초록

A device senses a static charge resulting from the impingement of particles on a surface, such as an aircraft's outer skin. The device includes a sensor adapted to be installed on the surface and a corona guard for guarding against corona discharge from the sensor.

대표청구항 ▼

1. A device comprising: a sensor installed over a surface, the sensor being configured to sense p-static charge accumulation resulting from impingement of particles on the sensor, the sensor including: a first dielectric layer installed directly on the surface;a second dielectric layer installed ove

1. A device comprising: a sensor installed over a surface, the sensor being configured to sense p-static charge accumulation resulting from impingement of particles on the sensor, the sensor including: a first dielectric layer installed directly on the surface;a second dielectric layer installed over a first portion of an electrically conductive layer such that the electrically conductive layer is sandwiched between the first and second dielectric layers, a second portion of the electrically conductive layer being exposed to the particle impingement, and the device further comprising:a corona guard installed over the surface and substantially surrounding the sensor, first edges of the corona guard being spaced from second edges of the electrically conductive layer of the sensor around the second portion, and the corona guard overlying the electrically conductive layer of the sensor outside of the second portion. 2. The device of claim 1, wherein the corona guard includes: an electrically conductive element spaced from and circumscribing the second portion. 3. The device of claim 1, wherein the corona guard substantially surrounds the sensor in one or more planes substantially parallel to the electrically conductive layer. 4. The device of claim 1, further comprising: a heater configured to heat the sensor. 5. The device of claim 4 wherein the heater includes an electrical heating element on the corona guard and coupled with a source of electrical power. 6. The device of claim 1, wherein the corona guard is generally flat and extends outwardly beyond a perimeter of the sensor, and wherein the sensor is generally flat. 7. Apparatus for sensing p-static charge accumulation resulting from the impingement of particle on an aircraft, comprising: a p-static sensor device, including a p-static charge sensor and a corona guard for guarding against corona discharge from the p-static charge sensor, the p-static charge sensor including: a first dielectric layer installed directly on a surface of the aircraft;a second dielectric layer installed over a first portion of an electrically conductive layer such that the electrically conductive layer is sandwiched between the first and second dielectric layers, a second portion of the electrically conductive layer being exposed to the particle impingement, first edges of the corona guard being spaced from second edges of the electrically conductive layer of the sensor around the second portion, and the corona guard overlying the electrically conductive layer of the sensor outside of the second portion, and the device further comprising:means for mounting the p-static sensor device on the aircraft. 8. The apparatus of claim 7, wherein the mounting means includes: a drogue having the static sensor device mounted thereon, anda tether connecting the drogue with aircraft for towing the drogue a preselected distance behind the aircraft. 9. The apparatus of claim 7, wherein the mounting means includes: a module having the static sensor device mounted thereon,the module being removable from the aircraft and forming part of an outer skin of the aircraft. 10. The apparatus of claim 7, wherein the p-static sensor device is mounted within the interior of a fuel tank on the aircraft. 11. The apparatus of claim 7, wherein the mounting means includes: a substrate having the p-static sensor device secured thereto, andfastening means for removably fastening the substrate on the aircraft. 12. The apparatus of claim 7, wherein the mounting means includes a layer of bonding adhesive. 13. A method of measuring a static charge resulting from impingement of particles over an aircraft, the aircraft comprising a p-static charge sensor mounted on a surface of the aircraft, the sensor including a first dielectric layer installed directly on the surface, a second dielectric layer installed over a first portion of an electrically conductive layer such that the electrically conductive layer is sandwiched between the first and second dielectric layers, a second portion of the electrically conductive layer being exposed to impingement of particles, and the sensor further comprising a corona guard installed over the surface and substantially surrounding the sensor, first edges of the corona guard being spaced from second edges of the electrically conductive layer of the sensor around the second portion, and the corona guard overlying the electrically conductive layer of the sensor outside of the second portion, and the method comprising: using the p-static charge sensor to accumulate a static charge on the second portion of the electrically conductive layer resulting from the impingement of particles on the sensor;suppressing corona discharge from the sensor using the corona guard; and,converting the p-static charge accumulation on the sensor into data related to magnitude of the accumulated static charge on surfaces of the aircraft. 14. The method of claim 13, further comprising: sensing the impingement of the particles on the aircraft;analyzing impinging particles; andusing combined results of analysis of the impinging particles and the data to control at least one system on-board the aircraft. 15. The method of claim 14, wherein the analysis of the impinging particles includes analyzing at least one of: a size of the impinging particlesa rate of impingement of the particles, anda density of the impinging particles.