Spark plug and associated propellant ignition system
AssigneeThe Boeing Company
InventorsLeora Peltz, William Gregory Peterson, Robert V. Frampton
Life of this patent
Estimating the term…
Loading patent…
AssigneeThe Boeing Company
InventorsLeora Peltz, William Gregory Peterson, Robert V. Frampton
Estimating the term…
A spark plug having an insulating body defining a longitudinal axis and including a base portion and an obstruction portion, a first electrode including a proximal portion, a sheathed portion and a distal portion, the sheathed portion of the first electrode extending through the base portion of the insulating body, and a second electrode including a proximal portion, a sheathed portion and a distal portion, the sheathed portion of the second electrode extending through the base portion and the obstruction portion of the insulating body, wherein the obstruction portion axially extends beyond the distal portion of the first electrode.
A spark plug comprising:
A rocket propellant ignition system comprising:
A method for igniting a flowing rocket propellant comprising the steps of:
Dependencies are inferred from the claim text.