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naca-report-982

naca-report-982
  • Version
  • 66 Downloads
  • 2.41 MB File Size
  • 1 File Count
  • September 1, 2016 Create Date
  • September 1, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Report - Icing Protection Requirements for Reciprocating Engine Induction Systems

naca-report-982 Icing Protection Requirements for Reciprocating Engine Induction Systems-1

Despite the derelop-ment of relatirely ice—free fuel—metering
systems, the widespread use of alternate and heated—air intakes,
and the use of alcohol for emergency tie-icing, icing of aircraft-
e-ngine induction systems is a seridas problem. Investigations
have been made to study and to combat all phases of this icing
problem. From these in-restigations, criterions for safe opera-
tion and for design of new induction systems have been estab-
lished.

The results were obtained from laboratory investigations of
carburetor-supercharger combinations, wind-tunnel i-ntestiga-
tions of air scoops, multicylinder—engine studies, and flight
inrestigations. Characteristics of the three forms of ice, impact,
throttling, and fuel eraporation, were studied. The ejects of
sereral factors on the icing characteristics were also studied and
included (I) atmospheric conditions, (fl) engine and air-scoop
configurations, including light-airplane systems, (3) type of
fuel used, and (4) operating rariables, such as power condition,
use of a manifold pressure regulator, mixture setting, carburetor
heat, and water-alcohol injection. In addition, ice-detection
methods were investigated and methods of prerenting and re-
moving induction-system ice were studied. Recommendations
are given for design and operation uith regard to induction-
system icing.

Ice formations within an aircraft—engine induction system
are serious hazards because: (1) the critical areas may be
sufiiciently restricted to reduce considerably the flow of
combustion air to the engine; (2) the fuel—metering process
may be upset and cause erratic engine operation; or (3) the
movable parts, such as the throttle or the heat damper, may
freeze and become inoperative.

The symptoms associated with induction-system icing are
not. always discernablc and recognition of icing conditions
usually requires considerable operational experience and
judgment. This type of icing is not. necessarily a cold-
weather phenomenon, but may occur at temperatures far
above the normal ambient freezing level.

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naca-report-982

naca-report-982
  • Version
  • 66 Downloads
  • 2.41 MB File Size
  • 1 File Count
  • September 1, 2016 Create Date
  • September 1, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Report - Icing Protection Requirements for Reciprocating Engine Induction Systems

naca-report-982 Icing Protection Requirements for Reciprocating Engine Induction Systems-1

Despite the derelop-ment of relatirely ice—free fuel—metering
systems, the widespread use of alternate and heated—air intakes,
and the use of alcohol for emergency tie-icing, icing of aircraft-
e-ngine induction systems is a seridas problem. Investigations
have been made to study and to combat all phases of this icing
problem. From these in-restigations, criterions for safe opera-
tion and for design of new induction systems have been estab-
lished.

The results were obtained from laboratory investigations of
carburetor-supercharger combinations, wind-tunnel i-ntestiga-
tions of air scoops, multicylinder—engine studies, and flight
inrestigations. Characteristics of the three forms of ice, impact,
throttling, and fuel eraporation, were studied. The ejects of
sereral factors on the icing characteristics were also studied and
included (I) atmospheric conditions, (fl) engine and air-scoop
configurations, including light-airplane systems, (3) type of
fuel used, and (4) operating rariables, such as power condition,
use of a manifold pressure regulator, mixture setting, carburetor
heat, and water-alcohol injection. In addition, ice-detection
methods were investigated and methods of prerenting and re-
moving induction-system ice were studied. Recommendations
are given for design and operation uith regard to induction-
system icing.

Ice formations within an aircraft—engine induction system
are serious hazards because: (1) the critical areas may be
sufiiciently restricted to reduce considerably the flow of
combustion air to the engine; (2) the fuel—metering process
may be upset and cause erratic engine operation; or (3) the
movable parts, such as the throttle or the heat damper, may
freeze and become inoperative.

The symptoms associated with induction-system icing are
not. always discernablc and recognition of icing conditions
usually requires considerable operational experience and
judgment. This type of icing is not. necessarily a cold-
weather phenomenon, but may occur at temperatures far
above the normal ambient freezing level.

FileAction
naca-report-982 Icing Protection Requirements for Reciprocating Engine Induction Systems.pdfDownload 
17,005 Documents in our Technical Library
2727408 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...