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

Taft-Peirce (Victor Lougheed) V-8 Engine

Air and Space Museum

There are restrictions for re-using this image. For more information, visit the Smithsonian's Terms of Use page .
International media Interoperability Framework
IIIF provides researchers rich metadata and media viewing options for comparison of works across cultural heritage collections. Visit the IIIF page to learn more.
View manifest View in Mirador Viewer

Object Details

Manufacturer

Taft-Peirce Manufacturing Company (Victor Lougheed)

Designer

Victor Lougheed

Physical Description

Two reproduction cylinders are displayed next to the engine.
Type: Reciprocating, V-8, 2-stroke cycle, air-cooled
Power: 45 kW (60 hp) at 3,500 rpm estimated (engine never ran)
Displacement: 2.3 liters (140 cu in.)
Bore and Stroke: 76.2 mm (3 in.) x 63.5 mm (2.5 in.)
Weight: 37 kg (81 lb)

Summary

This engine was designed by Victor Lougheed, elder brother to Allan and Malcolm Lougheed, founders of the Lockheed Aircraft Company, and manufactured in 1911 by the Taft-Peirce Manufacturing Company of Woonsocket, Rhode Island. It was made almost entirely of Krupp chrome nickel steel at the contemporary high cost of $15,000, with the crankcase and cylinders turned from solid billets weighing approximately 908 kg (2,000 lb.)
Fuel and lubrication were forced into the cylinders through bypasses in the sides of the cylinders and pistons. Multiple poppet valves, with six in the head of each power-producing cylinder, provided for excellent and rapid scavenging of combustion gases. The eight air pumps, projecting from the lower part of the crankcase, maintained in the crankcase at all times a compression of air which was expelled through the cylinders on the exhaust stroke, and assisted in keeping the cylinders cool.

Credit Line

Gift of Frederick S. Blackall, Jr., President and Treasurer, Taft-Peirce Manufacturing Company

Date

1911

Inventory Number

A19600151000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Reciprocating & Rotary

Dimensions

Unknown

Country of Origin

United States of America

See more items in

National Air and Space Museum Collection

Location

Steven F. Udvar-Hazy Center in Chantilly, VA

Hangar

Boeing Aviation Hangar

Data Source

National Air and Space Museum

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv961eb5d38-4f70-450d-9017-1b2ae315c8d4

Record ID

nasm_A19600151000

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