1 exhaust valve per cylinder Pushrod-actuated
Supercharger: Single-speed centrifugal type supercharger, 12.0:1 gear ratio
Fuel system: Two-barrel Stromberg carburetor
Fuel type: 87 octane rating gasoline
Cooling system: Air-cooled
Reduction gear: Epicyclic gearing, 2:3
Performance
Power output: 789 hp at 2,300 rpm for takeoff 589 kW
740 hp at 2,250 rpm at 7,000 ft (2,135 m) 552 kW
Specific power: 0.47 hp/cu in 21.26 kW/l
Compression ratio: 6.0:1
Specific fuel consumption: 0.6 lb/(hp•h) 362 g/(kW•h)
Oil consumption: 0.42 oz/(hp•h) 16 g/(kW•h)
Power-to-weight ratio: 0.78 hp/lb at cruising rpm 1.28 kW/kg

Pratt & Whitney Hornet Engine

On blue engine stand, sign that says it was used on Pilgrim

“Fairchild” written in marker on flattened cowl

525 HP at 1,900 rpm

Two data plates on right side of accessory case. Top for GE supercharger, bottom for engine.

ASM 92-21-13

P&W Hornet Engine

pw-asm-92-21-13-tag

pw-asm-92-21-13-data-plate

pw-asm-92-21-13-supercharger-data-plate

Pratt & Whitney R-1690-B Hornet

R-1690-B e01 R-1690-B e01 Data Plate

2,944 were produced from 1926 through 1942. It is a single-row, 9-cylinder air-cooled radial design. The B model is rated at 575 hp.

On black engine mount, oil pan, on pallet

US ARMY AIR CORPS

TYPE: R-1690-B

SERIAL NO: 30-760

DATE ACCEPTED: 10-9-30

The ‘TYPE’ of ‘R-1690-B’ on this engine data plate was hard to find. When you Google it, you almost always get redirected to the Pratt & ‘Whitney R-1860-B Hornet’. Two foreign language versions of the R-1690 page mention that the ‘R-1690-B’ variation puts out 575 hp (429 kW)

According to the Virtual Aircraft Museum, in 1930, in Finland, there were five VL Kotka (Eagle) open-cockpit biplane maritime patrol aircraft produced with an R-1690-B engine. The remains of one is on display at the Paijat-Hame Museum.

In 1931, the prototype for the Douglas T3D, a three place open-cockpit biplane torpedo bomber originally used an R-1690-B engine, but it was later replaced with a R-1830 engine. The T3D never made it into production.

There was one mention of a US government purchase in a Google scanned magazine:

U.S. Air Services - Volume 16 - Page 58 -June 1931

“Devoted to the Development of Aeronautics - Civil and Military - in the United States, Birthplace of the Flying Machine, and Throughout the World”

Contract awards were announced on May, 23 by the War Department:

Pratt & Whitney Aircraft Company, Hartford — Thirty Hornet type R-1690-B engines and spare parts; total, $174,591.39.

1929 Pratt & Whitney R-985 Wasp Junior

Smaller version of the Wasp

Used on: Beechcraft Model 18, Grumman Goose, Travelair 6000B DHC-2 Beaver, Stinson Reliant, Waco S3HD

The Pratt & Whitney R-985 Wasp Junior is a series of nine-cylinder, air-cooled, radial aircraft engines built by the Pratt & Whitney Aircraft Company from the 1930s to the 1950s.

These engines have a displacement of 985 cu in (16 L); initial versions produced 300 hp (220 kW), while the most widely used versions produce 450 hp (340 kW).

Wasp Juniors have powered numerous smaller civil and military aircraft, including small transports, utility aircraft, trainers, agricultural aircraft, and helicopters. Over 39,000 of these engines were built, and many are still in service today.

(Wikipedia) - P & W R-985 Wasp Junior

Pratt & Whitney Wasp Junior SB

First Run: 1929
Number Built: ≈39,000
General Characteristics
Type: 9-cylinder supercharged air-cooled radial piston engine
Bore: 5 3⁄16 in 132 mm
Stroke: 5 3⁄16 in 132 mm
Displacement: 985 cu in 16.4 L
Length: 41.59 in 1,056 mm
Diameter: 45.75 in 1,162 mm
Dry weight: 640 lb 290 kg
Components
Valvetrain: 1 inlet and 1 exhaust valve per cylinder Pushrod-actuated
Supercharger: Single-speed gear-driven General Electric centrifugal supercharger, with impeller driven at 10 times crankshaft speed
Fuel type: 80/87 octane rating gasoline
Cooling system: Air-cooled
Reduction gear: Direct drive
Performance
Power output: 450 hp at 2,300 RPM for takeoff 336 kW
400 hp at 2,200 RPM up to 5,000 ft (1,500 m) 298 kW
Specific power: 0.406 hp/cu in 18.5 kW/l
Compression ratio: 6.0:1
Power-to-weight ratio: 0.625 hp/lb at cruising rpm 1.03 kW/kg

Pratt & Whitney R-985 Wasp Junior - Beechcraft Model 18

More Wasp Junior details

The Pratt & Whitney R-985 Wasp Junior is a series of nine-cylinder, air-cooled, radial aircraft engines built by the Pratt & Whitney Aircraft Company from the 1930s to the 1950s.

N1047B-right-engine
Beechcraft N1047B Right Engine - R-985-AN-14B
N1047B-left-engine-data-plate
Beechcraft N1047B Left Engine data plate - R-985-AN-14B
N1047B-right-engine-data-plate
Beechcraft N1047B Right Engine data plate - R-985-AN-14B

Pratt & Whitney R-985 Wasp Junior - Grumman Goose

More Wasp Junior details

The Pratt & Whitney R-985 Wasp Junior is a series of nine-cylinder, air-cooled, radial aircraft engines built by the Pratt & Whitney Aircraft Company from the 1930s to the 1950s.

Note that the engines are not the exact same models. Left Engine - R-985-AN-1, Right Engine - R-985-AN-14B

n789-left-engine
Grumman Goose N789 Left Engine - R-985-AN-1
N789-left-engine-data-plate
Grumman Goose N789 Left Engine data plate - R-985-AN-1
N789-right-engine-data-plate
Grumman Goose N789 Right Engine data plate - R-985-AN-14B

Pratt & Whitney R-985 Wasp Junior - Travelair 6000B

More Wasp Junior details

The Pratt & Whitney R-985 Wasp Junior is a series of nine-cylinder, air-cooled, radial aircraft engines built by the Pratt & Whitney Aircraft Company from the 1930s to the 1950s.

travelair_engine
Travelair 6000B Engine - R-985-AN-1
travelair_data
Travelair 6000B Engine data plate - R-985-AN-1

1937 Pratt & Whitney R-2800 Double Wasp

Used on: Douglas DC-6

The Pratt & Whitney R-2800 Double Wasp is an American twin-row, 18-cylinder, air-cooled radial aircraft engine with a displacement of 2,800 cu in (46 L), and is part of the long-lived Wasp family.

The R-2800 is considered one of the premier radial piston engines ever designed and is notable for its widespread use in many important American aircraft during and after World War II. During the war years, Pratt & Whitney continued to develop new ideas to upgrade this already powerful workhorse, most notably water injection for takeoff in cargo and passenger planes and to give emergency power in combat.

(Wikipedia) - P & W R-2800 Double Wasp

Pratt & Whitney R-2800-54

First Run: 1937
Number Built: 125,334
General Characteristics
Type: 18-cylinder air-cooled twin-row radial engine with water injection
Bore: 5.75 in 146.05 mm
Stroke: 6 in 152.4 mm
Displacement: 2,804.5 cu in 45.96 L
Length: 81.4 in 2,068 mm
Diameter: 52.8 in 1,342 mm
Dry weight: 2,360 lb 1,073 kg
Components
Valvetrain: Poppet, two valves per cylinder
Supercharger: Variable-speed (in F8F-2, unified with throttle via AEC automatic engine control), single-stage single-speed centrifugal type supercharger
Fuel system: One Stromberg injection carburetor
Fuel type: 100/130 octane gasoline
Cooling system: Air-cooled
Performance
Power output: 2,100 hp @ 2,700 rpm 1,567 kW
Specific power: 0.75 hp/cu in 34.1 kW/L
Power-to-weight ratio: 0.89 hp/lb 1.46 kW/kg
pw-r-2800-outside-data-plate.jpg
1937 Pratt & Whitney R-2800 Double Wasp Data Plate
pw-r-2800-outside-pallet.jpg
1937 Pratt & Whitney R-2800 Double Wasp

1944 Pratt & Whitney R-4360 Wasp Major

Used on: Boeing 377, Boeing B-50 Superfortress, Boeing C-97 Stratofreighter, Convair B-36, Fairchild C-119 Flying Boxcar, Hughes H-4 Hercules ("Spruce Goose")

The Pratt & Whitney R-4360 Wasp Major is an American four-row, 28-cylinder four-row radial piston aircraft engine designed and built during World War II, and the largest-displacement aviation piston engine to be mass-produced in the United States. It was the last of the Pratt & Whitney Wasp family, and the culmination of its maker's piston engine technology. The war was over before it could power airplanes into combat. It powered many of the last generation of large piston-engined aircraft before turbojets, and equivalent (and superior) horsepower turboprops (such as the Allison T56), supplanted it. Its main rival was the twin-row, 18-cylinder, nearly 3,350 cu in (54.9 l) displacement Wright R-3350 Duplex-Cyclone, first run some seven years earlier (May 1937).

(Wikipedia) - P & W R-4360 Wasp Major

Pratt & Whitney R-4360-51VDT Wasp Major

First Run: 1944
Number Built: 18,697
General Characteristics
Type: 28-cylinder air-cooled four-row radial engine
Bore: 5.75 in 146.05 mm
Stroke: 6 in 152.4 mm
Displacement: 4,362.5 cu in 71.489 L
Length: 103 in 2,600 mm
Diameter: 61 in 1,500 mm
Dry weight: 3,720 lb 1,690 kg
Components
Valvetrain: Poppet, two valves per cylinder
Supercharger: Gear-driven single stage variable speed centrifugal type supercharger
Turbocharger: General Electric CHM-2 (optional)
Fuel system: Bendix-Stromberg PR-100E2 pressure carburetor
Fuel type: 115/145 octane gasoline
Oil system: Dry sump
Cooling system: Air-cooled
Performance
Power output: 4,300 hp @ 2,800 rpm 3,200 kW
Specific power: 0.99 hp/cu in 45 kW/L
Power-to-weight ratio: 1.1 hp/lb 1.82 kW/kg
pw-r-4360-outside-pallet.jpg
1944 Pratt & Whitney R-4360 Wasp Major

Pratt and Whitney JT8D-17 SER Engine

B737

The Pratt & Whitney JT8D is a low-bypass (0.96 to 1) turbofan engine, introduced by Pratt & Whitney in February 1963 with the inaugural flight of the Boeing 727.

Used on: Boeing 737 Combi

(Wikipedia) - Pratt & Whitney JT8D turbo fan engine.

Pratt & Whitney JT8D-219

First Run: 1960
Number Built:  
General Characteristics
Type: Dual-spool, low-bypass-ratio turbofan
Length: 12 ft 10 in 3.91 m
Diameter: 49.2 in fan 1.25 m
Dry weight: 4,741 lb 2,150 kg
Components
Compressor: Axial flow, 1-stage fan, 6-stage LP, 7-stage HP
Combustors: Nine can-annular combustion chambers
Turbine: 3-stage (1 stage HP 3 stage LP)
Fuel type: 1
Oil system: 2
Performance
Maximum thrust: 21,000 lbf -200 series : 18,500-21,700 lbf 93.4 kN
Overall pressure ratio: 19.4
Air mass flow: 331 lb/sec
Fuel consumption: 19% reduction over JT3D
Specific fuel consumption: 0.744 kg/daN.h
Thrust-to-weight ratio: 4.43