IP Library Granted Patent US 12,158,132
Granted Patent B2
US 12,158,132 · App. 17/396,225 · Granted Dec 3, 2024

Method and apparatus for operating traveling spark igniter at high pressure

Inventors: Artur P. Suckewer (Franklin Park, NJ); Szymon Suckewer (Princeton, NJ); Frederick H. Selmon, III (Lawrenceville, NJ)
Assignee: Knite, Inc.
F02P9/007F02P3/08F02P3/0807F02P3/0815F02P23/04H01T13/50H05H1/48
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Quick Facts
Patent No.
US 12,158,132
App. No.
17/396,225
Granted
Dec 3, 2024
Kind
B2
Abstract

An ignition circuit and a method of operating an igniter (preferably a traveling spark igniter) in an internal combustion engine, including a high pressure engine. A high voltage is applied to electrodes of the igniter, sufficient to cause breakdown to occur between the electrodes, resulting in a high current electrical discharge in the igniter, over a surface of an isolator between the electrodes, and formation of a plasma kernel in a fuel-air mixture adjacent said surface. Following breakdown, a sequence of one or more lower voltage and lower current pulses is applied to said electrodes, with a low “simmer” current being sustained through the plasma between pulses, preventing total plasma recombination and allowing the plasma kernel to move toward a free end of the electrodes with each pulse.

Claims (27)

1. A method of plasma generation, comprising:

a. applying to an igniter having at least a pair of electrodes a voltage of amplitude sufficient to cause breakdown to occur between the electrodes, resulting in a high current electrical discharge in the igniter in an initiation region, and formation of a plasma kernel adjacent said initiation region; and

b. following breakdown, switching a switching element to apply to said electrodes at least one follow-on pulse of current in the igniter by discharging a plasma-sustaining capacitor via a current-controlling discharge path such that at least most of the current in the igniter flows in the discharge path through each of the switching element and the plasma-sustaining capacitor.

2. The method of claim 1 , wherein the switching element is of a type that can be switched while current therethrough is not zero.

3. The method of claim 2 , wherein the switching of the switching element includes turning off the switching element while the current therethrough is not zero.

4. The method of claim 2 , wherein-the at least one follow-on pulse are voltage pulses generated by the capacitor pulling its discharge current through an inductance.

5. The method of claim 4 , wherein the inductance is in series with the capacitor and one of the electrodes.

6. The method of claim 1 , wherein the discharge path modulates the current in the igniter.

7. The method of claim 1 , further comprising providing at least one limit of current drain off of the plasma-sustaining capacitor.

8. The method of claim 4 , wherein the current flowing through the inductance induces a second current flowing through a second inductance inductively coupled to the inductance such that the second current flows from a second capacitor through the second inductance.

9. The method of claim 1 , further comprising applying a pulse to the switching element using a pulse generator to cause the discharging of the plasma-sustaining capacitor.

10. The method of claim 1 , wherein, while discharging the current from the plasma-sustaining capacitor, the current discharged by the plasma-sustaining capacitor flows between the switching element and the electrodes through an inductance.

11. The method of claim 1 , wherein the switching the switching element discharges the plasma-sustaining capacitor such that all of the current in the igniter flows in the discharge path through each of the switching element and the plasma-sustaining capacitor.

12. The method of claim 1 , wherein the switching element comprises a thyristor or an IGBT.

13. A circuit for plasma generation, the circuit comprising:

an igniter having at least a pair of electrodes and configured to have applied thereto a voltage of amplitude sufficient to cause breakdown to occur between the electrodes, resulting in a high current electrical discharge in the igniter in an initiation region, and formation of a plasma kernel adjacent said initiation region;

a plasma-sustaining capacitor; and

a current-controlling discharge path comprising a switching element, the switching element being configured such that, when the switching element is switched following breakdown to apply at least one follow-on pulse of current in the igniter, at least most of the current in the igniter flows in the discharge path through each of the plasma-sustaining capacitor and the switching element.

14. The circuit of claim 13 , wherein the switching element is of a type that can be switched while current therethrough is not zero.

15. The circuit of claim 14 , wherein the circuit is configured to, following breakdown, turn off the switching element while the current therethrough is not zero.

16. The circuit of claim 14 , further comprising an inductance, wherein the plasma-sustaining capacitor is configured to pull its discharge through the inductance to generate the at least one follow-on pulse as one or more voltage pulses.

17. The circuit of claim 16 , wherein the inductance is in series with the capacitor.

18. The circuit of claim 13 , wherein the switching element is configured to modulate a discharge current of the plasma-sustaining capacitor.

19. The circuit of claim 13 , wherein the circuit is further configured to provide at least one limit of current drain off of the plasma-sustaining capacitor.

20. The circuit of claim 13 , further comprising a first inductance and a second inductance that is inductively coupled to the first inductance, wherein the first inductance is configured to, when the current is flowing through the first inductance, induce a second current flowing through the second inductance such that the second current flows from the electrodes through the second inductance.

21. The circuit of claim 13 , further comprising a pulse generator configured to, following breakdown, apply a pulse to the switching element to cause the discharging of the plasma-sustaining capacitor.

22. The circuit of claim 16 , wherein the current controlling-discharge path is configured such that, while the switching element discharges the plasma-sustaining capacitor, at least most of the current flows through each of the inductance, the plasma-sustaining capacitor, and the switching element.

Assignments (10)
SECURITY INTEREST Recorded Sep 16, 2025
From: ADAMS RITE AEROSPACE, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NA INC; AMSAFE, INC.; ARMTEC DEFENSE PRODUCTS CO.; CHAMPION AEROSPACE LLC; HARCOSEMCO LLC; KING NUTRONICS, LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.; SHIELD RESTRAINT SYSTEMS, INC; SIMPLEX MANUFACTURING CO.; WHIPPANY ACTUATION SYSTEMS, LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 072267/0977 →
SECURITY INTEREST Recorded Sep 16, 2025
From: ADAMS RITE AEROSPACE, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NA INC; AMSAFE, INC.; ARMTEC DEFENSE PRODUCTS CO.; CHAMPION AEROSPACE LLC; HARCOSEMCO LLC; KING NUTRONICS, LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.; SHIELD RESTRAINT SYSTEMS, INC; SIMPLEX MANUFACTURING CO.; WHIPPANY ACTUATION SYSTEMS, LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 072268/0176 →
SECURITY INTEREST Recorded Sep 16, 2025
From: ADAMS RITE AEROSPACE, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NA INC; AMSAFE, INC.; ARMTEC DEFENSE PRODUCTS CO.; CHAMPION AEROSPACE LLC; HARCOSEMCO LLC; KING NUTRONICS, LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.; SHIELD RESTRAINT SYSTEMS, INC; SIMPLEX MANUFACTURING CO.; WHIPPANY ACTUATION SYSTEMS, LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 072267/0935 →
SECURITY INTEREST Recorded Sep 16, 2025
From: ADAMS RITE AEROSPACE, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NA INC; AMSAFE, INC.; ARMTEC DEFENSE PRODUCTS CO.; CHAMPION AEROSPACE LLC; HARCOSEMCO LLC; KING NUTRONICS, LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.; SHIELD RESTRAINT SYSTEMS, INC; SIMPLEX MANUFACTURING CO.; WHIPPANY ACTUATION SYSTEMS, LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 072268/0193 →
SECURITY INTEREST Recorded Sep 16, 2025
From: ADAMS RITE AEROSPACE, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NA INC; AMSAFE, INC.; ARMTEC DEFENSE PRODUCTS CO.; CHAMPION AEROSPACE LLC; HARCOSEMCO LLC; KING NUTRONICS, LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.; SHIELD RESTRAINT SYSTEMS, INC; SIMPLEX MANUFACTURING CO.; WHIPPANY ACTUATION SYSTEMS, LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 072268/0018 →
SECURITY INTEREST Recorded Sep 16, 2025
From: ADAMS RITE AEROSPACE, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NA INC; AMSAFE, INC.; ARMTEC DEFENSE PRODUCTS CO.; CHAMPION AEROSPACE LLC; HARCOSEMCO LLC; KING NUTRONICS, LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.; SHIELD RESTRAINT SYSTEMS, INC; SIMPLEX MANUFACTURING CO.; WHIPPANY ACTUATION SYSTEMS, LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 072268/0030 →
SECURITY INTEREST Recorded Sep 5, 2025
From: ADAMS RITE AEROSPACE, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NA INC.; AMSAFE, INC.; ARMTEC DEFENSE PRODUCTS CO.; CHAMPION AEROSPACE LLC; HARCOSEMCO LLC; KING NUTRONICS, LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; WHIPPANY ACTUATION SYSTEMS, LLC
To: GOLDMAN SACHS BANK USA, AS AGENT
Reel/Frame 072167/0457 →
SECURITY INTEREST Recorded Aug 26, 2025
From: TRANSDIGM INC.; 17111 WATERVIEW PKWY LLC; 4455 GENESEE PROPERTIES, LLC; 4455 GENESEE STREET, LLC; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC LLC; AIRBORNE ACQUISITION, INC.; AIRBORNE GLOBAL, INC.; AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS NA INC.; AIRBORNE SYSTEMS NORTH AMERICA INC.; AIRBORNE SYSTEMS NORTH AMERICA OF CA INC.; AMSAFE GLOBAL HOLDINGS, INC.; AMSAFE, INC.; ANGUS ELECTRONICS CO.; APICAL INDUSTRIES, INC.; ARKWIN INDUSTRIES, INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC COUNTERMEASURES TNO CO.; ARMTEC DEFENSE PRODUCTS CO.; ASHFORD PROPERTIES, LLC; AUXITROL WESTON USA, INC.; AVIATION TECHNOLOGIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECHTYEE, INC.; BETA TRANSFORMER TECHNOLOGY LLC; BREEZE-EASTERN LLC; BRIDPORT HOLDINGS, INC.; BRIDPORT-AIR CARRIER, INC.; BRUCE AEROSPACE INC.; CALSPAN, LLC; CALSPAN AIR FACILITIES, LLC; CALSPAN AIR SERVICES, LLC; CALSPAN ASE PORTUGAL, INC.; CALSPAN HOLDINGS, LLC; CALSPAN JETS LLC; CALSPAN TECHNOLOGY ACQUISITION LLC; CDA INTERCORP LLC; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; CHELTON AVIONICS HOLDINGS, INC.; CHELTON AVIONICS, INC.; CHELTON DEFENSE PRODUCTS, INC.; CMC ELECTRONICS AURORA LLC; CPI EDB INTERMEDIATE HOLDINGS, INC.; CPI ELECTON DEVICE BUSINESS, INC.; CTHC LLC; DART AEROSPACE USA, INC.; DART BUYER, INC.; DART HELICOPTER SERVICES, INC.; DART INTERMEDIATE, INC.; DART TOPCO, INC.; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; ESTERLINE EUROPE COMPANY LLC; ESTERLINE INTERNATIONAL COMPANY; ESTERLINE TECHNOLOGIES CORPORATION; ESTERLINE TECHNOLOGIES SGIP LLC; FPT INDUSTRIES LLC; GENESEE HOLDINGS, LLC; GENESEE HOLDINGS II, LLC; GENESSE HOLDINGS III, LLC; HARCOSEMCO LLC; HARTWELL CORPORATION; HELI TECH, INC.; HYTEK FINISHES CO.; ICEMAN HOLDCO, INC.; ILC HOLDINGS, INC.; JANCO CORPORATION; JOHNSON LIVERPOOL LLC; KING NUTRONICS, LLC; KIRKHILL INC.; KORRY ELECTRONICS CO.; LEACH HOLDING CORPORATION; LEACH INTERNATIONAL CORPORATION; LEACH MEXICO HOLDING LLC; LEACH TECHNOLOGY GROUP, INC.; MARATHONNORCO AEROSPACE, INC.; MASON ELECTRIC CO.; MCKECHNIE AEROSPACE DE, INC.; MCKECHNIE AEROSPACE HOLDINGS, INC.; MCKECHNIE AEROSPACE US LLC; MEDTHERM LABS, LLC; MICROWAVE POWER PRODUCTS, INC.; NAT SEATTLE INC.; NMC GROUP, INC.; NORDISK AVIATION PRODUCTS LLC; NORTH HILLS SIGNAL PROCESSING CORP.; NORTH HILLS SIGNAL PROCESSING OVERSEAS LLC; NORWICH AERO PRODUCTS, INC.; OFFSHORE HELICOPTER SUPPORT SERVICES, INC.; PALOMAR PRODUCTS, INC.; PARAVION TECHNOLOGY, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; POWER DEVICE CORPORATION; RAPTOR LABS HOLDCO, LLC; RAPTOR LABS INTERMEDIATE, LLC; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SENSOR CONCEPTS, LLC; SERVOTRONICS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; SKANDIA, INC.; SKURKA AEROSPACE INC.; SPACE ELECTRONICS LLC; SYMETRICS INDUSTRIES, LLC; TA AEROSPACE CO.; TACTIAR FLUID CONTROLS, INC.; TDG ESL HOLDINGS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR US LLC; TESTVONICS, INC.; TEXAS ROTRONICS, INC.; TRANSICOIL LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; BRIDPORT ERIE AVIATION, INC.; TRANSDIGM GROUP INCORPORATED; TRANSDIGM UK HOLDINGS LIMITED
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 072473/0485 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 21, 2025
From: KNITE INC.
To: CHAMPION AEROSPACE LLC
Reel/Frame 071183/0378 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 13, 2022
From: SUCKEWER, ARTUR P.; SUCKEWER, SZYMON; SELMON, FREDERICK H., III
To: KNITE, INC.
Reel/Frame 059900/0793 →
Continuity (10)
Continuation 16711083 · Dec 11, 2019
Continuation 15932360 · Feb 16, 2018
Continuation 15186319 · Jun 17, 2016
Continuation 14933938 · Nov 5, 2015
Continuation 14094922 · Dec 3, 2013
Continuation 13222298 · Aug 31, 2011
Continuation 12313927 · Nov 26, 2008
Continuation 11407850 · Apr 19, 2006
Provisional Application 60672892 · Apr 19, 2005
Related Publication 20220030694A1 · Jan 27, 2022