GB820592A - Whirling icing detector - Google Patents
Whirling icing detectorInfo
- Publication number
- GB820592A GB820592A GB15420/57A GB1542057A GB820592A GB 820592 A GB820592 A GB 820592A GB 15420/57 A GB15420/57 A GB 15420/57A GB 1542057 A GB1542057 A GB 1542057A GB 820592 A GB820592 A GB 820592A
- Authority
- GB
- United Kingdom
- Prior art keywords
- probe
- probes
- icing
- contacts
- lamp
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000000523 sample Substances 0.000 abstract 11
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/20—Means for detecting icing or initiating de-icing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Measuring Fluid Pressure (AREA)
Abstract
820,592. Detecting icing conditions. NATIONAL RESEARCH COUNCIL. May 15, 1957 [May 24, 1956], No. 15420/57. Class 97(3) [Also in Group XXXIII] A device for detecting icing conditions comprises two orifice type probes mounted to move in a circular path, one being continuously heated to prevent ice formation, a pressure switch being connected between the probes to be operated when the pressure in the unheated probe falls below a predetermined amount. In the form shown the probes 2 and 1, of which the former is continuously heated by a coil 8 energized from a source 19, are carried on an arm 3 rotated about an axis 4. The probes may be as described in Specification 739,527 and are connected by conduits 14, 15 to spaces 27, 27 on either side of a diaphragm 25 with which are associated contacts 12, 13. The orifices in the probe 1 are arranged to provide a greater pressure in the probe than those in the probe 2 so that the contacts 12, 13 are normally open but, if icing occurs on the probe 1, they close to give a warning indication on a lamp 20 and energize a heating coil 7 for the probe 1. Slip rings 16, 17, 18 provide electrical contacts to the rotating parts. A relay may be inserted in series with the lamp 20 to operate the main de-icing equipment e.g. of a helicopter on the rotor of which the probes may be mounted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US820592XA | 1956-05-24 | 1956-05-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB820592A true GB820592A (en) | 1959-09-23 |
Family
ID=22168785
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15420/57A Expired GB820592A (en) | 1956-05-24 | 1957-05-15 | Whirling icing detector |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB820592A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112373689A (en) * | 2020-11-02 | 2021-02-19 | 中国航天空气动力技术研究院 | Aeromagnetic geophysical prospecting unmanned aerial vehicle wing tip mounting device with adjustable posture |
CN114132512A (en) * | 2022-02-07 | 2022-03-04 | 中国空气动力研究与发展中心低速空气动力研究所 | Optical fiber icing sensor probe and adjusting method |
-
1957
- 1957-05-15 GB GB15420/57A patent/GB820592A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112373689A (en) * | 2020-11-02 | 2021-02-19 | 中国航天空气动力技术研究院 | Aeromagnetic geophysical prospecting unmanned aerial vehicle wing tip mounting device with adjustable posture |
CN114132512A (en) * | 2022-02-07 | 2022-03-04 | 中国空气动力研究与发展中心低速空气动力研究所 | Optical fiber icing sensor probe and adjusting method |
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