IP Library Granted Patent US 9,915,207
Granted Patent B2
US 9,915,207 · App. 14/386,656 · Granted Mar 13, 2018

Ignition unit for turbojet engine

Inventors: Christian Schaeffer (Moissy-Cramayel, FR); David Gino Stifanic (Moissy-Cramayel, FR); Bertrand Boedot (Moissy-Cramayel, FR)
Assignee: SNECMA
F02C7/266F02P15/003F02P15/02F02P3/0807F02P5/1512
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Quick Facts
Patent No.
US 9,915,207
App. No.
14/386,656
Granted
Mar 13, 2018
Kind
B2
Abstract

An ignition unit for a turbojet engine, including: an electrical power supply, a single control channel to receive a control signal from a computer, a main sparkplug ignition channel to energize at least one main sparkplug of a main combustion chamber, and an afterburner sparkplug ignition channel to energize at least one afterburner sparkplug of an afterburner chamber. The ignition unit is configured, in response to pulsed controls on the single control channel, to selectively activate the main sparkplug ignition channel or the afterburner sparkplug ignition channel.

Claims (35)

1. An ignition unit for a turbojet engine, comprising:

an electric power supply;

a single control channel for receiving a control signal from a computer, said control signal comprising pulses of different pulse durations;

a main spark plug ignition channel dedicated to at least one main spark plug of a main combustion chamber for energizing said at least one main spark plug;

an afterburning spark plug channel dedicated to at least one afterburning spark plug of a post combustion chamber for energizing said at least one afterburning spark plug; and

a control module for decoding the control signal received on the single control channel based on the pulse durations of the pulses of the control signal received on the single control channel, said control signal controlling a selective activation of the main spark plug channel or the afterburning spark plug channel,

wherein in response to pulses of the control signal on the single control channel, the control module of the ignition unit is configured to selectively and independently activate the main spark plug channel, or the afterburning spark plug channel, depending on pulse durations of the pulses of the control signal received on the single control channel.

2. The ignition unit for a turbojet engine according to claim 1 , wherein the pulse duration of a pulse of the control signal for controlling activation of an ignition channel depends on required energy for energizing the spark plug corresponding to the ignition channel.

3. The ignition unit according to claim 1 , wherein the control signal has a time-out after each pulse of the control signal, the time-out corresponding to a signal level different from a signal level of the pulse and being followed by a continuous command at a signal level corresponding to the signal level of the pulse.

4. The ignition unit for a turbojet engine according to claim 1 , further comprising an electric power supply channel common to the ignition channel of the main spark plug and to the afterburning spark plug ignition channel, the common electric power supply channel comprising a single capacitive block configured to be brought to a voltage depending on the ignition channel to be activated.

5. The ignition unit for a turbojet engine according to claim 4 , wherein each of the ignition channels includes a thyristor connected to the single capacitive block, the thyristor being controlled depending on a state of the common electric power supply channel and on the pulses of the control signal.

6. The ignition unit according to claim 4 , configured to begin charging the capacitive block as soon as a pulse has been detected and before determining the ignition channel to be activated.

7. The ignition unit according to claim 1 , configured, in response to a control on the single control channel, to alternately activate the main spark plug ignition channel and the afterburning spark plug ignition channel.

8. An ignition system for a turbojet engine, comprising:

an ignition unit comprising:

a single control channel for receiving a control signal from a computer, said control signal comprising pulses of different pulse durations;

a main spark plug ignition channel dedicated to at least one main spark plug of a main combustion chamber for energizing said at least one main spark plug;

an afterburning spark plug channel dedicated to at least one afterburning spark plug of a post combustion chamber for energizing said at least one afterburning spark plug; and

a control module for decoding the control signal received on the single control channel based on the pulse durations of the pulses of the control signal received on the single control channel, said control signal controlling a selective activation of the main spark plug channel or the afterburning spark plug channel,

wherein in response to pulses of the control signal on the single control channel, the control module of the ignition unit is configured to selectively and independently activate the main spark plug channel, or the afterburning spark plug channel, depending on the pulse durations of the pulses of the control signal received on the single control channel;

a main spark plug of a main combustion chamber which may be energized through the main spark plug ignition channel of the ignition unit;

an afterburning spark plug which may be energized through the afterburning spark plug ignition channel of the ignition unit, and

the computer connected to the single control channel of the ignition unit for sending a control signal to the ignition unit.

9. A method of operating an ignition system for a turbojet engine, the ignition system comprising:

an ignition unit comprising:

a single control channel for receiving a control signal from a computer, said control signal comprising pulses of different pulse durations;

a main spark plug ignition channel dedicated to at least one main spark plug of a main combustion chamber for energizing said at least one main spark plug;

an afterburning spark plug channel dedicated to at least one afterburning spark plug of a post combustion chamber for energizing said at least one afterburning spark plug; and

a control module for decoding the control signal received on the single control channel based on the pulse durations of the pulses of the control signal received on the single control channel, said control signal controlling a selective activation of the main spark plug channel or the afterburning spark plug channel,

wherein in response to pulses of the control signal on the single control channel, the control module of the ignition unit is configured to selectively and independently activate the main spark plug channel, or the afterburning spark plug channel, depending on the pulse durations of the pulses of the control signal received on the single control channel;

a main spark plug of a main combustion chamber which may be energized through the main spark plug ignition channel of the ignition unit;

an afterburning spark plug which may be energized through the afterburning spark plug ignition channel of the ignition unit; and

the computer connected to the single control channel of the ignition unit for sending a control signal to the ignition unit, the method comprising:

decoding, using the control module, the control signal received on the single control channel based on the pulse durations of the pulses of the control signal received on the single control channel, and in response to pulsed controls on said single control channel; and

selectively and independently activating the main spark plug channel, or the afterburning spark plug channel, depending on the pulse durations of the pulses of the control signal received on the single control channel.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 21, 2014
From: SCHAEFFER, CHRISTIAN; STIFANIC, DAVID GINO; BOEDOT, BERTRAND
To: SNECMA
Reel/Frame 033987/0757 →
Priority Claims (1)
FR 12 52648 · Mar 23, 2012 · national
Continuity (1)
Related Publication 20150033699A1 · Feb 5, 2015