GB2158939A - Monitoring condition of surface - Google Patents
Monitoring condition of surface Download PDFInfo
- Publication number
- GB2158939A GB2158939A GB08412385A GB8412385A GB2158939A GB 2158939 A GB2158939 A GB 2158939A GB 08412385 A GB08412385 A GB 08412385A GB 8412385 A GB8412385 A GB 8412385A GB 2158939 A GB2158939 A GB 2158939A
- Authority
- GB
- United Kingdom
- Prior art keywords
- optical fibre
- light
- output
- input
- detection
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N21/00—Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
- G01N21/17—Systems in which incident light is modified in accordance with the properties of the material investigated
- G01N21/41—Refractivity; Phase-affecting properties, e.g. optical path length
- G01N21/43—Refractivity; Phase-affecting properties, e.g. optical path length by measuring critical angle
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B19/00—Alarms responsive to two or more different undesired or abnormal conditions, e.g. burglary and fire, abnormal temperature and abnormal rate of flow
- G08B19/02—Alarm responsive to formation or anticipated formation of ice
Abstract
A surface-condition detection and/or monitoring arrangement comprises input and output optical fibres 1,2 having ends terminating in close proximity at the surface 4 being monitored (e.g. aircraft wing surface or rotor blade surface of helicopter). Source 5 applies light signals to the input optical fibre 1 which is so arranged relative to the output optical fibre that light emerging at the surface 4 will be variably reflected and scattered by surface ice, water, oil, etc, into the adjacent end of the output fibre 2. Detection means 8 is provided at the far end of the output fibre for detecting and analysing the light output at different wavelengths to determine and provide an indication of the presence and/or composition of any film on the surface 4. <IMAGE>
Description
SPECIFICATION
Improvements relating to the detection and/ or monitoring of surface conditions
This invention relates to arrangements for detecting and/or monitoring surface conditions.(e.g. ice, water and oil films etc.) and is especially concerned with the detection of ice on the wings or rotor blade surfaces of aircraft.
According to the present invention there is provided a surface-condition detection and/or monitoring arrangement comprising input and output optical fibres having ends thereof terminating in close proximity with one another at the surface concerned (e.g. aircraft wing surface or rotor blade surface of helicopter) means for generating and applying light signals to the input optical fibre which is so arranged relative to the output optical fibre that light emerging from the end of the input optical fibre terminated at said surface, will be variably reflected and scattered by surface ice, water, oil, etc, into the end of the output optical fibre, detection means being provided at the far end of the output fibre for detecting and analysing the light output to determine and provide an indication of surface conditions.
When the surface being monitored is free of ice, water, oil, etc, substantially none of the light emerging from the input optical fibre will enter the output fibre.
One of the principal advantages of the present invention, is that it does not require any part of the detection monitoring arrangement to project from the surface being monitored since the adjacent ends of the input and output optical fibres effectively form part of the surface being monitored. For this reason, the detection arrangement will be less vulnerable to damage than condition detecting arrangements already known.
The optical spectrum of the light output (or part of that spectrum) may by analysed by the analysing means to determine the composition of the surface film producing reflection and scattering of the light.
In order to distinguish between the light transmitted through the optical fibres and the ambient light, the light applied to the fibres may be of periodically-varying intensity in order to provide an alternating component to the light which can be detected by the detector analyser means.
By way of example, the present invention will now be described with reference to the accompanying drawing, in which:
Figures 1 and 2 are diagrams of the optical fibre surface-condition detector arrangement and illustrates the mode of operation of the arrangement.
Referring to Fig. 1, the detector arrangement comprises input and output optical fibres 1 and 2, which in the present example are embodied in a structure 3 which may be the wing of an aircraft. The upper ends of the optical fibres 1 and 2, as viewed in the Figure are terminated adjacent one another and flush with the surface 4 of the structure 3 so that they effectively define a continuation of the surface 4. In operation of the surface-condition detection/monitoring arrangement, the input end of the input optical fibre 1 will have a light signal applied to it from a light source 5. This light signal is preferably of periodically-varying intensity so that the detector arrangement can distinguish positively from ambient light impinging on the arrangement.
This periodically-varying light signal travels along the input fibre 1 until it reaches the end thereof. When the surface 4 is not covered with a transparent or translucent film of water, ice, oil, etc, the light emerging from the end of the fibre 1 defines a light beam 6 which radiates into the atmosphere above the surface 4 so that virtually none of the light beam 6 enters the output fibre 2.
However, in the presence of a film 7 of water, ice or oil, on the surface 4, as shown in Fig. 2, the light beam emerging from the input fibre 1 will be internally reflected by the film 7 so that a significant proportion of the light emerging from the optical fibre 1 enters the end of the output optical fibre 2. This light travels along the output fibre 2 and is detected and analysed at the far en'd of the optical fibre 2 by means of a detector/analyser means 8.
The detector/analyser means 8 serves to analyse the composition of the surface film 7 by making a simple analysis of the optical spectrum (or part of the spectrum) of the transmitted light which may have an alternating component due to the periodic variation of the light intensity. This anlysis serves to determine the degree of light absorption within spectral regions at which the ice, water or oil exhibit significant differences in transmission.
In this connection the principal absorption of light by hydrocarbon oil in the 0.8 to 1.0 ym and 1.2 to 1.6 ym wavelength region of the optical spectrum is due to C-H vibrational absorption and this differs significantly from the absorption spectrum of water in the same regions. Water has different absorption characteristic curves which are due to O-H vibrational absorption. Ice has a slightly different absorption from water due to hydrogen bonding mechanisms which cause alterations in the characteristic O-H absorption.
Thus the detector arrangement can identify the composition of the transparent film (e.g.
water, ice, oil etc); The detection of water at low temperatures may also serve as a warning of the likelihood of ice film formation.
As will readily be apparent from the foregoing description of one embodiment of the invention, the surface-condition detection/ monitoring arrangment has application in many different fields where the presence of water, ice or oil on surfaces can present serious hazards.
Claims (5)
1. A surface condition detection and/or monitoring arrangement comprising input and output optical fibre means having ends thereof terminated in close proximity with one another at the surface concerned, means for generating and applying light signals to the input optical fibre means which is so arranged relative the output optical fibre means that light emerging from the surface terminated end of the input optical fibre means will be variably reflected and scattered by surface ice, water, oil, etc, into the surface-terminated end of the output optical fibre means and detection means provided at the far end of the output optical fibre means for detecting and analysing the light output to determine and provide an indication of surface conditions.
2. A surface condition detection and/or monitoring arrangement as claimed in claim 1, in which the surface ends of the input and output optical fibre means are flush with and effectively form part of the surface being monitored.
3. A surface condition detection and/or monitoring arrangement as claimed in claim 1 or claim 2, in which the detection means analysies the optical spectrum (or part thereof) to determine the composition of the surface film producing reflection and scattering of the light.
4. A surface condition detection and/or monitoring arrangement as claimed in claim 1 or claim 2, in which the light applied to the input optical fibre means is of periodicallyvarying intensity in order to provide an alternating component to the light which can be detected by the detection means.
5. A surface condition detection arrangement substantially as hereinbefore described with reference to the accompanying drawing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08412385A GB2158939B (en) | 1984-05-15 | 1984-05-15 | Improvements relating to the detection and/or monitoring of surface conditions |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08412385A GB2158939B (en) | 1984-05-15 | 1984-05-15 | Improvements relating to the detection and/or monitoring of surface conditions |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2158939A true GB2158939A (en) | 1985-11-20 |
GB2158939B GB2158939B (en) | 1988-06-02 |
Family
ID=10560988
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08412385A Expired GB2158939B (en) | 1984-05-15 | 1984-05-15 | Improvements relating to the detection and/or monitoring of surface conditions |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2158939B (en) |
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2212913A (en) * | 1987-11-28 | 1989-08-02 | Robin Edward Carmic Washington | Ice warning detector |
EP0405625A2 (en) * | 1989-06-26 | 1991-01-02 | The Boeing Company | Laser ice detector |
WO1991014170A1 (en) * | 1990-03-15 | 1991-09-19 | TZN FORSCHUNGS- UND ENTWICKLUNGSZENTRUM UNTERLüSS GMBH | Process for determining the condition of a road surface |
WO1995035493A1 (en) * | 1994-06-20 | 1995-12-28 | Raymond James Noack | Ice and liquid detector |
WO1996013427A1 (en) * | 1994-10-31 | 1996-05-09 | Spar Aerospace Limited | Electro-optic ice detection |
AU681037B2 (en) * | 1994-06-20 | 1997-08-14 | Raymond James Noack | Ice and liquid detector |
EP0801300A2 (en) * | 1996-04-11 | 1997-10-15 | Hoechst Aktiengesellschaft | Device for determining superficial humidity |
US5801647A (en) * | 1995-09-08 | 1998-09-01 | Vaisala Oy | Method and apparatus for measuring road surface conditions |
FR2768122A1 (en) * | 1997-09-09 | 1999-03-12 | Sextant Avionique | OPTICAL DEVICE FOR DETECTION OF ICING CONDITIONS ON AIRCRAFT |
WO2003050778A1 (en) * | 2001-12-05 | 2003-06-19 | Mueller Walter | Optical sensor system for detecting the formation of ice |
US6813020B2 (en) | 2000-04-07 | 2004-11-02 | Airbus France | Device for determining the values of at least one parameter of particles, especially of water droplets |
WO2004110865A1 (en) * | 2003-06-13 | 2004-12-23 | Aerospace Composite Technologies Ltd | Ice detection apparatus and method |
WO2008007142A1 (en) * | 2006-07-14 | 2008-01-17 | Bae Systems Plc | Heat distribution in a distributed lighting apparatus |
WO2011009459A3 (en) * | 2009-07-23 | 2011-05-12 | Liwas Aps | Detection of ice on airfoils |
US7965201B2 (en) | 2003-04-16 | 2011-06-21 | The Boeing Company | Method and apparatus for detecting conditions conducive to ice formation |
RU2446080C1 (en) * | 2010-09-27 | 2012-03-27 | Олег Петрович Ильин | Helicopter rotor blade icing warning indicator |
CN105628654A (en) * | 2016-02-05 | 2016-06-01 | 华中科技大学 | Icing photoelectric sensor and icing measuring device |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101021759B1 (en) | 2003-08-20 | 2011-03-15 | 더 보잉 컴파니 | Methods and systems for detecting icing conditions |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB621489A (en) * | 1943-08-11 | 1949-04-11 | Bendix Aviat Corp | Ice detector means and de-icing means |
GB1289146A (en) * | 1969-10-07 | 1972-09-13 | ||
GB1364845A (en) * | 1970-12-05 | 1974-08-29 | Rotax Ltd | Ice detector |
GB1561667A (en) * | 1976-11-29 | 1980-02-27 | Grumman Aerospace Corp | Electro optical fluid measurement system |
-
1984
- 1984-05-15 GB GB08412385A patent/GB2158939B/en not_active Expired
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB621489A (en) * | 1943-08-11 | 1949-04-11 | Bendix Aviat Corp | Ice detector means and de-icing means |
GB1289146A (en) * | 1969-10-07 | 1972-09-13 | ||
GB1364845A (en) * | 1970-12-05 | 1974-08-29 | Rotax Ltd | Ice detector |
GB1561667A (en) * | 1976-11-29 | 1980-02-27 | Grumman Aerospace Corp | Electro optical fluid measurement system |
Cited By (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2212913A (en) * | 1987-11-28 | 1989-08-02 | Robin Edward Carmic Washington | Ice warning detector |
EP0405625A2 (en) * | 1989-06-26 | 1991-01-02 | The Boeing Company | Laser ice detector |
EP0405625A3 (en) * | 1989-06-26 | 1991-06-05 | The Boeing Company | Laser ice detector |
WO1991014170A1 (en) * | 1990-03-15 | 1991-09-19 | TZN FORSCHUNGS- UND ENTWICKLUNGSZENTRUM UNTERLüSS GMBH | Process for determining the condition of a road surface |
US5218206A (en) * | 1990-03-15 | 1993-06-08 | TZN Forschungz- und Entwicklungszentrum Unterluss GmbH | Method for determining the condition of a roadway surface |
WO1995035493A1 (en) * | 1994-06-20 | 1995-12-28 | Raymond James Noack | Ice and liquid detector |
AU681037B2 (en) * | 1994-06-20 | 1997-08-14 | Raymond James Noack | Ice and liquid detector |
WO1996013427A1 (en) * | 1994-10-31 | 1996-05-09 | Spar Aerospace Limited | Electro-optic ice detection |
US5801647A (en) * | 1995-09-08 | 1998-09-01 | Vaisala Oy | Method and apparatus for measuring road surface conditions |
EP0801300A2 (en) * | 1996-04-11 | 1997-10-15 | Hoechst Aktiengesellschaft | Device for determining superficial humidity |
EP0801300A3 (en) * | 1996-04-11 | 1998-03-11 | Clariant GmbH | Device for determining superficial humidity |
US6091335A (en) * | 1997-09-09 | 2000-07-18 | Sextant Avionique | Optical device for the detection of icing conditions on aircraft |
FR2768122A1 (en) * | 1997-09-09 | 1999-03-12 | Sextant Avionique | OPTICAL DEVICE FOR DETECTION OF ICING CONDITIONS ON AIRCRAFT |
US6813020B2 (en) | 2000-04-07 | 2004-11-02 | Airbus France | Device for determining the values of at least one parameter of particles, especially of water droplets |
WO2003050778A1 (en) * | 2001-12-05 | 2003-06-19 | Mueller Walter | Optical sensor system for detecting the formation of ice |
US7965201B2 (en) | 2003-04-16 | 2011-06-21 | The Boeing Company | Method and apparatus for detecting conditions conducive to ice formation |
WO2004110865A1 (en) * | 2003-06-13 | 2004-12-23 | Aerospace Composite Technologies Ltd | Ice detection apparatus and method |
US7586419B2 (en) | 2003-06-13 | 2009-09-08 | Gkn Aerospace Services Limited | Ice detection apparatus and method |
WO2008007142A1 (en) * | 2006-07-14 | 2008-01-17 | Bae Systems Plc | Heat distribution in a distributed lighting apparatus |
US7780328B2 (en) | 2006-07-14 | 2010-08-24 | Bae Systems Plc | Heat distribution in a distributed lighting apparatus |
WO2011009459A3 (en) * | 2009-07-23 | 2011-05-12 | Liwas Aps | Detection of ice on airfoils |
CN102753818A (en) * | 2009-07-23 | 2012-10-24 | 利瓦斯有限责任公司 | Detection of ice on airfoils |
RU2446080C1 (en) * | 2010-09-27 | 2012-03-27 | Олег Петрович Ильин | Helicopter rotor blade icing warning indicator |
CN105628654A (en) * | 2016-02-05 | 2016-06-01 | 华中科技大学 | Icing photoelectric sensor and icing measuring device |
Also Published As
Publication number | Publication date |
---|---|
GB2158939B (en) | 1988-06-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |