IPC분류정보
| 국가/구분 |
United States(US) Patent
등록
|
| 국제특허분류(IPC7판) |
|
| 출원번호 |
US-0568793
(2003-08-20)
|
| 등록번호 |
US-8711008
(2014-04-29)
|
| 국제출원번호 |
PCT/US03/26403
(2003-08-20)
|
| §371/§102 date |
20080527
(20080527)
|
| 국제공개번호 |
WO2005/020175
(2005-03-03)
|
|
발명자
/ 주소 |
- Cook, Donald E.
- Feider, Michael P.
|
| 출원인 / 주소 |
|
| 대리인 / 주소 |
|
| 인용정보 |
피인용 횟수 :
6 인용 특허 :
103 |
초록
▼
Methods and systems for detecting icing or incipient icing conditions external to a vehicle (100) are disclosed. An apparatus in accordance with one embodiment of the invention includes a temperature sensor (120) configured to direct a first signal corresponding to a temperature of an airstream, and
Methods and systems for detecting icing or incipient icing conditions external to a vehicle (100) are disclosed. An apparatus in accordance with one embodiment of the invention includes a temperature sensor (120) configured to direct a first signal corresponding to a temperature of an airstream, and a water content sensor (130) configured to direct a second signal corresponding to a water content of the airstream. A processing unit (140) can receive the first and second signals and, based on at least the first and second signals, provide an indication (150) when at least the first and second signals taken together correspond to an at least incipient icing condition. Accordingly, the system can be installed on aircraft to provide notice to the crew of incipient or existing icing conditions.
대표청구항
▼
1. A system for detecting icing conditions external to a vehicle, comprising: a housing carried by the vehicle and positioned external to the vehicle and having a straight flow channel positioned along a straight flow axis external to the vehicle, the straight flow channel having an entrance and an
1. A system for detecting icing conditions external to a vehicle, comprising: a housing carried by the vehicle and positioned external to the vehicle and having a straight flow channel positioned along a straight flow axis external to the vehicle, the straight flow channel having an entrance and an exit positioned to receive an airstream;a probe positioned in the straight flow channel, along the straight flow axis, external to the vehicle, and having a first surface positioned to face toward the airstream as the airstream travels along the straight flow axis, the probe further having a second surface facing opposite from the first surface;a temperature sensor positioned in the housing, mounted to the probe and positioned in the flow channel along the straight flow axis between the entrance and the exit, the temperature sensor being positioned to face downstream at least proximate to the second surface of the probe, the temperature sensor being configured to direct a first signal corresponding to a temperature of the airstream;a water content sensor positioned in the housing, mounted to the probe and positioned in the flow channel along the straight flow axis between the entrance and the exit, the water content sensor being configured to direct a second signal corresponding to a water content of the airstream; anda processing unit coupled to the temperature sensor and the water content sensor to receive the first and second signals and, based on at least the first and second signals, provide an indication when at least the first and second signals taken together correspond to an at least incipient icing condition. 2. The system of claim 1 wherein the water content sensor includes at least one of a liquid water content sensor, a total water content sensor and an ice crystal sensor. 3. The system of claim 1 wherein the temperature sensor, the water content sensor and the processing unit are configured to mount to an aircraft. 4. The system of claim 1 wherein the water content sensor includes a heated wire positioned to be impinged by water contained in the airstream. 5. The system of claim 1 wherein the processing unit is configured to provide a positive indication of an at least incipient icing condition when the temperature sensor detects a temperature corresponding to a static temperature at or below a local freezing point for water, and the water content sensor detects liquid water. 6. The system of claim 1 wherein the temperature sensor is configured to detect a total temperature of the airstream. 7. The system of claim 1 wherein the temperature sensor is configured to detect a total temperature of the airstream, and wherein the processing unit is configured to determine a static temperature of the airstream based at least in part on the first signal. 8. The system of claim 1 wherein the processing unit is operatively couplable to a pressure sensor to receive a third signal corresponding to a pressure of the airstream, and wherein the processing unit is configured to provide the indication based on the first, second and third signals. 9. The system of claim 1, further comprising an aircraft having a fuselage portion, a wing portion, an empennage portion and a propulsion system, and wherein each of the temperature sensor, the water content sensor and the processing unit is carried by at least one of the fuselage portion, the wing portion, the empennage portion and the propulsion system. 10. A system for detecting icing conditions external to a vehicle, comprising: a housing carried by the vehicle and positioned external to the vehicle and having a straight flow channel positioned along a straight flow axis external to the vehicle, the flow channel having an entrance and an exit positioned to receive an airstream;a probe positioned in the straight flow channel, along the straight flow axis external to the vehicle and having a first surface positioned to face toward the airstream as the airstream travels along the straight flow axis, the probe further having a second surface facing opposite from the first surface;temperature sensing means positioned in the straight flow channel and configured to sense a temperature of an airstream and direct a first signal corresponding to the temperature, the temperature sensing means being mounted to the probe and positioned in the straight flow channel along the straight flow axis between the entrance and the exit, the temperature sensing means being positioned to face downstream at least proximate to the second surface of the probe;water content sensing means positioned in the housing, mounted to the probe and positioned in the straight flow channel along the straight flow axis between the entrance and the exit, the water content sensing means being configured to sense a water content of the airstream and direct a second signal corresponding to the water content; andprocessing means coupled to the temperature sensing means and the water content sensing means and configured to receive the first and second signals and, based at least on the first and second signals, provide an indication when at least the first and second signals taken together correspond to an at least incipient icing condition. 11. The system of claim 10 wherein the temperature sensing means, the water content sensing means and the processing means are configured to mount to an aircraft. 12. The system of claim 10 wherein the processing means is configured to provide a positive indication of an at least incipient icing condition when the temperature sensing means detects a temperature corresponding to a static temperature at or below a local freezing point for water, and the water content sensing means detects liquid water. 13. A method for detecting icing conditions external to a vehicle, comprising: receiving signals from a device carried external to the vehicle, the device including:a housing carried by the vehicle and positioned external to the vehicle and having a straight flow channel positioned along a straight flow axis external to the vehicle, the flow channel having an entrance and an exit positioned to receive an airstream;a probe positioned in the straight flow channel, along the straight flow axis external to the vehicle, and having a first surface positioned to face toward the airstream as the airstream travels along the straight flow axis, the probe further having a second surface facing opposite from the first surface;a temperature sensor positioned in the housing, mounted to the probe and positioned in the straight flow channel along the straight flow axis between the entrance and the exit, the temperature sensor being positioned to face downstream at least proximate to the second surface of the probe, and being configured to direct a first signal corresponding to a temperature of the airstream;a water content sensor positioned in the housing, mounted to the probe and positioned in the straight flow channel along the straight flow axis between the entrance and the exit, the water content sensor being configured to direct a second signal corresponding to a water content of the airstream, wherein receiving signals includes receiving a first signal from the temperature sensor corresponding to a temperature of an airstream external to a vehicle;receiving a second signal from the water content sensor corresponding to a water content of the airstream; andbased on at least the first and second signals, automatically generating an indication when at least the first and second signals taken together correspond to an at least incipient icing condition. 14. The method of claim 13 wherein receiving the second signal includes receiving the second signal from at least one of a liquid water content sensor, a total water content sensor and an ice crystal sensor. 15. The method of claim 13 wherein the processes of receiving the first signal, receiving the second signal and automatically generating an indication of claim are performed on board an aircraft. 16. The method of claim 13, further comprising: determining when the temperature sensor detects a temperature corresponding to a static temperature at or below a local freezing point for water;determining when the water content sensor detects liquid water; andgenerating the indication only when both the temperature sensor detects a temperature corresponding to a static temperature at or below a local freezing point for water and the water content sensor detects liquid water. 17. The method of claim 13 wherein receiving a first signal includes receiving a first signal corresponding to a total temperature of the airstream, and wherein the method further comprises determining a static temperature of the airstream based at least in part on the first signal. 18. The method of claim 13, further comprising: receiving a third signal corresponding to a pressure of the airstream; anddetermining whether the first signal corresponds to a temperature at or below which water freezes, based on the first signal and the third signal. 19. The system of claim 1 wherein the temperature sensor includes a static temperature sensor. 20. The system of claim 1 wherein the flow axis is a straight flow axis between the entrance and the exit.
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