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Discharge characteristics of a high speed fuel injection engine / by Robertson Matthews.

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Format:
Book
Government document
Author/Creator:
Matthews, Robertson, author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 213.
Technical notes / National Advisory Committee for Aeronautics ; No. 213
Language:
English
Subjects (All):
Internal combustion engines.
Fuel pumps--Testing.
Fuel pumps.
gas engines.
Physical Description:
1 online resource (21 pages, 12 unnumbered pages) : illustrations
Place of Publication:
[Washington, D.C.] : National Advisory Committee for Aeronautics, 1925.
Summary:
This paper deals with some discharge characteristics of a fuel injection system intended primarily for high speed service. The system consisted of a cam actuated fuel pump, a spring loaded automatic injection valve and connecting tube. The pump was provided with two ball inlet valves, but no discharge valves, and was operated at speeds from 600 to 1800 R.P.M. The data were taken by spraying on blackened paper attached to the side of the flywheel rim. Patterns were thus formed on the paper, a single record pattern being the result of a number of discharges. From oscilloscope observations, it is believed that the discharges during each run were fairly uniform.
The spray patterns showed the beginning of discharge to be definite while the end was drawn out and somewhat indefinite. For any given R.P.M. the lag of the jet was nearly constant for different lengths of plunger stroke. Discharge continued for a considerable interval after the plunger stroke was completed.
Notes:
Online resource, PDF version; title from title page (TRAIL, viewed April 23, 2020).
"February 1925."
"Langley Memorial Aeronautical Laboratory."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical reference (page 21).
Print version record.
Other Format:
Print version: Matthews, Robertson. Discharge characteristics of a high speed fuel injection engine
OCLC:
1127388875

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