IP Library Granted Patent US 11,715,935
Granted Patent B2
US 11,715,935 · App. 17/368,515 · Granted Aug 1, 2023

Traveling spark igniter

Inventor: Artur P. Suckewer (Franklin Park, NJ)
Assignee: Knite, Inc.
H01T13/52F02P9/007F02P23/04H01T13/22H01T13/34H01T13/467
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Quick Facts
Patent No.
US 11,715,935
App. No.
17/368,515
Granted
Aug 1, 2023
Kind
B2
Abstract

An igniter having at least two electrodes spaced from each other by an insulating member having a substantially continuous surface along a path between the electrodes. The electrodes extend substantially parallel to each other for a distance both above and below said surface. The insulating member has a channel (recess) for receiving at least a portion of a length of at least one of said electrodes below and to said surface of the insulating member. The surface of the insulating member may preferably be augmented with a conductivity enhancing agent. The insulating member and electrodes are configured so that an electric field between the electrodes at said surface does not have abrupt field intensity changes, whereby when a potential is applied to the electrodes sufficient to cause breakdown to occur between the electrodes, discharge occurs at said surface of the insulating member to define a plasma initiation region.

Claims (41)

1. An igniter having at least two electrodes spaced from each other by an insulating member having a continuous surface along a path between the at least two electrodes, the at least two electrodes extending parallel to each other in a first direction for a distance both above and below said continuous surface, the insulating member being shaped with a first inset channel for receiving at least a portion of a length of a first electrode of said at least two electrodes below and to said continuous surface of the insulating member and a second inset channel for receiving at least a first side of at least a portion of a length of a second electrode of said at least two electrodes and exposing at least a second side of the portion of the length of the second electrode, the first and second sides facing in directions perpendicular to the first direction, wherein said continuous surface of the insulating member defines a plasma initiation region for when a potential is applied to the at least two electrodes sufficient to cause breakdown to occur between the at least two electrodes.

2. The igniter of claim 1 , wherein said continuous surface of the insulating member is doped with a conductivity-enhancing agent.

3. The igniter of claim 2 , wherein the insulating member is of a ceramic material and the conductivity-enhancing agent is a metallic material.

4. The igniter of claim 1 , wherein said continuous surface of the insulating member is at least partially coated with a conductivity-enhancing agent.

5. The igniter of claim 1 , wherein the first inset channel is a bore, surrounded by the insulating member, that receives the first electrode.

6. The igniter of claim 1 , wherein:

the first electrode is an inner electrode; and

the second electrode is one of a plurality of outer electrodes elongated in the first direction, the insulating member having, for each of the plurality of outer electrodes, an inset channel running parallel to the inner electrode and shaped to receive at least a third side of said outer electrode and to expose at least a fourth side of said outer electrode, the third and fourth sides facing in directions perpendicular to the first direction.

7. The igniter of claim 1 , wherein the continuous surface is a flat surface.

8. The igniter of claim 1 , wherein the at least two electrodes remain parallel for at least 0.080″ below the initiation region.

9. The igniter of claim 1 , wherein the second electrode has a curved surface inset into the second inset channel, the second inset channel being correspondingly curved.

10. The igniter of claim 1 , wherein the second electrode has a curved surface with a convex orientation toward the first electrode in an area of minimum separation between the first and second electrodes.

11. The igniter of claim 1 , wherein the first electrode is centered at a first axis and the second electrode is centered at a second axis that is radially offset from the first axis.

12. The igniter of claim 1 , wherein said first and second electrodes being of circular cross-section, and the second inset channel is circular or partially circular, running parallel to the first electrode, and sized to receive said second electrode.

13. The igniter of claim 1 , wherein the second electrode is part of a unitary structure coaxially oriented around the first electrode.

14. The igniter of claim 1 , wherein at least one of said first and second electrodes is larger in cross-section above said continuous surface of the insulating member than below said continuous surface.

15. The igniter claim 1 , wherein the at least two electrodes remain parallel for at least 0.250″ below the plasma initiation region.

16. An igniter, comprising:

an insulating member shaped with:

a first inset channel;

second and third inset channels disposed on different respective sides of the first inset channel; and

a surface spacing apart the first, second, and third inset channels;

a first electrode having at least a portion of a length thereof received in the first inset channel below and to the surface of the insulating member;

a second electrode having at least a portion of a length thereof received in the second inset channel below and to the surface of the insulating member; and

a third electrode having at least a portion of a length thereof received in the third inset channel below and to the surface of the insulating member,

wherein:

at least two of the first, second, and third electrodes are configured as an anode and a cathode, respectively; and

the surface of the insulating member defines a plasma initiation region for when a potential is applied to at least the anode and the cathode sufficient to cause breakdown to occur between at least the anode and the cathode.

17. The igniter of claim 16 , wherein the first inset channel is a bore, surrounded by the insulating member, that receives the first electrode, and the first electrode is configured as one of the anode and the cathode.

18. The igniter of claim 16 , wherein:

the first electrode is an inner electrode and configured as one of the anode and the cathode; and

the second and third electrodes are outer electrodes and each configured as anodes or each configured as cathodes.

19. The igniter of claim 16 , wherein:

the first, second, and third electrodes are elongated in a first direction;

the first inset channel is shaped to fully receive surround the first electrode on sides that face in directions perpendicular to the first direction; and

the second inset channel is shaped to surround the second electrode on at least a first side and expose the second electrode on at least a second side, the first and second sides facing in directions perpendicular to the first direction; and

the third inset channel is shaped to surround the third electrode on at least a third side and expose the third electrode on at least a fourth side, the third and fourth sides facing in directions perpendicular to the first direction.

20. The igniter of claim 16 , wherein:

the first, second, and third electrodes are elongated in a first direction;

a cross-section of the second electrode that is normal to the first direction, where the second electrode is received in the second inset channel, has a diameter smaller than the length of the second electrode in the first direction; and

a cross-section of the third electrode that is normal to the first direction, where the third electrode is received in the third inset channel, has a diameter smaller than the length of the third electrode in the first direction.

Assignments (11)
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 072268/0030 →
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 072267/0977 →
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 072268/0018 →
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 Jul 24, 2025
From: KNITE INC.
To: CHAMPION AEROSPACE LLC
Reel/Frame 071823/0238 →
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 Sep 6, 2022
From: SUCKEWER, ARTUR P.
To: KNITE, INC.
Reel/Frame 060995/0063 →
Continuity (7)
Continuation 16722162 · Dec 20, 2019
Continuation 16034173 · Jul 12, 2018
Continuation 15164786 · May 25, 2016
Continuation 14879989 · Oct 9, 2015
Continuation 14234756
Provisional Application 61511592 · Jul 26, 2011
Related Publication 20220173577A1 · Jun 2, 2022