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US3953707A Expired / Lapsed US ⏱️ 0.0 years remaining

Method for preheating aircooled, aircraft engines

Assignee: COLE KRUEGER INVESTMENTS Inc
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Filing: 1973-09-14
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Granted: 1976-04-27
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Expires: 1993-09-14
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Abstract

Abstract An aircooled aircraft engine is preheated prior to starting by the insertion of electric heating devices into the blind holes, normally provided for the reception of thermocouples, in the metal castings of the cylinder heads immediately adjacent to the spark plugs. The heating devices are of such size and shape that the heating devices are entirely confined in the metal wall of the cylinder casting so that when energized substantially all the heat is transferred to the castings immediately adjacent the spark plug. The heating devices are energized for a sufficient time prior to starting to generate enough heat to prevent frosting of the spark plug, prevent condensation and improve vaporization of fuel when starting the engine. Additional electric heating devices may be inserted into drain hole of the oil sump and/or the oil suction screen in the sump for simultaneous energization with the heating devices in the cylinder heads whereby heat is supplied to the engine oil to facilitate proper lubrication of the cylinders when starting the engine.

Inventors

  • 👤 Peter G. Tanis

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 11:21
CPC Classifications
F; F02; F02N; F02N19/00; F02N19/02; F01; F01M; F01M5/00; F01M5/02; H; H05; H05B; H05B3/00; H05B3/40; H05B3/42; H05B3/48; H05B3/78; H05B3/82

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 144 words
The method of preheating an aircooled, aircraft engine prior to starting the engine, said engine having a cylinder head casting, a spark plug in the casting of the cylinder head and a blind hole formed entirely in the metal of said casting immediately adjacent the spark plug, which comprises inserting in said blind hole an electric heating device of construction, size and shape such that the device is substantially entirely confined in the metal wall of the casting, applying an electric current to said heating device to generate heat therein whereby substantially all the heat is transferred to the casting to heat the casting immediately adjacent the spark plug, and maintaining the current for sufficient time to generate enough heat in the casting to prevent frosting of the spark plug and to prevent condensation and to improve vaporization of fuel when starting the engine.
Claim 2
Independent Claim 144 words
The method of preheating an aircooled, aircraft engine prior to starting the engine, said engine having a cylinder head casting, a spark plug in the casting of the cylinder head and a blind hole formed entirely in the metal of said casting immediately adjacent the spark plug, which comprises inserting in said blind hole an electric heating device of construction, size and shape such that the device is substantially entirely confined in the metal wall of the casting, applying an electric current to said heating device to generate heat therein whereby substantially all the heat is transferred to the casting to heat the casting immediately adjacent the spark plug, and maintaining the current for sufficient time to generate enough heat in the casting to prevent frosting of the spark plug and to prevent condensation and to improve vaporization of fuel when starting the engine.
Claim 3
Dependent Claim 28 words
The method as described in claim 1 in which the heating device is installed in a hole normally provided in the cylinder head casting for holding a thermocouple.
Claim 4
Independent Claim 290 words
The method of preheating an aircooled, aircraft engine prior to starting the engine, said engine having cylinder head castings, spark plugs in the castings, a blind hole formed entirely in the metal of the castings immediately adjacent to each of the spark plugs required to be heated, an oil sump casing, holes in the casing for receiving a drain plug and an oil suction screen, which comprises inserting in each of said blind holes immediately adjacent the spark plugs an electric heating device of construction, size and shape such that the heating device is confined substantially entirely in the walls of the casting, applying an electric current to said heating devices to generate heat therein whereby substantially all the heat is transferred to the castings to heat the castings immediately adjacent the spark plugs, and in addition inserting a heating device containing an electric heating element in at least one of said holes in the oil sump casing which are normally provided for said drain plug and oil suction screen, the contruction, size and shape of the latter heating device being such that a portion thereof containing the electric heating element is in contact with the wall of the oil sump casing and another portion extends into the interior of the casing occupied by the oil, applying simultaneously an electric current to the latter device whereby a substantial portion of the heat from the device is transferred directly to the casing and a portion to the oil in the sump, and maintaining the electric current to the heating device in the cylinder head and in the oil sump for sufficient time to prevent frosting of the spark plugs and to prevent improper lubrication of the cylinders when starting the engine.
Claim 5
Independent Claim 290 words
The method of preheating an aircooled, aircraft engine prior to starting the engine, said engine having cylinder head castings, spark plugs in the castings, a blind hole formed entirely in the metal of the castings immediately adjacent to each of the spark plugs required to be heated, an oil sump casing, holes in the casing for receiving a drain plug and an oil suction screen, which comprises inserting in each of said blind holes immediately adjacent the spark plugs an electric heating device of construction, size and shape such that the heating device is confined substantially entirely in the walls of the casting, applying an electric current to said heating devices to generate heat therein whereby substantially all the heat is transferred to the castings to heat the castings immediately adjacent the spark plugs, and in addition inserting a heating device containing an electric heating element in at least one of said holes in the oil sump casing which are normally provided for said drain plug and oil suction screen, the contruction, size and shape of the latter heating device being such that a portion thereof containing the electric heating element is in contact with the wall of the oil sump casing and another portion extends into the interior of the casing occupied by the oil, applying simultaneously an electric current to the latter device whereby a substantial portion of the heat from the device is transferred directly to the casing and a portion to the oil in the sump, and maintaining the electric current to the heating device in the cylinder head and in the oil sump for sufficient time to prevent frosting of the spark plugs and to prevent improper lubrication of the cylinders when starting the engine.
Claim 6
Dependent Claim 29 words
The method as described in claim 3 in which the heating device in the oil sump casing is inserted in the hole normally provided for an oil suction screen.
Claim 7
Dependent Claim 28 words
The method as described in claim 3 in which the heating device in the oil sump casing is inserted in the hole normally provided for said drain plug.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-04-27 1979-10-27 1980-04-27 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-04-27 1983-10-27 1984-04-27 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-04-27 1987-10-27 1988-04-27 $7700.00 Window Closed / Lapsed

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