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Hamilton Standard 2E40 Propeller, controllable-pitch, two-blade, metal

Catalog Data

Manufacturer:
Hamilton Standard Propellers  Search this
Materials:
Aluminum
Type:
PROPULSION-Propellers & Impellers
Country of Origin:
United States of America
Date:
c.1933
Physical Description:
Type: Two-Blades, Controllable Pitch, Metal
Diameter: 198.8 cm (78.25 in.)
Chord: 24.8 cm (9.75 in.)
Engine Application: Unknown
Summary:
The stock market crash of 1929 and the Great Depression threatened the continued existence the American aviation industry just as it started to grow in the wake of unprecedented government legislation and Lindbergh's transatlantic flight. The newly-formed Hamilton Standard Propeller Corporation, suffering from dwindling government contracts, scrambled for a new product to sustain the young corporation. Chief engineer Frank Caldwell's design for a hydraulic two-position, controllable-pitch, or hydro-controllable, propeller that he had patented in 1929 saved the company.
In 1933 Hamilton Standard and Frank Caldwell won the prestigious Collier Trophy for development of the company's controllable pitch propeller. This is a chromed cutaway of that type of propeller on its crankcase.
Credit Line:
Gift of Hamilton Standard Propellers, Division of United Aircraft Corporation, East Hartford, CT
Inventory Number:
A19400003000
Restrictions & Rights:
Usage conditions apply
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
GUID:
http://n2t.net/ark:/65665/nv96282f141-02c6-45ae-b1be-64c81852df4f
EDAN-URL:
edanmdm:nasm_A19400003000