The time lag and interval of discharge with a spring actuated fuel injected pump / by Robertson Matthews and A.W. Gardiner.

Format:

Book

Government document

Author/Creator:

Matthews, Robertson, author.

Gardiner, Arthur W., author.

Contributor:

United States. National Advisory Committee for Aeronautics, issuing body.

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 159.

Technical notes / National Advisory Committee for Aeronautics ; No. 159

Language:

English

Subjects (All):

Airplanes--Motors.

Airplanes.

Fuel pumps--Testing.

Fuel pumps.

Internal combustion engines--Fuel systems--Testing.

Internal combustion engines.

Physical Description:

1 online resource (15 pages, 2 unnumbered pages) : illustration

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1923.

Summary:

This note deals with some research on a spring actuated fuel pump for solid or airless injection with small, high speed internal combustion engines. The characteristics under investigation were.

(1) The interval of fuel injection in terms of degrees of crank travel and in absolute time.

(2) The lag between the time the injection pump plunger begins its stroke and the appearence of the jet at the orifice.

(3) The manner in which the fuel spray builds up to a maximum when the fuel valve is opened, and then diminishes.

Notes:

Title from title screen (viewed August 9, 2019).

"September 1923."

No Federal Depository Library Program (FDLP) item number.

Print version record.

Other Format:

Print version: Matthews, Robertson. Time lag and interval of discharge with a spring actuated fuel injected pump

OCLC:

1117765924