GB775013A - Improvements in or relating to apparatus for detecting the formation of ice on a surface - Google Patents

Improvements in or relating to apparatus for detecting the formation of ice on a surface

Info

Publication number
GB775013A
GB775013A GB526254A GB526254A GB775013A GB 775013 A GB775013 A GB 775013A GB 526254 A GB526254 A GB 526254A GB 526254 A GB526254 A GB 526254A GB 775013 A GB775013 A GB 775013A
Authority
GB
United Kingdom
Prior art keywords
diaphragm
coil
frequency
ice
triode
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
Application number
GB526254A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GEORGE LEE D OMBRAIN
JOHN MORTON MACINTYRE
Bristol Aeroplane Co Ltd
Original Assignee
GEORGE LEE D OMBRAIN
JOHN MORTON MACINTYRE
Bristol Aeroplane Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by GEORGE LEE D OMBRAIN, JOHN MORTON MACINTYRE, Bristol Aeroplane Co Ltd filed Critical GEORGE LEE D OMBRAIN
Priority to GB526254A priority Critical patent/GB775013A/en
Publication of GB775013A publication Critical patent/GB775013A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/20Means for detecting icing or initiating de-icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Measuring Fluid Pressure (AREA)

Abstract

775,013. Electric indicating and control systems. BRISTOL AEROPLANE CO., Ltd., OMBRAIN, G. L. D'., and MACINTYRE, J. M. April 19, 1955 [Feb. 23, 1954], No. 5262/54. Class 40 (1). [Also in Groups XXXIII, XXXIX and XL (c)] Apparatus for detecting ice formation on a surface comprises a vibratable element located for subjection to the same conditions as the surface, means for maintaining the element in a state of free vibration, and means for producing an electricl potential which varies in response to an increase in the frequency of vibration of the element and thus to an increase in the thickness of ice thereon. In Fig. 1, the element is a diaphragm 3 flush with the surface, vibratable by a coil 6 on a core 5. A rod 15 of non-magnetic material has a permanent or electromagnet 16 at one end and is secured to the diaphragm at its other end, so that vibration of the diaphragm results in a signal in a pick-up coil 9. This coil is connected through leads 10, 11 to the input of a triode 22, which feeds a second triode 23 through a phase shift network 26. A transformer 25 in the anode circuit of triode 23 has one secondary winding 24 connected through leads 7, 8 to coil 6, so that the diaphragm acts as the resonant frequency determining element in the oscillator circuit of triodes 22, 23. The other secondary winding 30 of the transformer 25 feeds a frequency discriminating bridge (see Group XL (c)) coupled to a magnetic amplifier 41, the D.C. output of which is fed to an indicator 50, so that an indication is given of the sense and magnitude of the departure of the resonant frequency of the diaphragm from a reference frequency, which is chosen as that of the diaphragm free from ice. Ice formation is stated to raise the resonant frequency, and liquid or mushy deposits to lower it. In Figs. 3 and 4 (not shown) alternative frequency discriminators are shown, and a three-phase transductor may replace the magnetic amplifier. The output may control current to heating elements in the surface and near the vibrating element, or may control the supply of hot gas or a liquefying agent for deicing.
GB526254A 1954-02-23 1954-02-23 Improvements in or relating to apparatus for detecting the formation of ice on a surface Expired GB775013A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB526254A GB775013A (en) 1954-02-23 1954-02-23 Improvements in or relating to apparatus for detecting the formation of ice on a surface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB526254A GB775013A (en) 1954-02-23 1954-02-23 Improvements in or relating to apparatus for detecting the formation of ice on a surface

Publications (1)

Publication Number Publication Date
GB775013A true GB775013A (en) 1957-05-15

Family

ID=9792779

Family Applications (1)

Application Number Title Priority Date Filing Date
GB526254A Expired GB775013A (en) 1954-02-23 1954-02-23 Improvements in or relating to apparatus for detecting the formation of ice on a surface

Country Status (1)

Country Link
GB (1) GB775013A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3240054A (en) * 1962-12-24 1966-03-15 Gabb Special Products Inc Ice detector
US4461178A (en) * 1982-04-02 1984-07-24 The Charles Stark Draper Laboratory, Inc. Ultrasonic aircraft ice detector using flexural waves

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3240054A (en) * 1962-12-24 1966-03-15 Gabb Special Products Inc Ice detector
US4461178A (en) * 1982-04-02 1984-07-24 The Charles Stark Draper Laboratory, Inc. Ultrasonic aircraft ice detector using flexural waves

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