Skip to main content Skip to main navigation
heart-solid My Visit Donate
Home Smithsonian Institution IK development site for ODI
Press Enter to activate a submenu, down arrow to access the items and Escape to close the submenu.
    • Overview
    • Museums and Zoo
    • Entry and Guidelines
    • Museum Maps
    • Dine and Shop
    • Accessibility
    • Visiting with Kids
    • Group Visits
    • Overview
    • Exhibitions
    • Online Events
    • All Events
    • IMAX & Planetarium
    • Overview
    • Topics
    • Collections
    • Research Resources
    • Stories
    • Podcasts
    • Overview
    • For Caregivers
    • For Educators
    • For Students
    • For Academics
    • For Lifelong Learners
    • Overview
    • Become a Member
    • Renew Membership
    • Make a Gift
    • Volunteer
    • Overview
    • Our Organization
    • Our Leadership
    • Reports and Plans
    • Newsdesk
heart-solid My Visit Donate

Engine, Speco (Michell) Crankless Barrell 12

Air and Space Museum

Object Details

Designer

A. G. M. Michell, Australian

Manufacturer

Steel Products Engineering Corporation (SPECO)

Physical Description

Type: Reciprocating, 12 cylinders, four stroke cycle, barrel type, liquid-cooled
Power rating: 597 kW (800 hp) at 2,500 rpm
Displacement: 34 L (2,096 cu in.)
Bore and Stroke: 158 mm (6.22 in.) x 146 mm (5.74 in.)
Weight: 2596.9 kg (1,316 lb)

Summary

This artifact was built by the Steel Products Engineering Company for the Michell-Crankless Engines Corporation, and tested by the U.S. Navy Bureau of Aeronautics. It is based on an invention of A. G. M. Michell, an Australian reciprocating engine expert. The barrel engine has a driveshaft on which is fitted an inclined disc or swashplate. Twelve cylinders are arranged radially around the driveshaft, with six cylinders on one end opposing six on the other end. The pistons act on both sides of the swashplate, and by means of almost frictionless pads, produces the rotary motion of the driveshaft. Fuel is supplied through four carburetors, two on each side. Valves are located on each side of the swashplate.
The weight and space economy of the crankless design was claimed to make it particularly well suited for application to aircraft engines. However, the Navy concluded that the performance compared unfavorably to conventional engines, and development was discontinued.

Credit Line

Transferred from the U.S. Navy, Naval Supply Center, Norfolk, Virginia

Date

Circa 1929

Inventory Number

A19650281000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Reciprocating & Rotary

Materials

Aluminum
Steel
Copper Alloy
Fabric
Rubber
Paint
Cadmium Plating

Dimensions

Length 213.4 cm (84 in.), Width 95.9 cm (37.75 in.), Height 134.6 cm (53 in.)

Country of Origin

United States of America

See more items in

National Air and Space Museum Collection

Data Source

National Air and Space Museum

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv986db5ca2-95aa-4da6-81c6-4b0acadd20d9

Record ID

nasm_A19650281000

Discover More

Image of Packard Merlin V-1650-7 engine

Propulsion

Image of Packard Merlin V-1650-7 engine

Propulsion

arrow-up Back to top
Home
  • Facebook facebook
  • Instagram instagram
  • LinkedIn linkedin
  • YouTube youtube

  • Contact Us
  • Get Involved
  • Shop Online
  • Job Opportunities
  • Equal Opportunity
  • Inspector General
  • Records Requests
  • Accessibility
  • Host Your Event
  • Press Room
  • Privacy
  • Terms of Use