Object Details
Designer
Lawrance Aero Engine Corp
Manufacturer
Wright Aeronautical
Physical Description
Type: Radial, 9 cylinders, air cooled
Power rating: 160 kW (215 hp) at 1,800 rpm
Displacement: 12.9 L (788 cu in)
Bore and Stroke: 114 mm (4.5 in.) x 140 mm (5.5 in.)
Weight: 231 kg (508 lb)
Summary
Charles Lawrance started his designs for an air-cooled engine in 1915. In 1921, Lawrance designed his first engine for a U.S. Navy contract, which wanted a compact lightweight engine not plagued with water leakage problems. Following a Navy encouraged merger with Wright, the Lawrance engine progressed through design stages, as the Wright Whirlwind J-3, J-4, J-5, and J-6 series. The most famous of these was the J-5, used by Lindbergh.
J-4 engines powered such aircraft as the Fairchild FC-1 and FC-2, Fokker Universal, Laird Commercial LC-B200, Stearman C2B and C3B, and Stinson Detroiter SB-1. When introduced in 1925, the J-4 was adopted by the Navy as a stock power plant. A total of 190 J-4 engines were built.
In 1926, Admiral Richard Byrd and Floyd Bennett made a flight from Spitzbergen, Norway over the North Pole and back. This was the first airplane flight over the Pole, and used the J-4B engine in a Fokker F-VII Tri-motor.
Credit Line
Transferred from the U.S. Air Force, Wright-Patterson AFB, Ohio. No known restrictions.
Date
Circa 1926
Inventory Number
A19750207000
Restrictions & Rights
CC0
Type
PROPULSION-Reciprocating & Rotary
Materials
Steel, Paint, Aluminum, Copper, Rubber, Textile, Phenolic, Preservative Coating, Brass
Dimensions
Other: 52 x 51 x 42 in., 336.6kg (132.1 x 129.5 x 106.7cm, 742lb.)
Country of Origin
United States of America
See more items in
National Air and Space Museum Collection
Data Source
National Air and Space Museum
Link to Original Record
Record ID
nasm_A19750207000
