# US 9,038,364 B2 · Thruster grid clear circuits and methods to clear thruster grids > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 9,038,364 B2 - Document ID: US9038364B2 - Status: Granted - Kind: B2 - Application number: 13/655,138 - Filed: 2012-10-18 - Published: 2014-04-24 - Granted: 2015-05-26 - Earliest claimed: 2012-10-18 - Assignees: The Boeing Company - Applicants: The Boeing Company - Inventors: John F. Stickelmaier; Philip D. Nguyen - Web page: https://patentgrep.com/patent/US9038364B2 ## CPC - F03H 1/0043: {characterised by the acceleration grid (extraction optics for ion sources H01J27/024)} - B64G 1/413: {Ion or plasma engines} - F03H: PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR (from combustion products F02K) - B64G: COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR ## Abstract Thruster grid clear circuits and methods to clear thruster grids are disclosed. An example apparatus includes a low voltage grid clear circuit to apply first energy to a grid at a first voltage, and a high voltage grid clear circuit to detect a failure of the applied energy to clear a short circuit condition of the grid and to apply second energy to the grid at a second voltage higher than the first voltage. ## Claims ### Claim 1 An ion propulsion system comprising: a first ion propulsion system thruster grid and a second ion propulsion system thruster grid; and a grid clear circuit for clearing a short circuit between the first ion propulsion system thruster grid and the second ion propulsion system thruster grid, the grid clear circuit comprising: a low-voltage grid clear circuit configured to apply a first energy by applying a first voltage between the first ion propulsion system thruster grid and the second ion propulsion system thruster grid; and a high-voltage grid clear circuit configured to apply a second energy by applying a second voltage between the first ion propulsion system thruster grid and the second ion propulsion system thruster grid, the second voltage being higher than the first voltage. ### Claim 2 (depends on 1) A method of operating the ion propulsion system of claim 1 comprising: measuring a first node voltage in the low-voltage grid clear circuit; and comparing the first node voltage to a threshold voltage to detect the short circuit between the first ion propulsion system thruster grid and the second ion propulsion system thruster grid. ### Claim 3 (depends on 2) The method as defined in claim 2, further comprising: measuring a second node voltage in the low-voltage grid clear circuit; detecting a failure of the first energy to clear the short circuit by comparing a difference between the first node voltage and the second node voltage to a second threshold voltage; and applying the second energy in response to detection of the failure. ### Claim 4 (depends on 1) A method of operating the ion propulsion system of claim 1 comprising: applying a first grid clear process, wherein the first grid clear process comprises applying the first voltage between the first ion propulsion system thruster grid and the second ion propulsion system thruster grid; detecting a failure of the first grid clear process to clear the short circuit; and applying a second grid clear process, wherein the second grid clear process comprises applying the second voltage between the first ion propulsion system thruster grid and the second ion propulsion system thruster grid. ### Claim 5 (depends on 4) The method as defined in claim 4, wherein detecting the failure comprises measuring a first node voltage at a first node of the low-voltage grid clear circuit. ### Claim 6 (depends on 5) The method as defined in claim 5, wherein detecting the failure further comprises: measuring a second node voltage at a second node of the low-voltage grid clear circuit; and detecting the failure of the first grid clear process to clear the short circuit based on comparing a voltage difference between the second node voltage and the first node voltage to a threshold voltage difference, the second grid clear process being applied in response to the detecting of the failure. ### Claim 7 (depends on 4) The method as defined in claim 4, wherein the second grid clear process comprises applying the second voltage between the grids to cause an electrical arc between the first ion propulsion system thruster grid and the second ion propulsion system thruster grid. ### Claim 8 (depends on 7) The method as defined in claim 7, wherein applying the first energy at the first voltage is not sufficient to cause an arc between the first ion propulsion system thruster grid and the second ion propulsion system thruster grid. ### Claim 9 (depends on 4) The method as defined in claim 4, further comprising: while applying the second grid clear process, detecting a current being applied via the first grid clear process; and stopping application of the second grid clear process in response to detecting the current. ### Claim 10 (depends on 9) The method as defined in claim 9, further comprising: detecting that the current has stopped when application of the second grid clear process is stopped; and reapplying the second grid clear process. ### Claim 11 (depends on 4) The method as defined in claim 4, wherein applying the second grid clear process is performed while applying the first grid clear process. ### Claim 12 (depends on 4) The method as defined in claim 4, further comprising: detecting that the low-voltage grid clear circuit is applying the first energy and stopping application of the second energy in response to detecting that the low-voltage grid clear circuit is applying the first energy. ### Claim 13 (depends on 12) The method as defined in claim 12, wherein detecting that the low-voltage grid clear circuit is applying the first energy comprises detecting a voltage drop in the low-voltage grid clear circuit. ### Claim 14 (depends on 1) The ion propulsion system as defined in claim 1, further comprising a third ion propulsion system thruster grid, the grid clear circuit further configured to clear a short circuit between the second ion propulsion system thruster grid and the third ion propulsion system thruster grid.