US2414000A - Ignition system - Google Patents

Ignition system Download PDF

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US2414000A
US2414000A US433174A US43317442A US2414000A US 2414000 A US2414000 A US 2414000A US 433174 A US433174 A US 433174A US 43317442 A US43317442 A US 43317442A US 2414000 A US2414000 A US 2414000A
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cylinders
magnetos
engine
magneto
spark plugs
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US433174A
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Walter J Spengler
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Bendix Aviation Corp
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Bendix Aviation Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P7/00Arrangements of distributors, circuit-makers or -breakers, e.g. of distributor and circuit-breaker combinations or pick-up devices
    • F02P7/02Arrangements of distributors, circuit-makers or -breakers, e.g. of distributor and circuit-breaker combinations or pick-up devices of distributors

Definitions

  • Another object of the invention is to provide a ternal combustion engine of the above type.
  • Th singleembodiment 0f the invention illustrated in the drawings, by way of example, is adapted foruse on an internal combustion engine I! of the type whereinseveral axially extending rows ll of cylinders are radially disposed about a common crankshaft (not shown), each of said rows comprising a .plurality of cylinders in-line.
  • a novel and simple system for generating and distributing high tension current to spark plugs A still further object is to provid a novel igvnition system which is so constituted and ar ranged as to materially reduce the danger of ignition failures and inemclency at high altitudes in engines having large numbers of cylinders.
  • Tubes or conduits 45 may be detachably secured to magnetos [5 as well as to the outer periphery of ring 46, the connection at the magneto being of the plug and socket type for leads 43 and 44 to thus permit quick and easy assembly and disassembly.
  • 4 10 For the purpose of convenience and simplicity, all of the so-called ground wires in ring 46 (two for each magneto) are connected to separate terminals in the socket portion 41 of a "Cannon" connector or similar multiple plu and socket connector, the details of which are well-known and, hence, not shown.
  • the abovedescribed ignition system may be supplemented with a novel booster circuit, the current producing ability of which does not depend upon the speed of rotation of the engine crankshaft as does the current supplied by magnetos l5.
  • the booster circuit comprises a buzzer coil 52 which includes a primary winding 53, a secondary winding 54, and buzzer contacts 55 and 56 (Fig. 3).
  • Movable contact 55 of booster coil 52 is connected to one end of primary winding 53, and the other end of said winding is connected to a battery 51 through a lead 58 which extends through the ground wire harness manifold 46 and is connected by means of plug connector 41, 48 with a lead 59.
  • the latter branches ofi from shieldin tube 49 at any suitable point and has a starter operated switch 60 interposed therein so that the booster circuit altitudes.
  • booster coil 52 is mounted on the nose of engine i relatively near ground wire harness manifold 16.
  • the magnetos of the novel ignition system comprehended by the present invention may be readily and conveniently supercharged for this purpose by the addition of very little extra equipment.
  • the air or other gas, such as an inert gas may be supplied to the magnetos through the ground wire harness 45, 46 from a suitable pressure source, such as a tank of compressed gas or a suitable pump ill (Fig. 3).
  • a suitable pressure source such as a tank of compressed gas or a suitable pump ill (Fig. 3).
  • the output or pressure side of pump 10 is operatively connected to one end of manifold ring 48.
  • an ignition system for a dual ignition internal combustion engine comprising a plurality of magnetos, each of said magnetos being adapted to generate electrical current for. fir-ing spark plugs in a. separate group of adjacent cylinders of said engine, a pair of ignition distributors operatively associated with each of said magnetos, means operatively connecting the dis- 'tributors of each of said pairs to spark plugs in the same group of adjacent cylinders, a source of booster currentmeans in at least one distributor of each of said magnetos for distributing booster current to spark plugs connected to said distributor, and means for connecting said last-named means in parallel and to said source of booster current.

Description

Jan. 7, 1947. I SPENGLERI 2,414,000
IGNITION SYSTEM Filed March 3, 1942 2 Sheets-Sheet l 7/ INVENTOR I BY ATTORNEY w. J. SPENGLER 2,414,000
IGNITION SYSTEM Jan. 7, 1947.
'2 Sheets-Sheet 2 Filed March 3, 1942 1 IyENTOR ATTORNEY Patented Jan. 7, I
UNITED STATES rarenriorrlcs IGNITION SYSSIFEM Walter J. Spengler, Sidney, N. Y., assignor to Bendix Aviation Corporation, South Bend, Ind., a corporation of Delaware Application lilarch 3, 1942, Serial No. 433,174
13 Claims. (01. 123-148) -This invention relates to ignition apparatus and more particularly to an ignition system for multi-cylinder internal radio shielding means therefor.
One of the objects of the present invention is I to provide a novel, simple and eflective ignition system for engines having a plurality of radiallydisposed, axially-extending rows of cylinders.
Another object of the invention is to provide a ternal combustion engine of the above type.
combustion engines and,
. 2 Fig. 4 is a detail view, with parts broken away,
showing aportion of the shielding harness for one banker-cylinders; and,
Fig. 5 is a sectional view, with parts broken away, taken substantially on line 5- -5 of Fig. 4.
Th singleembodiment 0f the invention illustrated in the drawings, by way of example, is adapted foruse on an internal combustion engine I!) of the type whereinseveral axially extending rows ll of cylinders are radially disposed about a common crankshaft (not shown), each of said rows comprising a .plurality of cylinders in-line.
As shown, the engine comprises seven rows l l of six cylinder each, forty-two cylinders in all. Each cylinder has'two diametrically disposed spark plugs l2 and I3 to provide the safety and power affordedby double ignition. Each row of cylinders isprefe'rably surrounded by a cooling jacket [4 for the circulation of a cooling fluid.
A novel and simple system for generating and distributing high tension current to spark plugs A still further object is to provid a novel igvnition system which is so constituted and ar ranged as to materially reduce the danger of ignition failures and inemclency at high altitudes in engines having large numbers of cylinders.
Another object is to provide a novel system of supercharging' the distributor chambers of an ig- -.nition system to thus enhance 'the operating characteristics of the engin at high altitudes.
The above and further objects. and novel features of the invention will more fully appear from the following detailed description when the same' is read in connection with the accompanying drawings. It is'to be expressly understood, however, that the drawings are for the purpose of illustration only and are not intended to define the limits of the invention, reference being primarily had for this latter purpose to the appended claims.
In the drawings, wherein like reference characters refer to like parts throughout the several views, 4
Fig. 1 is a diagrammatic, isometric view or a portion of an engine embodying one form of the I2 and it! of engine 10 is provided whereby the lengths of the high tension leads or conductors are keptto a minimum, thereby reducing capacity losses, the possibilities of ignition failures, and the radio shielding requirements. Likewise, thenecessary parts or units of. the present novel ignition system are kept relatively small, and are adapted to be relatively evenly distributed on the engine, thereby conserving space and insuring less air resistance and better balance and, hence, a minimum of vibration. Said system, in the form shown, comprises a double magneto l5 for supplying and distributing high tension current ,to both sets of spark plugs l2 and I3 in each row of cylinders ll. One suitable form of magneto for this purpose is illustrated in U. S. applica tlon for patentserial No. 433,175, filed on March 3, 1942 by Jakob R. Frei for improvements in magneto It is believed to be unnecessary to show a magneto in detail in the present application, since'the magneto, per se, does not constitute a part of the present invention.
novel ignition system comprehended by the pres ent invention;
Fig.2 is adiagrammatic illustration of said ignition system as viewed from the front of the engine;
Fig. 3 is a diagrammatic view of said system, with parts broken away, showing samples of the electrical connections for one bank or row of cylinders;
Each magneto I5 is preferably removably secured on a so-called mounting pad l6, which may be integrally cast with the cone-like nose of engine l0 and has an opening I! that receives the driven end of the rotor shaft of the magneto. Said shaft is drivably connected in any suitable manner, preferably through an adjustable coupling to an engine driven shaft (not shown) jour naled in a hollow boss I8 on the nose of the englue. The rotor of each magneto l5 may be constructed in accordance with any of several wellknown and suitable designs and is rotated in any suitable manner, such as in the manner pointed The primary windings a and 2la of said coils are connected in circuit with circuit breakers 22 and 23 in the usual well-known manner, said circuit breakers being simultaneously and periodl cally opened and closed by a cam 24 that may be on the rotor shaft of the magneto, or otherwise operatlvely connected thereto, for rotation in timed relation therewith for the purpose of causing high tension current to be induced in secondary windings of said coils.
Secondary windings 20b and 21b of ignition coils 20 and 21, respectively, of each of the seven magnetos l5 are electrically connected by suitable brushes to the rotating arms 25 and 26 of distributors 21 and 28, respectively. which are housed in oppositely disposed portions 29 and 30 of the metallic casings of said magnetos. Distributor arms 25 and 26 may be opera'tively connected to and driven synchronously with the magneto rotor, as is common practice in the magneto art, for conducting high tension current in predetermined sequence to circularly arranged, non-uniformly spaced contacts or terminals 3| and 32 in distributor blocks that arepreferably .(Fig. 4). Extending radially from each tube 31 are six flexible metallic conduits 4| provided with means for detachably securing the same to shielded spark plugs l2 and I3 in a manner well understood in the art, one of said conduits being shOWn in detail-in F t. 5. High tension current conductors 33 and 34 are thus led from conductor housings 29a and 30a where they are connected to terminals 3| and 32 through manifold shielding conduits 38, 31, and individual conductors branch ofl through flexible conduits 4| for electrical connection to spark plugs I2 and I3.
All free space in the distributor block housings 29a and 30a and in shields 31, 38, 4| is preferably filled with a yieldable insulating compound 42, such as polymerized cashew nutshell oil. The latter may be injected in liquid form into the space to be filled and is then reduced to a unitary yieldable solid by chemical reactions, 2. solid. which has good electrical'qualities and is capable of withstanding high temperatures. Shields 31, 38 may be secured by means of suitable brackets (not shown) to a suitable rigid portion of the engine structure.
' In order to provide simultaneous and simplified control of the operation of all seven of the magnetos l5 from a centralized and convenient point, means are provided for grounding all of the primary windings 20a and 2Ia in all of said magnetos through a common control switch that may be located in the cockpit of an airplane or at some other suitable location. From the ungrounded ends of the primary windings of the coils in. each magneto, leads 43 and 44 are led from the magneto into a metallic shielding tube 45 which is preferably flexible and, thence,
4 through a metallic manifold ring or tube 46 which is mounted on the nose of engine III inside of the circularly arranged magnetos i 5. Tubes or conduits 45 may be detachably secured to magnetos [5 as well as to the outer periphery of ring 46, the connection at the magneto being of the plug and socket type for leads 43 and 44 to thus permit quick and easy assembly and disassembly. 4 10 For the purpose of convenience and simplicity, all of the so-called ground wires in ring 46 (two for each magneto) are connected to separate terminals in the socket portion 41 of a "Cannon" connector or similar multiple plu and socket connector, the details of which are well-known and, hence, not shown. The plug portion 48 of said connector is secured to a flexible metallic shielding tube 49 housing the necessary extensions of said ground wires 43 and 44 from each magneto. Tube 49 may be similarly provided at its other end-with a "Cannon" connector for ready connection to a switch mechanism 50. The latter, which does not, per se, constitute a part of the present invention, is so constructed that when the control lever 5| is in the illustrated or ofi position, all primary windings 20a and Ma of the magneto coils will be grounded through the switch mechanism and, hence, render the magnetos inoperative for generating high tension current for distribution to spark plugs I 2 and. i3. When lever 5! points to "I on the face of switch 50, only the coils for furnishing current to spark plugs l3 on the exhaust side of the cylinders are grounded, thus permitting the engine to run on a single set of spark plugs i2. When lever 5| is at E only the coils for furnishing current to spark plugs l2 are grounded, thereby permitting the engine to run on spark plugs 13. With lever 5| pointing toward "B." full operation of all magnetos and, hence, ignition by both sets of spark plugs is permitted.
Conduits 45 and manifold ring 46 may be conveniently referred to as a ground wire harness, said ring being secured to the nose of the engine 45 by suitable brackets or the like in any manner well understood in' the art. Manifold conduit 49 may also be considered as a portion or extension of the ground wire harness. This harness serves notonly to protect the electrical con- 50 ductors contained therein and. to prevent electrical and magnetic radiations therefrom, but,
as hereafter pointed out, may also be employed as a unit in a system for superchargin the magnetos and distributor chambers associated therewith.
For the purpose of increasing the ease with which engine i9 may be started, the abovedescribed ignition system may be supplemented with a novel booster circuit, the current producing ability of which does not depend upon the speed of rotation of the engine crankshaft as does the current supplied by magnetos l5. .As shown, the booster circuit comprises a buzzer coil 52 which includes a primary winding 53, a secondary winding 54, and buzzer contacts 55 and 56 (Fig. 3). Movable contact 55 of booster coil 52 is connected to one end of primary winding 53, and the other end of said winding is connected to a battery 51 through a lead 58 which extends through the ground wire harness manifold 46 and is connected by means of plug connector 41, 48 with a lead 59. The latter branches ofi from shieldin tube 49 at any suitable point and has a starter operated switch 60 interposed therein so that the booster circuit altitudes.
is, permitted to function only when the engme starting mechanism (not shown) is in operation. Stationary contact '56 of the booster coil is also connected to a lead 6i which extends through manifold ring 48. Lead BI is extended through "Cannon plug 41, 48 anda wire in tube I! to switch 50, the connection thereof to said switch.
being such that when the latter is in any of the three 'fon positions, the primary winding 63 is grounded through the switch to permit the completion of an electrical circuit containing said primary winding and battery 51 when starter v operated switch 80 is moved to closed position- When lever 5| of the switch is in' off position, as shown, winding 53 is not grounded and, hence,- the booster coil will not function even thoughswitch 801s closed.
The secondary winding 54 of booster coil 52 is permanently grounded at one end and is con-.
nected'at its other end to one distributor of each magneto l5 by means ofa single although discontinuous lead 62. 1 The latter together with the shieldingtherefor is divided into a plurality of sections 63 and one section 64. Each of the sections 63 comprises a shielded insulated conductor having a'plug connector at each end similar to that shown at the outer end of spark plug lead 33, ll of Fig. 5; The plug connectors at the adiacent ends of adjacent sections B3-extend into sockets at opposed sides of portions or bosses 65 on distributor housings 29 and yieldably engagea conductor 66 (Fig. 3) which-conducts high tension current from secondary winding 54 to a sta-f tionary ring 61' inan insulating block mounted in distributor housing 29. From said ring the current jumps across ashort gap to a contact 68 that rotates with distributor arm 25 and distributes the booster current to contacts 3| for transmission to spark plugs I! in the desired se-* quence (Fig. 3). .The distributor contacts for the booster current in the seven magnetos 15 are thus electrically connected in parallel with each other, thereby simplifying both the booster circuit, per se, and the radio shielding required therefor. Section 64 of the booster circuit is similar to sections 63, except that one end thereof I plugs into the booster coil 52 for connection with one end of secondary winding 54.
As best illustrated in Figs. 1 and 2, booster coil 52 is mounted on the nose of engine i relatively near ground wire harness manifold 16.
maintain a pressure within the magnetos and particularly within the distributor I chambers thereof, which pressure is higher than the atmospheric pressure surrounding the aircraft at high The magnetos of the novel ignition system comprehended by the present invention may be readily and conveniently supercharged for this purpose by the addition of very little extra equipment. The air or other gas, such as an inert gas, may be supplied to the magnetos through the ground wire harness 45, 46 from a suitable pressure source, such as a tank of compressed gas or a suitable pump ill (Fig. 3). As shown, the output or pressure side of pump 10 is operatively connected to one end of manifold ring 48.
If desired, the supercharging gas may be passed through a suitable fllter and dryer to remove any foreign matter or moisture therefrom.
Leads '58 and 6| from the booster coil may be shielded The gas may be supplied directly into the magnet'o casings from the ground wire harness. which casings may be rendered relatively gastight-by suitable sealing means around the shafts which extend therefrom, or the same may be supplied into a gas-tight. casing or hood surrounding each magneto. A small amount of leakage is, of course, desirable to permit proper circulation and, hence, prevent. any undue ionization of the gaseous medium within the distributor chambers. However, if an inert gas is employed, it is likely that very little, if any, cir culatlon would be required.
There is thus provided a novel ignitionsystem for engines having large numbers of cylinders and particularly for such engines employing double ignition in each cylinder. Having regard for the large number of cylinders, the ignition system provided is very simple from the standpoints of construction and installation and lends itself readily to inspection, repair and over hauling. Additionally, said system includes simply constructed parts and units which are interchangeable and which may be inexpensively repaired or replaced in case of damage without removing the entire system, thus I materially reducingthe costs of operation and upkeep .v The system is also novelly constituted by separable units which may be conveniently arranged on the engine to minimize the lengths of high tension leads'and, hence, minimize ignition losses and increase operating efficiency. The novel ignition system comprehended also includes a novel booster circuit for starting purposes. Furthermore, the system provided lends itself to efficient supercharging of the distributor chambers for high altitude 'fiyingand is so constructed that it permits of maintaining critical flash-over distances relatively large without unduly increasing the spacerequired by any of the parts or units Although only a single embodiment of the invention has been illustrated and described in detail, it is to be expressly understood that the invention is not limited thereto. For example, various changes in the design and arrangement of parts illustrated will now be apparent to those skilled in the art and may be effected without departing from the spirit and scope of the invention. For a definition of the limits of the invention, reference is had primarily to the appended claims. 7
What is claimed is: 1. An ignition system for a' dual ignition internal combustion engine with a plurality of groups of adiacent cylinders comprising a plurality of magnetos, a pair of ignition distributors operatively associated with each of said magnetos, and means operatively connecting the disgo tributors of each of said pairs to spark plugs in the same group of adjacent cylinders of said engine.
2. An ignition system for a dual ignition internal'combus'tion engine comprising a plurality of magnetos, each of said magnetos being adapted to generate electrical current for firing spark plugs in a separate group of adjacent cylinders of said engine,'a pair of ignition distributors opadapted to generate electrical current for spark plugs in a separate group of adjacent; cylinders, two ignition distributors operatively associated with each magneto, and means operatively connecting the distributors associated with each magneto to spark plugs in the same group of adjacent cylinders, said magnetos and distributors being so constructed and operated that successive ignitions of charges in the engine cylinders take place in cylinders of different groups.
4. An ignition system for a dual ignition internal combustion engine comprising a plurality of magnetos,. a, pair ofignition distributors operatively associated with each of said magnetos, and means operatively connecting the distributors of each of said pairs to spark plugs in the same group of adjacently mounted cylinders of said engine, said distributors being 'so'operated that successively firing spark plugs are located in cylinders of different ones of said groups of cylinders.
5. In an ignition system for a dual ignition internal combustion engine comprising a plurality of magnetos, each of said magnetos being adapted to generate electrical current for. fir-ing spark plugs in a. separate group of adjacent cylinders of said engine, a pair of ignition distributors operatively associated with each of said magnetos, means operatively connecting the dis- 'tributors of each of said pairs to spark plugs in the same group of adjacent cylinders, a source of booster currentmeans in at least one distributor of each of said magnetos for distributing booster current to spark plugs connected to said distributor, and means for connecting said last-named means in parallel and to said source of booster current.
6. In an ignition system for internal combustion engines, a plurality of magnetos, a distributor having cooperable stationary and rotary conductors for distributing high tension current from each of said magnetos, a source of high tension current, such as a booster coil, and means for connecting said stationary conductors in parallel with each other andto said source of high tension current whereby current from said source is distributed by saiddistributors.
"7. An ignition system for internal combustion engines comprising a plurality of distributors for distributing high tension current to the spark plugs in the engine cylinders, each distributor comprising a plurality of spaced output terminals and a rotating element adapted to transmit high tension current to said output terminals in predetermined-sequence, a common source of high tension current, conducting means in each of said distributors in spark gap relation with said rotating element, and means connecting said conducting means of each distributor in parallel with each other and in a circuit with said common source of high tension current.
8. In an ignition system for an internal combustion engine, a plurality of distributors adapted to distribute high tension current to the spark plugs of the engine, a regular source of high tension current operatively connected to each of said 8 distributors, a source of booster current, and means including a conductor and a rotary conducting element in each distributor for distributing current from said booster source, said conductors being connected in parallel branches of an electric circuit including said booster source.
9. In an ignition systemfor an internal combustion engine, a source of high tension current, a plurality of distributors for distributing said current to the spark plugs of said engine, each of said distributors comprising a conducting element, and means connecting said elements to said source, said elements being connected in parallel with each other.
10. In an ignition system for an internal combustion engine having a plurality of radially disposed rows of cylinders, the combination of a magneto mounted on said engine adjacent each of said rows of cylinders, each of said magnetos comprising a distributor, and a radio-shielding harness for the high tension leads to a set of spark plugs in each row of cylinders, each of said shielding harnesses having the manifold thereof connected directly to the casing of the magneto mounted adjacent the corresponding row and extending therefrom along said row of cylinders.
l1.-In an ignition system for an internal combustion engine having a plurality of radially disposed rows of cylinders, the combination of a magneto mounted on said engine adjacent each of said rows of cylinders, a distributor on each of two opposite sides of each magneto, and a radio-shielding harness on each side of each row of cylinders for shielding the high tension leads to sets of spark plugs on opposite sides of each of said rows of cylinders, the manifold of each harness being directly connected to the casing of the magneto adjacent the corresponding row of cylinders.
12. In an ignition system for a radial type internal combustion engine, the combination of a plurality of magnetos circularly arranged on said engine, each of said magnetos having at least one distributor operatively associated therewith, a single source of booster current, contact means in each of said distributors for distributing current from said source to the spark plugs of said engine, said contact means including a ring-like stationary conductor in each distributor, and means for connecting said conductors in parallel with each other and to said source.
13. In an ignition system for a dual ignition internal combustion engine having a crankshaft and a plurality of rows of cylinders extending radially from said shaft, the combination of two sets of spark plugs in the cylinders oieach row, a plurality of magnetos for generating high tension current, and distributor means for distributing high tension current from each of said magnetos to two of said sets of spark plugs in the same row of cylinders, each of said magnetos supplying current to spark plugs in different cylinders than each other magneto.
WALTER J. SPENGLER.
US433174A 1942-03-03 1942-03-03 Ignition system Expired - Lifetime US2414000A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2474510A (en) * 1944-11-13 1949-06-28 Gen Motors Corp Ignition system
US20080115969A1 (en) * 2006-11-21 2008-05-22 Carl John Micu Conduit enclosure system for enclosing an engine wiring harness

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2474510A (en) * 1944-11-13 1949-06-28 Gen Motors Corp Ignition system
US20080115969A1 (en) * 2006-11-21 2008-05-22 Carl John Micu Conduit enclosure system for enclosing an engine wiring harness
US7478616B2 (en) * 2006-11-21 2009-01-20 Deere & Company Conduit enclosure system for enclosing an engine wiring harness
CN101187335B (en) * 2006-11-21 2012-08-01 迪尔公司 Conduit enclosure system for enclosing an engine wiring harness

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