IP Library Granted Patent US 12,627,118
Granted Patent B2
US 12,627,118 · App. 18/705,545 · Granted May 12, 2026

Ignition system and igniter having ruthenium ground electrode and platinum-iridium alloy center electrode

Inventors: Steven J. Cannady (Liberty, SC); Thomas L. Justice (Anderson, SC); George D. Lambrinos (Fountain Inn, SC); Stanley K. Thompson (Liberty, SC)
Assignee: Champion Aerospace LLC
H01T13/39
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Quick Facts
Patent No.
US 12,627,118
App. No.
18/705,545
Granted
May 12, 2026
Kind
B2
Abstract

An igniter for a gas turbine engine has a shell; an insulator secured within said shell; a center electrode secured within said insulator and electrically isolated from said shell by said insulator, said center electrode having a firing tip formed from a platinum-iridium (PtIr) alloy and having a diameter of at least 0.09 inches; and a ground electrode mounting on said shell and terminating at a firing end of the igniter that is spaced from the firing tip by a gap, said ground electrode having at least one pin comprising ruthenium (Ru) or a ruthenium alloy. The igniter is advantageously used with an ignition system having a positive polarity pulse output.

Claims (32)

1 . An igniter for use with a positive polarity exciter of a gas turbine engine, comprising:

a shell;

an insulator secured within said shell;

a center electrode secured within said insulator and electrically isolated from said shell by said insulator, said center electrode having a firing tip formed from a platinum-iridium (PtIr) alloy that accepts electrons from the positive polarity exciter and having a diameter within a range that is about 0.12 inches; and

a ground electrode mounted on said shell and terminating at a firing end of the igniter that is spaced from the firing tip by a gap, said ground electrode having at least one pin comprising ruthenium (Ru) or a ruthenium alloy and having a diameter in the range of 0.022 inches to 0.122 inches.

2 . The igniter of claim 1 , wherein the firing tip has a diameter of 0.11-0.15 inches.

3 . The igniter of claim 1 , wherein the PtIr alloy comprises a mix of platinum and iridium in the range of Pt70Ir30 to Pt99Ir1.

4 . The igniter of claim 1 , wherein the PtIr alloy comprises a mix of platinum and iridium in the range of Pt80Ir20 to Pt95Ir5.

5 . The igniter of claim 1 , wherein the PtIr alloy comprises a mix of platinum and iridium in the range of Pt85Ir15 to Pt95Ir5.

6 . The igniter of claim 1 , wherein the ground electrode comprises a plurality of pins each having a diameter of about 0.072 inches.

7 . The igniter of claim 6 , wherein each of the pins comprises at least 99.9% ruthenium.

8 . An ignition system comprising the igniter of claim 1 .

9 . An igniter for a gas turbine engine, comprising:

a shell;

an insulator secured within said shell;

a center electrode secured within said insulator and electrically isolated from said shell by said insulator, said center electrode having a firing tip formed from a platinum-iridium (PtIr) alloy and having a diameter of at least 0.09 inches; and

a ground electrode mounted on said shell and terminating at a firing end of the igniter that is spaced from the firing tip by a gap, said ground electrode having at least one pin comprising ruthenium (Ru) or a ruthenium alloy;

wherein the firing tip has a diameter of 0.12 inches, the PtIr alloy comprises Pt90Ir10, the pins have a diameter of 0.072 inches, and the ruthenium comprises at least 99.9% ruthenium.

10 . The ignition system of claim 8 , further comprising a positive polarity exciter and an ignition lead connected at one end to the exciter and at another end to the igniter.

11 . The ignition system of claim 10 , wherein:

the PtIr alloy comprises a mix of platinum and iridium in the range of Pt70Ir30 to Pt99Ir1; and

the ground electrode comprises a plurality of pins each comprising at least 99.9% ruthenium and having a diameter in the range of 0.022 inches to 0.122 inches.

12 . An ignition system, comprising:

a unipolar positive polarity exciter that outputs positive polarity spark pulses;

an ignition lead that connects to the exciter to receive and transmit the spark pulses; and

an igniter that connects to the ignition lead to receive the spark pulses from the exciter, wherein the igniter comprises:

a shell;

an insulator secured within said shell;

a center electrode secured within said insulator and electrically isolated from said shell by said insulator, said center electrode having a firing tip formed from a platinum-iridium (PtIr) alloy and having a diameter of at least 0.10 inches; and

a ground electrode mounted on said shell and terminating at a firing end of the igniter that is spaced from the firing tip by a gap, said ground electrode having at least one pin comprising ruthenium (Ru) or a ruthenium alloy;

wherein the center electrode firing tip and at least one ground electrode pin form a spark gap across which electrons from the positive polarity spark pulses are received by the PtIr firing tip from the at least one Ru or Ru-alloy pin; and

wherein the igniter provides an extended service life from a combination of (1) the applied positive polarity spark pulses to the igniter, (2) the use of PtIr alloy for the firing tip, (3) the use of Ru or Ru alloy for the at least one pin, and (4) the firing tip having a diameter of at least 0.10 inches.

Assignments (9)
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 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 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 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 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 14, 2024
From: CANNADY, STEVEN J.; JUSTICE, THOMAS L.; LAMBRINOS, GEORGE D.; THOMPSON, STANLEY K.
To: CHAMPION AEROSPACE LLC
Reel/Frame 067400/0543 →