Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.

Patents

  1. Advanced Patent Search
Publication numberUS2496279 A
Publication typeGrant
Publication dateFeb 7, 1950
Filing dateFeb 10, 1945
Priority dateFeb 10, 1945
Publication numberUS 2496279 A, US 2496279A, US-A-2496279, US2496279 A, US2496279A
InventorsRobert S Ely, Irving M Ketcham
Original AssigneeSafeway Heat Elements Inc
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Flexible electric heater for deicing airfoils
US 2496279 A
Images(2)
Previous page
Next page
Description  (OCR text may contain errors)

Feb. 7, 1950 R. s. ELY ET AL 2,496,279

FLEXIBLE ELECTRIC HEATER FOR DE-ICING AIR FOILS Feb. 7, 1956 R. s. ELY ET AL. 2,496,279

RLEXIBLRELECTRIC HEATER RoR DE-ICING AIR Fons Filed Feb. l0, 1945 2 Sheees-SheeftI 2 INVENTORS ROer'/SZEZ fi/@asses BY Patented Feb. 7, 1950 FLEXIBLE ELECTRIC HEATER FOR DEICING AIRFOILS Robert S. Eiy, Westbury, and Irving M. Ketcham,

Roslyn Heights, N. Y., assignors, by mesne assignments, to Safeway Heat Elements, Inc., New York, N. Y., a corporation of Delaware Application February 10, 1945, Serial No. 577,232

3 Claims.

One object of the invention is to provide a heater which will emit different amounts of heat per unit of surface from different areas of the heater. A further object of the invention is to provide a heater which is flexible enough to be cemented or otherwise aixed in heat eX- j change relationship to curved or uneven surfaces.

Devices in use for de-icing of the pulsating boot type are heavy, expensive to maintain and uncertain in their function. The resistor type heaters used heretofore, for this purpose emit uniform amounts of heat from all parts of their surface Whereas it has been found that greater concentrations of heat are demanded in some areas and less heat in others.

In our invention these objects to construction of the prior art are overcome by providing a heater which is Woven in the formr of a flexible blanket or tape in which different concentrations of heat are emitted at various parts of the heater so that when it is used for de-icing the greatest amount of heat will be given olf at the places Where ice forms the fastest. In the Vpreferred embodiment of the invention the heater fabric consists of flexible resistor Wires forming the warp and the Woof is Woven with thread made from glass, asbestos or other heat resisting dielectric material. In some cases We may use resistor wire in both the warp and the Woof of the fabric. In this case the warp or Woof wires or both would be insulated with a heat resisting dielectric such as braided glass or asbestos sleeving. We may also use some dielectric threads in the warp to reinforce the fabric at the edges and between the groups of Wires.

In the preferred form the diierent heat concentrations are achieved by serially connecting warp Wires of different resistance or by serially connecting groups of warp wires of different resistance. In a series circuit the greatest wattage will develop where the resistance is highest. It is thus possible to provide a heater in which the Vheat varies in longitudinal strips or in lateral bands or in both strips and bands. When heater Wires are used for both the Warp and the Woof, We ft.

may connect the warp and Woof circuits in series or in parallel or each may be connected to operate independently of the other. Thermostatic means may be provided to control the operation of either circuit.

To give mechanical strength and dielectric protection the heater fabric may be impregnated with rubber, silicone, resin or other flexible bind..- er. Where' additional protection or a smooth surface is required, We may encase the heater in a sheath of rubber or other suitable material such as neoprene. The sheath may be moulded or vulcanized directly to the heater or it maybe removable.

These and other features and objects of our invention will appear from the following description thereof in which reference is made to the accompanying figures of the drawings.

In the drawings- Figure 1 is a side elevation of a propeller blade embodying a form of our invention;

Figure 2 is an enlarged cross sectional View of the leading edge of a surface carrying one of our de-icers;

Figure 3 is a cross sectional enlarged nview of one of the de-icers;

Figure 4 is a view of the heating element;

Figure 5 is a schematic view of a series of elements adapted to be positioned Within one cover;

Figure 6 is another View of a heating element Woven in the form of a flexible fabric; l

Figures 7 to 11 inclusive are wiring diagrams.

Referring more particularly to the drawings, Figure 4 discloses a heating element I'U made up of Warpwires Il and Woof members l2. The warp is made of flexible resistor Wires while the Woof is Woven of thread made of glass, asbestos, yor other heat resisting vdielectric material. The length of unit l0 depends upon the area to be covered and, in the case of the propeller blade, this would be determined by the length ofthe blade. As the unit is woven and completeda copper element l5 is woven into the fabric ad- 'jacent the end of the unit to form two strands I6 and I'l. It will be noticed that the strand I6 passes under the copper Wires which the strand I1 passes over so that each wire is contacted on both sides by the copper element. This element may then be soldered to the warp wires Il and then cut in sections to form separate connection members, as illustrated in Figure 6. The type of cutting members shown in Figure 6 are slightly different but the effect of cutting the copper element I5 is the same. For strength and to form a proper edge 22 the glass fibers 23 may be used as warp threads rather than the resistor wires. It will be understood that lead wires 24 and 25, as shown in Figure 1, will be connected to the element similarto the lead 55 shown in Figure 6. v v

y In making thegunit the copper element 'l5 is cut so that the connecting element in the center of the unit connects fewer ywires than those` at the outer edge. This resultsV in increased heating in the central zones and of varying watt density per square inch.

The heating element l is preferably engaged in a suitable cover 3U which is `feathered at 3l for smooth installation. It has been found that the heating element l0 may :be readily encased in uncured neoprene which may then be cured and fused about the heating element to form a flexible covering which may be cemented on the leading edge of the plane wing or lon the leading edge of a propeller blade, as shown in Figure 2. If the area to be heated is such that the continuous heat of the entire surface will overtax the capacity of the generator furnishing the current the area may be divided into zones, each supplied by a Separate heating element, as Shown in Figure 5. There the area 35 is divided into zones by separate heating elements 36, 31, 38 and 39 having separate leads 4t. By any conventional means the current may be alternately or successively fed to selected zones. Similarly a 4fourblade propeller having a unit on each blade may be heated by successively feeding the current for a predetermined time, thus using a minimum amount of current to :prevent the formation of ice.

Referring to Figure 6, this particular unit 50 is made up with a warp composed of 60 heater wires 5I of equal resistance and eight glass threads 52. The Woof 53 is a glass thread. The warp wires are connected in series of groups by connectors 54 made of flexible braided copper tabs. The numerical grouping of the sixty wires is as follows- 9-8-7-6-6-'7-8-9. The amount lof heat emitted per unit of surface will be greatest in the central longitudinal strip covered by the six wire groups and the heat will decrease in three successive steps toward each edge. The entire circuit is connected to a source of electric power by lead wires 55.

It will be appreciated that the ends of each adjacent group at one end of the unit are connected by one yof the connectors 54.

Figure 7 is a simplified diagram of the type of circuit shown in Figure 6. The twelve equal resistance wires VI, VII and VIII are arranged in serially connected groups having the numerical 'ratio 3, 2, I-l, 2, 3. The greatest amo-unt of heat is emitted by wires VIII, lless is emitted by Wires VII and least by Wires VI.

In Figure 8 the modification of circuit shown in Figures 6 and 7 is shown. The wires IX and X are serially connected in groups of 2-2-2 with wires X having greater resistance than wires IX.

With this arrangement more heat is emitted by the two center strips than by the two outer strips.

In Figure 9 is shown a heater composed of equal resistors in which the heat decreases from the center to the edges and valso from the bottom to the top. Thus a section through the line B-B will emit more heat than a section through the line A-A.

Figure 10 is a modication of the circuit shown in Figure 9. The wires XVII have the greatest resistance, wires XVI have less and wires XV the least resistance. Here again the heat will decrease fromzthe center to the edges and from the bottom to the top. A section through the line D-D will be hotter than a section through the line C-C.

In Figure 11 a diagram of a heater is shown in 'which the Woof 56 forms one `or more electric heater circuits woven through but insulated from the warp 51. The warp circuits may consist of any combination of resistors including the arrangements shown in Figures 1 5. The warp and Woof circuits may be connected in series, in parallel or they maybe separated by separate controls.

It will be understood that the foregoing are merely examples of the application of our invention and Iare typical of the embodiments which may 'be employed. However, numerous changes and modications may be made in the form and the .arrangement of parts without departing from the spirit of the invention and it should be understood that we do not intend the invention to be limited to the illustrative embodiments set forth.

We claim:

1. A flexible heating element for heating the leading edge of an air foil, said element comprising a woven fabric, the warp of said fabric running parallel to said airfoil edge and consisting of a plurality of resistor wires and the Woof of heat resisting dielectric material, electrical conducting elements woven into said heating element, said conducting elements contacting and connecting certain of said resistor wires in mechanically and electrically parallel groups and connecting said groups electrically in series whereby the heat intensity developed in said groups will vary in inverse proportion to the number of wires in each group.

2. A flexible heating element for heating the leading edge of `an air Ifoil, said element comprising a woven falbric, the warp of said fabric running parallel to said air foil edge and consisting of a plurality of resistor wires and the Woof of heat resisting dielectric material, electrical conducting elements woven into said heating element, said conducting elements contacting and connecting certain of said resistor wires in mechanically and electrically parallel groups and connecting said groups electrically in series whereby the heat `producing area of the greatest intensity is in closest proximity to the edge of the air foil paralleling the same, the second heat producing area of intermediate intensity is spaced from the first and the third heat producing area of least intensity is spaced from the second area.

3. A flexible heating element for heating the leading edge of an airfoil, said element comprising a woven fabric encased in a protective covering, the warp of said fabric running parallel to said airfoil edge and yconsisting of a plurality of resistor wires, and the Woof consisting of heat resisting dielectric material, said resistor wires being grouped with the ends yof each group being connected and with each group connected t0 the adjacent group, a conducting element connected to each of the outside groups whereby the heat intensity developed in said groups will vary in inverse proportion to the number .of wires in each group.

ROBERT S. ELY. IRVING M. KETCHAM.

REFERENCES CIIED The following references are of record in the le of this patent:

UNITED STATES PATENTS Rideau et al June 25, 1940

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US1741054 *Oct 11, 1926Dec 24, 1929Walter D GrahamElectrically-heated fabric and the like
US2108041 *Aug 21, 1934Feb 15, 1938Paul GayneAeroplane
US2205543 *Nov 1, 1937Jun 25, 1940Maxime Ducret AndreHeating surface
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2582342 *Aug 18, 1949Jan 15, 1952Celanese CorpMethod of weaving electrical resistance devices
US2590944 *Dec 27, 1949Apr 1, 1952Napier & Son LtdElectrical heating apparatus
US2627012 *Aug 5, 1950Jan 27, 1953English Electric Co LtdHeating of surfaces by laminated foil resistance elements with timed connecting means
US2643206 *Sep 28, 1949Jun 23, 1953Wingfoot CorpPackage for shipping and storing a conductive rubber heating element and method of making same
US2643320 *Apr 19, 1950Jun 23, 1953Connecticut Hard Rubber CoHeating element
US2665090 *Aug 3, 1950Jan 5, 1954Holdaway George HPropeller ice-prevention heating unit
US2686640 *Apr 13, 1951Aug 17, 1954Bergrun Norman RThermal-electric means of airfoil ice prevention
US2690984 *Jan 25, 1950Oct 5, 1954Gen ElectricElectric cable jacket
US2732479 *Jun 15, 1953Jan 24, 1956 Rowland
US2743890 *Jul 31, 1952May 1, 1956Goodrich Co B FElectrically heated protective covering for aircraft
US2762897 *Jun 28, 1951Sep 11, 1956Lockheed Aircraft CorpDe-icing means for aircraft and the like
US2852821 *Dec 20, 1954Sep 23, 1958Olin MathiesonCasting apparatus
US2938992 *Apr 18, 1958May 31, 1960Electrofilm IncHeaters using conductive woven tapes
US3372487 *Jul 10, 1963Mar 12, 1968Eisler PaulMethod of drying by electrical means
US3541303 *Nov 8, 1967Nov 17, 1970Gen Motors CorpLint collecting and burning screen
US4581522 *Nov 23, 1983Apr 8, 1986Intermountain Thermafloor, Inc.Electrical heating system including a mesh heating element
US4841124 *Apr 27, 1987Jun 20, 1989Cox & Company, Inc.Strain-resistant heated helicopter rotor blade
US5131812 *Apr 1, 1991Jul 21, 1992United Technologies CorporationAircraft engine propulsor blade deicing
US5298722 *Mar 20, 1992Mar 29, 1994Teijin LimitedTire warm-up wrap
US5657951 *Jun 23, 1995Aug 19, 1997The B.F. Goodrich CompanyElectrothermal de-icing system
US6031214 *Feb 6, 1997Feb 29, 2000EurocopterDevice for heating an aerofoil
US6137083 *Nov 29, 1999Oct 24, 2000EurocopterDevice for heating an aerofoil
US6229123 *Sep 25, 1998May 8, 2001Thermosoft International CorporationSoft electrical textile heater and method of assembly
US6369369Jan 22, 2001Apr 9, 2002Thermosoft International CorporationSoft electrical textile heater
US6403935Feb 27, 2001Jun 11, 2002Thermosoft International CorporationSoft heating element and method of its electrical termination
US6452138 *May 11, 1999Sep 17, 2002Thermosoft International CorporationMulti-conductor soft heating element
US6563094Feb 15, 2002May 13, 2003Thermosoft International CorporationSoft electrical heater with continuous temperature sensing
US6713733Apr 25, 2003Mar 30, 2004Thermosoft International CorporationTextile heater with continuous temperature sensing and hot spot detection
US6870139Feb 11, 2003Mar 22, 2005The Trustees Of Dartmouth CollegeSystems and methods for modifying an ice-to-object interface
US6958463Apr 23, 2004Oct 25, 2005Thermosoft International CorporationHeater with simultaneous hot spot and mechanical intrusion protection
US7087876Oct 11, 2001Aug 8, 2006The Trustees Of Dartmouth CollegeHigh-frequency melting of interfacial ice
US7164100Jan 24, 2002Jan 16, 2007The Trustees Of Dartmouth CollegeHigh-frequency de-icing of cableways
US7291815 *Feb 24, 2006Nov 6, 2007Goodrich CorporationComposite ice protection heater and method of producing same
US7556221Jun 28, 2007Jul 7, 2009Goodrich CorporationAircraft ice protection method
US7588212 *Jul 8, 2003Sep 15, 2009Rohr Inc.Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip
US7629558Apr 24, 2006Dec 8, 2009The Trustees Of Dartmouth CollegeSystems and methods for modifying an ice-to-object interface
US7638735Jan 24, 2006Dec 29, 2009The Trustees Of Dartmouth CollegePulse electrothermal and heat-storage ice detachment apparatus and methods
US7703300Jun 22, 2005Apr 27, 2010The Trustees Of Dartmouth CollegePulse systems and methods for detaching ice
US7832983May 1, 2007Nov 16, 2010Goodrich Corporationcomposite materials containing carbon fibers for use in aircraft engines; having enhanced strength and stiffness
US7837150Dec 21, 2007Nov 23, 2010Rohr, Inc.Ice protection system for a multi-segment aircraft component
US7883609Jan 22, 2002Feb 8, 2011The Trustees Of Dartmouth CollegeIce modification removal and prevention
US7923668Apr 10, 2007Apr 12, 2011Rohr, Inc.Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
US8405002Dec 19, 2008Mar 26, 2013The Trustees Of Dartmouth CollegePulse electrothermal mold release icemaker with safety baffles for refrigerator
US8424324Nov 5, 2009Apr 23, 2013The Trustees Of Dartmouth CollegeRefrigerant evaporators with pulse-electrothermal defrosting
US8561934Aug 28, 2009Oct 22, 2013Teresa M. KruckenbergLightning strike protection
US8752279Apr 8, 2011Jun 17, 2014Goodrich CorporationMethods of protecting an aircraft component from ice formation
US20110042515 *Feb 11, 2009Feb 24, 2011Airbus Operations GmbhArrangement for providing active fire protection in aircraft
US20120074118 *Nov 24, 2010Mar 29, 2012Kia Motors CorporationVehicle Heating System and Method Using PTC Heater
DE1186157B *Feb 13, 1958Jan 28, 1965Goodyear Tire & RubberElektrisches flexibles Heizelement
DE1254264B *Mar 11, 1959Nov 16, 1967Goodrich Co B FVerfahren und Vorrichtung zum Herstellen eines geschichteten elektrischen Heizkoerpers von plattenfoermiger Gestalt
EP1242280A1 *Dec 28, 2000Sep 25, 2002Trustees of Dartmouth CollegeSystem and method for an electrical de-icing coating
WO2001049564A1 *Dec 28, 2000Jul 12, 2001Dartmouth CollegeSystem and method for an electrical de-icing coating
Classifications
U.S. Classification219/528, 139/425.00R, 219/552, 219/544, 244/134.00D, 338/208, 219/545, 219/202, 338/67
International ClassificationH05B3/34, B64D15/12
Cooperative ClassificationH05B2203/017, H05B2203/033, H05B3/342, B64D15/12, H05B2203/005, H05B2203/015, H05B2203/011, B64D2700/62114
European ClassificationB64D15/12, H05B3/34B