GB2198529A - Optical pyrometer - Google Patents
Optical pyrometer Download PDFInfo
- Publication number
- GB2198529A GB2198529A GB08727759A GB8727759A GB2198529A GB 2198529 A GB2198529 A GB 2198529A GB 08727759 A GB08727759 A GB 08727759A GB 8727759 A GB8727759 A GB 8727759A GB 2198529 A GB2198529 A GB 2198529A
- Authority
- GB
- United Kingdom
- Prior art keywords
- optical radiation
- radiation sensor
- sensor apparatus
- casing
- detector
- 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
- 230000003287 optical effect Effects 0.000 title claims abstract description 40
- 230000005855 radiation Effects 0.000 claims abstract description 46
- 238000012545 processing Methods 0.000 claims abstract description 31
- 238000012546 transfer Methods 0.000 claims abstract description 9
- 230000003750 conditioning effect Effects 0.000 claims abstract description 7
- 230000013011 mating Effects 0.000 claims abstract description 5
- 239000000446 fuel Substances 0.000 claims abstract description 4
- 239000007788 liquid Substances 0.000 claims abstract description 4
- 238000000034 method Methods 0.000 claims abstract description 4
- 239000013307 optical fiber Substances 0.000 claims description 4
- 239000012809 cooling fluid Substances 0.000 claims description 3
- 230000000717 retained effect Effects 0.000 claims description 2
- 239000002184 metal Substances 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000013500 data storage Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
- G01J5/10—Radiation pyrometry, e.g. infrared or optical thermometry using electric radiation detectors
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
- G01J5/02—Constructional details
- G01J5/08—Optical arrangements
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
- G01J5/02—Constructional details
- G01J5/08—Optical arrangements
- G01J5/0818—Waveguides
- G01J5/0821—Optical fibres
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
- G01J5/60—Radiation pyrometry, e.g. infrared or optical thermometry using determination of colour temperature
- G01J2005/607—Radiation pyrometry, e.g. infrared or optical thermometry using determination of colour temperature on two separate detectors
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Radiation Pyrometers (AREA)
Abstract
An optical pyrometer for a gas-turbine engine has a radiation receiving head 1 located to view the blades 2 of the engine and supply radiation from the blades to one end of a fibre-optic cable 4. At the other end of the cable there is mounted a detector 3 comprising a cylindrical metal casing containing a photodiode and a signal conditioning circuit that amplifies the photodiode output. The output of the circuit is supplied to a connector 32 mounted on the casing. The detector 3 can be mounted directly on the casing 53 of a processing unit 5 by mating its connector 32 with a connector 52 fixed on the processing unit casing thereby avoiding the need for cables between the two casings. The connector 32 on the detector 3 has a flange that provides good thermal contact with the connector 52 on the processing unit casing so as to help equalise the temperatures of the two casings. The processing unit casing 53 is cooled by means of a thermal transfer unit 60 suppled with liquid fuel. The processing unit 5 has an electrical circuit 54 that processes the output of the detector circuit and inputs 56 from other sources to provide an output 57 to an engine control unit 6. Two photodiodes responsive to different wavelengths may be employed. <IMAGE>
Description
OPTICAL R & IATION SENSOR APPARATUS
This invention relates to optical radiation sensor apparatus.
The invention is more especially, but not exclusively, concerned with optical pyrometer apparatus.
Optical pyrometer apparatus are used for measuring high temperatures in for example, gas-turbine engines and furnaces. The pyrometer apparatus includes a radiation receiving head, a radiation detector which produces an electrical output, a preamplifer for amplifying the detector output, and utilising apparatus for scaling, comparison and calculation on the preamplified output of the detector to provide an output suitable-for display of temperature, data storage, performance of a control function and so on.
The radiation detector may be contained in the receiving head so that an electrical output is produced, but there are advantages to mounting the detector remotely and interconnecting the detector and receiving head by a flexible radiation guide, such as a fibre-optic cable. In this way, the detector can be mounted at a cooler location. Such fibre-optic pyrometers, therefore comprise -three separate units: the pyrometer head; the detector and preamplifier or other signal conditioning unit; and the utilising apparatus.
The pyrometer head is connected to the detector by a fibre-optic cable: the detector is connected to the utilisation apparatus by an electrical cable
Other similar optical radiation sensor apparatus are also divided into three units interconnected by cables.
Such apparatus has several disadvantages. The- electrical cable and connectors between the detector and utilisation apparatus adds to the overall weight of the pyrometer, especially where the cable is screened which is usually necessary in aircraft applications. The cable and connectors can also be susceptible to electromagnetic interference. The detector must also be clamped, screwed or otherwised secured in place, making installation more difficult.
It is an object of the present invention to provide optical radiation sensor apparatus with advantages over previous apparatus.
According to one aspect of the present invention there is provided optical radiation sensor apparatus comprising an optical radiation receiving head arranged to receive radiation; optical radiation guide means having one end coupled with the receiving head, said guide means being arranged to transmit radiation from the receiving head; optical detector assembly including a first rigid casing enclosing an optical radiation detector device and electrical signal conditioning means having an input connected with the detector device and an output connected with a first mateable connector device on said casing; and a processing unit including a second rigid casing containing electrical circuit means having an input connected with a second mateable connector device on the second casing, said circuit means being arranged to process the output of the detector assembly, said second connector device being adapted to mate and engage directly with the first connector device such that the optical detector assembly can be connected with the processing unit without the interposition of any cable between the respective casings.
The detector assembly is preferably retained on the processing unit substantially solely by mating of the first and second connector devices. The first rigid casing may be of substantially cylindrical shape. The first mateable connector device may be secured with the first casing by means of cooperating screw threads on the connector device and casing. The electrical signal conditioning means preferably includes amplifier means arranged to amplify the output of the detector device. The guide means may include an optical fibre cable. The receiving head may include converging lens means arranged to focus radiation onto an end of the optical fibre cable and the detector device may include a photodiode.
The first and second connector devices are preferably arranged to be in good thermal contact with one another when mated such as to promote equalisation of the temperatures of the first and second casings. The first connector device may be provided with an annular flange that is arranged to contact a surface on the second connector device so as to provide good thermal contact between the two connector devices. Thermal transfer means may be associated with the second casing and the thermal transfer means may be supplied with a cooling fluid such as liquid fuel. The optical radiation detector device may be thermally insulated from the first casing. The processing unit may be arranged to receive input signals from other sources.
The apparatus may be a pyrometer and the output of the processing unit may be supplied to an engine control unit.
Pyrometer apparatus for a gas-turbine engine in accordance with the present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
Figure 1 illustrates the pyrometer apparatus
installed on a gas-turbine engine;
Figure 2 is a sectional view of a part of the
apparatus; and
Figure 3 shows the electronic components of the
apparatus schematically.
With reference first to Figure 1, the pyrometer apparatus comprises a pyrometer head 1, mounted to view the blades 2 of a gas-turbine engine, a detector 3 connected with the pyrometer head by means of a cable 4, and a processing unit 5 which receives the detector output and provides a signal related to temperature and other parameters to an engine control unit 6.
The pyrometer head 1 is of conventional construction, such as described in GB 2158576A or GB 1589531, having a heat-resistant converging lens 10 mounted towards the rear of a sighting tube 11. The lens 10 focuses radiation emitted by the blades 2, which enters the sighting tube 11, onto the forward end 40 of the cable 4. The cable 4 is a fibre-optic cable, or some similar optical radiation guide, and is flexible or bendable so that there is freedom in the mounting of the pyrometer head 1 and detector 3. The cable 4 may be armoured for protection and is long enough to enable the detector 3, at the rear end 41 of the cable, to be located at a cooler region.
With reference now to Figure 2, the detector has a cylindrial casing 30 formed by a forward part 31 and rear connector or plug assembly 32. The forward part 31 comprises an inner sleeve 33 welded to the rear end of the cable termination 41, and an outer sleeve 34, the forward end of which engages a shoulder 35 on the inner sleeve and the rear end of which is joined to the plug assembly 32. The overall length of the detector 3 is 60mum and it has a diameter of 20mm. Within the forward part 31 of the detector 3 there are mounted one or more photodiodes 36 which receive radiation emitted from the rear end termination 41 of the cable 4. The photodiode 36 is supported in the inner sleve 33 by a heat insulating support ring 42.A self-regulating heating element (not shown) may be mounted close to the photodiode to enable its temperature to be raised when necessary.
The electrical output of the photodiode 36 is supplied to an electrical circuit assembly 37 within the casing 30 which is shown in greater detail in
Figure 3.
The circuit assembly 37 includes an amplifier 38 which produces a voltage output proportional to the current output of the photodiode 36. This voltage is amplified at a gain stage 39. A circuit 50 may be included for removing signals produced by extraneous flames within the engine. In general, the circuit assembly 37 produces electrical signal conditioning of the output of the photodiode 36 into a form suitable for handling by the processing unit 5. The signals at the output of the circuit assembly 37 are supplied via lines 51 to the plug assembly 32 formed at the rear end of the detector casing 30. The plug assembly 32 is a multi-pin plug-in mateable connector and includes pins by which electrical power is supplied to the circuit assembly 37. The plug assembly 32 has a radially extending flange 43 that is embraced by an outer, threaded locking ring 44.
The plug assembly 32 on the detector 3 is arranged to mate directly with a cooperating connector 52 on the casing 53 of the processing unit 5. The connector 52 has a flat surface (not shown) against which the flange 43 on the connector 32 is abutted in good thermal contact. The processing unit 5 contains electronic processing circuits, indicated generally by the numeral 54. These circuits are connected to the connector 52 so as to receive the signal conditioned output of the photodiode 36 in the detector 3. The processing unit also receives inputs on lines 56 from various other sensors and control devices indicative of, for example, speed, temperature and pressure, and provides an output to the engine control unit 6.The processing unit 5 includes a thermal transfer unit 60 mounted on its casing 53 which is supplied with a fluid, such as liquid fuel, to effect heat transfer, and, more particularly, cooling of the processing unit 5.
One typical method of measuring temperature involves comparing the radiation levels at two different wavelengths. In such an arrangement, the detector would include two photodiodes responsive to the respective two wavelengths. The two outputs produced may either be compared by circuitry in the detector 3 itself, or in the processing unit 5.
The output of the processing unit 5 is supplied by a cable 57 to the engine control unit 6 which provides control of various engine functions. The output of the processing unit 5 may additionally, or alternatively, be supplied to some other form of utilisation means 6' such as, for example, a data recorder or a display.
The arrangement of the present invention, by having a connector 32 on the casing of the detector 3 that is directly mateable with a connector 52 on the casing 53 of the processing unit 5, without the interposition of any cable between the two casings, leads to a very compact arrangement and is less susceptible to electrical noise and other electromagnetic interference. By avoiding the need for a cable between the casings of the detector and processing unit, the overall weight of the apparatus can be kept to a minimum.
The detector is directly mounted on the processing unit thereby facilitating installation and maintenance. In this respect, the mating connectors on the detector and processing unit may be locking connectors which are sufficient in themselves to support the detector 3.
Because the mating connectors 32 and 52 are in good thermal contact, via the flange 43, any external heating of the detector 3 can be dissipated efficiently via the casing 53 of the processing unit 5 and the thermal transfer unit 60. This reduces the risk of overheating the photodiode 36 which is further reduced by the heat insulating ring 42. Where the apparatus is used in an environment that is below the optimum temperature of the photodiode 36,the thermal transfer unit 60 can be used to raise the temperature of the detector 3, and the heating element (not shown) used to raise the temperature of the photodiode 36 directly.
In severe temperature environments, the temperature of the detector 3 can be maintaned more stable by means of a protective shroud around the detector, separated from the outer sleeve 34 by an air gap. This is especially effective where the detector is located in a stream of flowing gas at extreme temperature.
Claims (19)
1. Optical radiation sensor apparatus comprising an optical
radiation receiving head arranged to receive radiation; optical
radiation guide means having one end coupled with the receiving
head, said guide means being arranged to transmit radiation from the
receiving head; optical detector assembly including a first rigid
casing enclosing an optical radiation detector device and electrical
signal conditioning means having an input connected with the
detector device and an output connected with a first mateable
connector device on said casing; and a processing unit including a
second rigid casing containing electrical circuit means having an
input connected with a second mateable connector device on the
second casing, said circuit means being arranged to process the
output of the detector assembly, said second connector device being
adapted to mate and engage directly with the first connector device
such that the optical detector assembly can be connected with the
processing unit without the interposition of any cable between the
respective casings.
2. Optical radiation sensor appparatus according to Claim 1,
wherein the detector assembly is retained on the processing unit
substantially solely by mating of the first and second connector
devices.
3. Optical radiation sensor apparatus according to Claim 1 or 2,
wherein the first rigid casing is of substantially cylindrical
shape.
4. Optical radiation sensor apparatus according to Claim 3,
wherein said first mateable connector device is secured with said
first casing by means of cooperating screw threads on the connector
device and casing.
5. Optical radiation sensor apparatus according to any one of the
preceding claims, wherein the said electrical signal conditioning
means includes amplifier means arranged to amplify the output of the
detector device.
6. Optical radiation sensor apparatus according to any one of the
preceding claims, wherein the guide means includes an optical fibre
cable.
7. Optical radiation sensor apparatus according to Claim 6,
wherein the said receiving head includes converging lens means
arranged to focus radiation onto an end of said optical fibre cable.
8. Optical radiation sensor apparatus according to any one of the
preceding claims, wherein the said detector device includes a
photodiode.
9. Optical radiation sensor apparatus according to any one of
the preceding claims, wherein the said first and second connector
devices are arranged to be in good thermal contact with one another
when mated such as to promote equalisation of the temperatures of
the first and second casings.
10. Optical radiation sensor apparatus according to Claim 9,
wherein the said first connector device is provided with an annular
flange that is arranged to contact a surface on the second connector
device so as to provide good thermal contact between the two
connector devices.
11. Optical radiation sensor apparatus according to Claim 9 or
10, including thermal transfer means associated with said second
casing.
12. Optical radiation sensor apparatus according to Claim 11,
wherein the thermal transfer means is supplied with a cooling fluid.
13. Optical radiation sensor apparatus according to Claim 12,
wherein the cooling fluid is liquid fuel.
14. Optical radiation sensor appparatus according to any one of
the preceding claims, wherein the optical radiation detector device
is thermally insulated from the first casing.
15. Optical radiation sensor apparatus according to any one of the
preceding claims, wherein the said processing unit is arranged to
receive input signals from other sources.
16. Optical radiation sensor apparatus according to any one of the
preceding claims, wherein the apparatus is a pyrometer.
17. Optical radiation sensor apparatus according to Claim 16,
wherein the output of the processing unit is supplied to an engine
control unit.
18. Optical radiation sensor apparatus substantially as
hereinbefore described with reference to the accompanying drawings.
19. Any novel feature or combination of features as hereinbefore
described.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8727759A GB2198529B (en) | 1986-12-10 | 1987-11-27 | Optical pyrometer |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB868629492A GB8629492D0 (en) | 1986-12-10 | 1986-12-10 | Optical radiation sensor apparatus |
GB8727759A GB2198529B (en) | 1986-12-10 | 1987-11-27 | Optical pyrometer |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8727759D0 GB8727759D0 (en) | 1987-12-31 |
GB2198529A true GB2198529A (en) | 1988-06-15 |
GB2198529B GB2198529B (en) | 1991-01-09 |
Family
ID=26291674
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8727759A Expired - Fee Related GB2198529B (en) | 1986-12-10 | 1987-11-27 | Optical pyrometer |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2198529B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2671177A1 (en) * | 1990-12-31 | 1992-07-03 | Smiths Industries Plc | ELECTRO-OPTICAL APPARATUS COMPRISING A NETWORK OF PHOTODETECTORS |
GB2257508A (en) * | 1991-06-28 | 1993-01-13 | Ferodo Ltd | Apparatus for temperature variation detection |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1049836A (en) * | 1963-11-21 | 1966-11-30 | Land Pyrometers Ltd | Improvements in or relating to radiation pyrometers |
GB1503042A (en) * | 1974-05-21 | 1978-03-08 | Smiths Industries Ltd | Radiation-detecting devices |
-
1987
- 1987-11-27 GB GB8727759A patent/GB2198529B/en not_active Expired - Fee Related
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1049836A (en) * | 1963-11-21 | 1966-11-30 | Land Pyrometers Ltd | Improvements in or relating to radiation pyrometers |
GB1503042A (en) * | 1974-05-21 | 1978-03-08 | Smiths Industries Ltd | Radiation-detecting devices |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2671177A1 (en) * | 1990-12-31 | 1992-07-03 | Smiths Industries Plc | ELECTRO-OPTICAL APPARATUS COMPRISING A NETWORK OF PHOTODETECTORS |
GB2257508A (en) * | 1991-06-28 | 1993-01-13 | Ferodo Ltd | Apparatus for temperature variation detection |
GB2257508B (en) * | 1991-06-28 | 1994-11-16 | Ferodo Ltd | Apparatus for temperature detection |
Also Published As
Publication number | Publication date |
---|---|
GB2198529B (en) | 1991-01-09 |
GB8727759D0 (en) | 1987-12-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19991127 |