IP Library Granted Patent US 11,419,204
Granted Patent B2
US 11,419,204 · App. 16/826,123 · Granted Aug 16, 2022

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.
H05H1/48F02P3/08F02P3/0807F02P3/0815F02P9/007F02P23/04H01T13/50
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Quick Facts
Patent No.
US 11,419,204
App. No.
16/826,123
Granted
Aug 16, 2022
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 (45)

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 pulse of high current electrical discharge in the igniter in an initiation region between the pair of electrodes, and formation of a plasma kernel adjacent said initiation region;

b. switching a switching element, in response to a signal from a pulse generator, to draw at least most of the pulse of high current electrical discharge from between the pair of electrodes of the igniter through the switching element; and

c. switching the switching element off while current therethrough is not zero.

2. The method of claim 1 , further comprising, following breakdown, switching the switching element to apply to said electrodes at least one follow-on pulse by discharging a plasma-sustaining capacitor in response to a signal from the pulse generator.

3. The method of claim 2 , wherein:

one or more of the at least one follow-on pulse are voltage pulses generated by the plasma-sustaining capacitor pulling its discharge current through an inductance; and

the inductance is in series with the plasma-sustaining capacitor and inductively coupled to a second inductance that is in series with one of the electrodes.

4. The method of claim 3 , wherein the inductance is further in series with a second switching element that modulates a discharge current of the plasma-sustaining capacitor.

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

6. The method of claim 1 , wherein the switching element is switched on a plurality of times, each time to draw at least most of a respective pulse of high current electrical discharge from the igniter through the switching element, and wherein the switching element is switched off at least once between the plurality of times the switching element is switched on.

7. The method of claim 1 , wherein switching the switching element draws all of the pulse of high current electrical discharge from between the pair of electrodes of the igniter through the switching element.

8. The method of claim 1 , wherein switching the switching element draws most of the pulse of high current electrical discharge from between the pair of electrodes of the igniter through the switching element.

9. The method of claim 8 , wherein switching the switching element draws, through the switching element, all of the pulse of high current electrical discharge beyond simmer current used to avoid total plasma recombination between the pair of electrodes.

10. The method of claim 1 , further comprising:

discharging a plasma-sustaining capacitor to cause at least most of the pulse of high current electrical discharge in the igniter,

wherein switching the switching element draws, through the switching element, all of the pulse of high current electrical discharge caused by discharging the plasma-sustaining capacitor.

11. The method of claim 1 , wherein the switching element is in series with an inductance that is coupled to the pair of electrodes, and the switching element is configured to draw, through the switching element, all of the pulse of high current electrical discharge that passes through the inductance.

12. 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 pulse of high current electrical discharge in the igniter in an initiation region between the pair of electrodes, and formation of a plasma kernel adjacent said initiation region; and

a switching element configured to:

switch, in response to a signal from a pulse generator, to draw at least most of the pulse of high current electrical discharge from between the pair of electrodes of the igniter through the switching element; and

be switched off while current therethrough is not zero.

13. The circuit of claim 12 , further comprising:

a plasma-sustaining capacitor,

wherein the switching element is further configured to, following breakdown, apply to the electrodes at least one follow-on pulse by discharging the plasma-sustaining capacitor in response to a signal from the pulse generator.

14. The circuit of claim 13 , wherein:

one or more of the at least one follow-on pulse are voltage pulses generated by the plasma-sustaining capacitor pulling its discharge current through an inductance; and

the inductance is in series with the plasma-sustaining capacitor and inductively coupled to a second inductance that is in series with one of the electrodes.

15. The circuit of claim 14 , wherein the inductance is further in series with a second switching element configured to modulate a discharge current of the plasma-sustaining capacitor.

16. The circuit of claim 12 , wherein the igniter is a traveling spark igniter.

17. The circuit of claim 12 , wherein the switching element is of a type that can be switched while the current therethrough is not constant.

18. The circuit of claim 12 , wherein the pulse generator is configured to switch the switching element on a plurality of times, each time to draw at least most of a respective pulse of high current electrical discharge from the igniter through the switching element and to switch the switching element off at least once between the plurality of times the switching element is switched on.

19. The circuit of claim 12 , wherein the switching element is coupled in series with the pair of electrodes of the igniter to receive at least most of the pulse of high current electrical discharge from the igniter.

20. The circuit of claim 12 , wherein the switching element is configured to draw all of the pulse of high current electrical discharge from between the pair of electrodes of the igniter through the switching element.

21. The circuit of claim 12 , wherein the switching element is configured to draw most of the pulse of high current electrical discharge from between the pair of electrodes of the igniter through the switching element.

22. The circuit of claim 21 , wherein the switching element is configured to draw, through the switching element, all of the pulse of high current electrical discharge beyond simmer current used to avoid total plasma recombination between the pair of electrodes.

23. The circuit of claim 12 , further comprising:

a plasma-sustaining capacitor to cause at least most of the pulse of high current electrical discharge in the igniter,

wherein the switching element is configured to:

cause the plasma-sustaining capacitor to discharge at least most of the pulse of high current electrical discharge in the igniter; and

draw, through the switching element, all of the pulse of high current electrical discharge caused by discharging the plasma-sustaining capacitor.

24. The circuit of claim 12 , further comprising:

an inductance coupled to the pair of electrodes,

wherein the switching element is in series with the inductance and configured to draw, through the switching element, all of the pulse of high current electrical discharge that passes through the inductance.

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 Dec 29, 2020
From: SUCKEWER, ARTUR P.; SUCKEWER, SZYMON; SELMON, FREDERICK H., III
To: KNITE, INC.
Reel/Frame 054768/0686 →
Continuity (10)
Continuation 15877369 · Jan 22, 2018
Continuation 15268253 · Sep 16, 2016
Division 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 20210059038A1 · Feb 25, 2021