|Publication number||US2496279 A|
|Publication date||Feb 7, 1950|
|Filing date||Feb 10, 1945|
|Priority date||Feb 10, 1945|
|Publication number||US 2496279 A, US 2496279A, US-A-2496279, US2496279 A, US2496279A|
|Inventors||Robert S Ely, Irving M Ketcham|
|Original Assignee||Safeway Heat Elements Inc|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (3), Referenced by (84), Classifications (21)|
|External Links: USPTO, USPTO Assignment, Espacenet|
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
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.
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
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US1741054 *||Oct 11, 1926||Dec 24, 1929||Walter D Graham||Electrically-heated fabric and the like|
|US2108041 *||Aug 21, 1934||Feb 15, 1938||Paul Gayne||Aeroplane|
|US2205543 *||Nov 1, 1937||Jun 25, 1940||Maxime Ducret Andre||Heating surface|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US2582342 *||Aug 18, 1949||Jan 15, 1952||Celanese Corp||Method of weaving electrical resistance devices|
|US2590944 *||Dec 27, 1949||Apr 1, 1952||Napier & Son Ltd||Electrical heating apparatus|
|US2627012 *||Aug 5, 1950||Jan 27, 1953||English Electric Co Ltd||Heating of surfaces by laminated foil resistance elements with timed connecting means|
|US2643206 *||Sep 28, 1949||Jun 23, 1953||Wingfoot Corp||Package for shipping and storing a conductive rubber heating element and method of making same|
|US2643320 *||Apr 19, 1950||Jun 23, 1953||Connecticut Hard Rubber Co||Heating element|
|US2665090 *||Aug 3, 1950||Jan 5, 1954||Holdaway George H||Propeller ice-prevention heating unit|
|US2686640 *||Apr 13, 1951||Aug 17, 1954||Bergrun Norman R||Thermal-electric means of airfoil ice prevention|
|US2690984 *||Jan 25, 1950||Oct 5, 1954||Gen Electric||Electric cable jacket|
|US2732479 *||Jun 15, 1953||Jan 24, 1956||Rowland|
|US2743890 *||Jul 31, 1952||May 1, 1956||Goodrich Co B F||Electrically heated protective covering for aircraft|
|US2762897 *||Jun 28, 1951||Sep 11, 1956||Lockheed Aircraft Corp||De-icing means for aircraft and the like|
|US2852821 *||Dec 20, 1954||Sep 23, 1958||Olin Mathieson||Casting apparatus|
|US2938992 *||Apr 18, 1958||May 31, 1960||Electrofilm Inc||Heaters using conductive woven tapes|
|US3372487 *||Jul 10, 1963||Mar 12, 1968||Eisler Paul||Method of drying by electrical means|
|US3541303 *||Nov 8, 1967||Nov 17, 1970||Gen Motors Corp||Lint collecting and burning screen|
|US4581522 *||Nov 23, 1983||Apr 8, 1986||Intermountain Thermafloor, Inc.||Electrical heating system including a mesh heating element|
|US4841124 *||Apr 27, 1987||Jun 20, 1989||Cox & Company, Inc.||Strain-resistant heated helicopter rotor blade|
|US5131812 *||Apr 1, 1991||Jul 21, 1992||United Technologies Corporation||Aircraft engine propulsor blade deicing|
|US5298722 *||Mar 20, 1992||Mar 29, 1994||Teijin Limited||Tire warm-up wrap|
|US5657951 *||Jun 23, 1995||Aug 19, 1997||The B.F. Goodrich Company||Electrothermal de-icing system|
|US6031214 *||Feb 6, 1997||Feb 29, 2000||Eurocopter||Device for heating an aerofoil|
|US6137083 *||Nov 29, 1999||Oct 24, 2000||Eurocopter||Device for heating an aerofoil|
|US6229123 *||Sep 25, 1998||May 8, 2001||Thermosoft International Corporation||Soft electrical textile heater and method of assembly|
|US6369369||Jan 22, 2001||Apr 9, 2002||Thermosoft International Corporation||Soft electrical textile heater|
|US6403935||Feb 27, 2001||Jun 11, 2002||Thermosoft International Corporation||Soft heating element and method of its electrical termination|
|US6452138 *||May 11, 1999||Sep 17, 2002||Thermosoft International Corporation||Multi-conductor soft heating element|
|US6563094||Feb 15, 2002||May 13, 2003||Thermosoft International Corporation||Soft electrical heater with continuous temperature sensing|
|US6713733||Apr 25, 2003||Mar 30, 2004||Thermosoft International Corporation||Textile heater with continuous temperature sensing and hot spot detection|
|US6870139||Feb 11, 2003||Mar 22, 2005||The Trustees Of Dartmouth College||Systems and methods for modifying an ice-to-object interface|
|US6958463||Apr 23, 2004||Oct 25, 2005||Thermosoft International Corporation||Heater with simultaneous hot spot and mechanical intrusion protection|
|US7087876||Oct 11, 2001||Aug 8, 2006||The Trustees Of Dartmouth College||High-frequency melting of interfacial ice|
|US7164100||Jan 24, 2002||Jan 16, 2007||The Trustees Of Dartmouth College||High-frequency de-icing of cableways|
|US7291815 *||Feb 24, 2006||Nov 6, 2007||Goodrich Corporation||Composite ice protection heater and method of producing same|
|US7556221||Jun 28, 2007||Jul 7, 2009||Goodrich Corporation||Aircraft ice protection method|
|US7588212 *||Jul 8, 2003||Sep 15, 2009||Rohr Inc.||Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip|
|US7629558||Apr 24, 2006||Dec 8, 2009||The Trustees Of Dartmouth College||Systems and methods for modifying an ice-to-object interface|
|US7638735||Jan 24, 2006||Dec 29, 2009||The Trustees Of Dartmouth College||Pulse electrothermal and heat-storage ice detachment apparatus and methods|
|US7703300||Jun 22, 2005||Apr 27, 2010||The Trustees Of Dartmouth College||Pulse systems and methods for detaching ice|
|US7832983||May 1, 2007||Nov 16, 2010||Goodrich Corporation||Nacelles and nacelle components containing nanoreinforced carbon fiber composite material|
|US7837150||Dec 21, 2007||Nov 23, 2010||Rohr, Inc.||Ice protection system for a multi-segment aircraft component|
|US7883609||Jan 22, 2002||Feb 8, 2011||The Trustees Of Dartmouth College||Ice modification removal and prevention|
|US7923668||Apr 10, 2007||Apr 12, 2011||Rohr, Inc.||Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein|
|US8405002||Dec 19, 2008||Mar 26, 2013||The Trustees Of Dartmouth College||Pulse electrothermal mold release icemaker with safety baffles for refrigerator|
|US8424324||Nov 5, 2009||Apr 23, 2013||The Trustees Of Dartmouth College||Refrigerant evaporators with pulse-electrothermal defrosting|
|US8561934||Aug 28, 2009||Oct 22, 2013||Teresa M. Kruckenberg||Lightning strike protection|
|US8752279||Apr 8, 2011||Jun 17, 2014||Goodrich Corporation||Methods of protecting an aircraft component from ice formation|
|US8931296||Nov 23, 2010||Jan 13, 2015||John S. Chen||System and method for energy-saving inductive heating of evaporators and other heat-exchangers|
|US8962130||Mar 9, 2007||Feb 24, 2015||Rohr, Inc.||Low density lightning strike protection for use in airplanes|
|US9067679 *||Dec 28, 2012||Jun 30, 2015||Aerospace Filtration Systems, Inc.||Heated screen for air intake of aircraft engines|
|US20020092849 *||Oct 11, 2001||Jul 18, 2002||Petrenko Victor F.||High-frequency melting of interfacial ice|
|US20030000718 *||Jan 24, 2002||Jan 2, 2003||Petrenko Victor F.||High-frequency de-icing of cableways|
|US20030155467 *||Feb 11, 2003||Aug 21, 2003||Victor Petrenko||Systems and methods for modifying an ice-to-object interface|
|US20050006529 *||Jul 8, 2003||Jan 13, 2005||Moe Jeffrey W.||Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip|
|US20050247700 *||Apr 23, 2004||Nov 10, 2005||Eric Kochman||Heater with simultaneous hot spot and mechanical intrusion protection|
|US20060231683 *||Apr 18, 2005||Oct 19, 2006||Orr James R||Aircraft & motor vehicle protection system that eliminates eleven safety and environmental hazards associated with aircraft and vehicles parked or tied down and exposed to the elements and animals|
|US20060272340 *||Jan 24, 2006||Dec 7, 2006||Victor Petrenko||Pulse electrothermal and heat-storage ice detachment apparatus and methods|
|US20070045282 *||Apr 24, 2006||Mar 1, 2007||The Trustees Of Dartmouth College||Systems and methods for modifying an ice-to-object interface|
|US20070210073 *||Feb 24, 2006||Sep 13, 2007||Goodrich Corporation||Composite ice protection heater and method of producing same|
|US20080156937 *||Jun 28, 2007||Jul 3, 2008||Hindel James T||Aircraft ice protection method|
|US20080166563 *||Dec 19, 2007||Jul 10, 2008||Goodrich Corporation||Electrothermal heater made from thermally conducting electrically insulating polymer material|
|US20080179448 *||Apr 10, 2007||Jul 31, 2008||Rohr, Inc.||Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein|
|US20080196429 *||Oct 31, 2007||Aug 21, 2008||The Trustees Of Dartmouth College||Pulse Electrothermal And Heat-Storage Ice Detachment Apparatus And Method|
|US20080223842 *||Oct 31, 2007||Sep 18, 2008||The Trustees Of Dartmouth College||Systems And Methods For Windshield Deicing|
|US20090176112 *||May 1, 2007||Jul 9, 2009||Kruckenberg Teresa M||Modification of reinforcing fiber tows used in composite materials by using nanoreinforcements|
|US20090199569 *||Jun 22, 2005||Aug 13, 2009||Victor Petrenko||Pulse systems and methods for detaching ice|
|US20090227162 *||Mar 9, 2007||Sep 10, 2009||Goodrich Corporation||Low density lightning strike protection for use in airplanes|
|US20090235681 *||Dec 19, 2008||Sep 24, 2009||The Trustees Of Dartmouth College||Pulse Electrothermal Mold Release Icemaker For Refrigerator Having Interlock Closure And Baffle For Safety|
|US20090235682 *||Dec 19, 2008||Sep 24, 2009||The Trustees Of Dartmouth College||Pulse Electrothermal Mold Release Icemaker With Safety Baffles For Refrigerator|
|US20100038475 *||Dec 21, 2007||Feb 18, 2010||Goodrich Corporation||Ice protection system for a multi-segment aircraft component|
|US20100059503 *||May 22, 2007||Mar 11, 2010||Victor Petrenko||Pulse Electrothermal Deicing Of Complex Shapes|
|US20100084389 *||Dec 3, 2009||Apr 8, 2010||Petrenko Victor F||Systems And Methods For Modifying An Ice-To-Object Interface|
|US20100123044 *||Nov 17, 2009||May 20, 2010||Botura Galdemir C||Aircraft Ice Protection System|
|US20110001086 *||Mar 25, 2009||Jan 6, 2011||Goodrich Corporation||Methods of making nanoreinforced carbon fiber and components comprising nanoreinforced carbon fiber|
|US20110042515 *||Feb 11, 2009||Feb 24, 2011||Airbus Operations Gmbh||Arrangement for providing active fire protection in aircraft|
|US20110049292 *||Aug 28, 2009||Mar 3, 2011||Rohr, Inc||Lightning strike protection|
|US20110132588 *||Nov 23, 2010||Jun 9, 2011||Icecode, Llc||System and Method for Energy-Saving Inductive Heating of Evaporators and Other Heat-Exchangers|
|US20110233340 *||Feb 22, 2011||Sep 29, 2011||Christy Daniel P||Aircraft ice protection system|
|US20120074118 *||Nov 24, 2010||Mar 29, 2012||Kia Motors Corporation||Vehicle Heating System and Method Using PTC Heater|
|US20140077039 *||Dec 28, 2012||Mar 20, 2014||Aerospace Filtration Systems, Inc.||Heated Screen For Air Intake Of Aircraft Engines|
|US20140086748 *||May 30, 2012||Mar 27, 2014||Esa Peltola||Wind turbine blade and related method of manufacture|
|DE1186157B *||Feb 13, 1958||Jan 28, 1965||Goodyear Tire & Rubber||Elektrisches flexibles Heizelement|
|DE1254264B *||Mar 11, 1959||Nov 16, 1967||Goodrich Co B F||Verfahren und Vorrichtung zum Herstellen eines geschichteten elektrischen Heizkoerpers von plattenfoermiger Gestalt|
|EP1242280A1 *||Dec 28, 2000||Sep 25, 2002||Trustees of Dartmouth College||System and method for an electrical de-icing coating|
|WO2001049564A1 *||Dec 28, 2000||Jul 12, 2001||Trustees Of Dartmouth College||System and method for an electrical de-icing coating|
|U.S. Classification||219/528, 139/425.00R, 219/552, 219/544, 244/134.00D, 338/208, 219/545, 219/202, 338/67|
|International Classification||H05B3/34, B64D15/12|
|Cooperative Classification||H05B2203/017, H05B2203/033, H05B3/342, B64D15/12, H05B2203/005, H05B2203/015, H05B2203/011, B64D2700/62114|
|European Classification||B64D15/12, H05B3/34B|