US2540472A - Electrically heated blade and process of manufacture - Google Patents
Electrically heated blade and process of manufacture Download PDFInfo
- Publication number
- US2540472A US2540472A US90994A US9099449A US2540472A US 2540472 A US2540472 A US 2540472A US 90994 A US90994 A US 90994A US 9099449 A US9099449 A US 9099449A US 2540472 A US2540472 A US 2540472A
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- United States
- Prior art keywords
- electrical
- heating element
- blade
- sheet
- helix
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49082—Resistor making
- Y10T29/49083—Heater type
Definitions
- This invention relates to means of preventing ice formation on the blades of rotary power conversion machines and particularly on the blades of axial compressors which form a component part of aircraft gas turbine engines.
- a main object of this invention is therefore to provide means to raise the temperature of the compressor inlet guide vanes and of other compressor blades, when considered desirable, suiliciently to prevent the formation of ice on these parts when flying through atmospheric conditions conducive to icing.
- Another object is to provide a means of antiicing which may be readily controlled to suit atmospheric conditions and which requires only a simple electrical installation free of the bulky ducts, pumps and piping associated with other constructions which have heretofore been adopted.
- Another important object is to provide, in each blade to be heated, an electrical heating element of minimum cross-sectional area so that the cavity within the blade occupied by the heater will not detract unnecessarily from the structural strengthof the blade.
- a further object of this invention is to provide a heating element construction which may be embedded in and form an integral part of a metal casting and also to provide a process of making such a construction.
- Fig. 1 is an elevation view of a blade constructed in accordance with this invention and showing, in dotted outline, the disposition of the heating element within the blade;
- Fig. 2 is a cross sectional view through the line 2-2 of the blade shown in Fig. 1;
- Fig. 3 is a broken elevation of a partially completed heating element
- Fig. 4 is a broken elevation of a partially completed heating element showing the manner in which glass thread is wrapped over the wound resistance ribbon to provide electrical insulation for the latter
- r Fig. 5 is a broken elevation of the completed heating element.
- a heating element generally indicated at IU comprises a thin sheet II of mica or other suitable electrical insulating material having spaced recesses 52 in its edges, thus providing serrations, and also having perforations i3.
- An electrical resistance ribbon I4 is wound upon the sheet H in such a manner as to pass through the recesses i2, the turns being thus held in spaced relationship.
- One end of the resistance ribbon IA is spot Welded at i5 to a conducting locating lug I6, and the other end is similarly spot welded at ii to a conducting terminal lug I8.
- a double winding [9 of inorganic heat-resisting electrical insulating material is applied over the electrical resistance ribbon l4 and mica sheet H, one winding being in a clockwise direction and the other winding being in a counter-clockwise direction; both of these windings are applied in such a manner as to pass through the recesses l2 and so that the completely wound heating element appears as shown in Fig. 4.
- an electrical insulating sheath 2! Around a portion of the terminal lu I8 is provided an electrical insulating sheath 2!].
- the heating element described above is then coated or impregnated with ceramic cement 2
- the double winding IS, the sheath 20 and the coat of ceramic cement 2! must be of materials which are thermally stable at the maximum temperatures that the heating element might attain.
- the double winding i9 is preferably made of glass threads whereas the sheath 2e is preferably woven from glass threads.
- a satisfactory ceramic cement is an aqueous mixture of nine parts kaolin and 1 part bcrax.
- the ceramic cement provides additional electrical insulation and moreover secures the components of the assembly, namely the mica sheet H, the resistance ribbon 14, the glass thread winding l9 and the sheath 20 in a unitary structure. Th perforations 13 enable the ceramic cement on opposite faces of the mica sheet to be bound together.
- the heating element [0 After the heating element [0 has been coated with the ceramic cement it is placed in a suitable form and heat is applied to it; this bakes the ceramic cement and at the same time gives to the element a curvature conforming to the curvature of the blade of which it is to form a part.
- the finished heating element is illustrated in Fig. 5.
- the heating element made as described above is eventually placed in spaced relationship within a mold, and molten metal is introduced into the mold to encase the heating element with a metallic structure having the form of a blade.
- the completed blade manufactured in accordance with this invention is illustrated in Figs. 1 and 2.
- any of the guide vanes or blades of a compressor that ay be found subject to ice formation are constructed as previously described, and obviously the electrical heating elements are suitably connected to an electrical power supply.
- an electrical current is passed through the resistance ribbons of the heating element, causing sufficient heat to be generated within the vanes and blades to raise their surface temperature above the freezing point of water, thereby eliminating undesirable ice formation thereon.
- a blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material, electrical resistance wiring supported by the sheet, a helix of inorganic heat resisting electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of the helix being spaced apart, and a coating of ceramic material covering the aforesaid assembly and filling the spaces between the turns of the helix; and a metallic structure having the form of a blade and encasing the electrical heating element.
- a blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material, electrical resistance wiring supported by the sheet, criss-crossed helices of inorganic heat resisting electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of each helix being spaced apart, this arrangement of helices providing rhombic openings, and a coating of ceramic material covering the aforesaid assembly and filling the openings; and a metallic structure having the form of a blade and encasing the electrical heating element.
- a blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material having serrations in its edges, electrical resistance wiring supported by the sheet, a helix of inorganic heat resisting electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of the helix being spaced apart by the serrations, and a coating of ceramic material covering the aforesaid assembly and filling the spaces between the turns of the helix; and a metallic structure having the form of a blade and encasing the electrical heating element.
- a blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material having perforations extending through it, electrical resistance wiring supported by the sheet, a helix of inorganic heat resistin electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of the helix being spaced apart, and a coating of ceramic material covering the aforesaid assembly, the ceramic material filling the spaces between the turns of the helix and also the perforations, thereby locking the coating to the inorganic heat resisting electrical insulating material, the wiring and the sheet; and a metallic structure having the form of a blade and encasing the electrical heating element.
- a blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material having serrations in its edges and having perforations extending through it, electrical resistance wiring sup-ported by the sheet, a helix of inorganic heat resisting electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of the helix being spaced apart by the serrations, and a coating of ceramic material covering the aforesaid assembly, the ceramic material filling the spaces between the turns of the helix and also the perforations, thereby locking the coatin to the inorganic heat resisting electrical insulating material, the wiring and the sheet; and a metallic structure having the form of a blade and encasing the electrical heating element.
- a blade for a rotary power conversion machine comprising making an electrical element by winding an electrical resistance wire around a sheet of electrical insulating material, winding a helix of inorganic heat resisting electrical insulating material over and around the electrical resistance wire and the sheet, adjacent turns of the helix being spaced apart, and applying a coating of ceramic material over the aforesaid assembly, the said coating filling the spaces between the turns of the helix; locating the electrical heating element so made in spaced relationship within a mould; and introducing metal into said mould to encase the heating element with a metallic structure haivng the form of a blade.
- a blade for a rotary power conversion machine comprising making an electrical element by winding an electrical resistance wire around a sheet of elec trical insulating material, winding a helix of inorganic heat resisting electrical insulating material over and around the electrical resistance wire and the sheet, adjacent turns of the helix being spaced apart, and applying a coating of ceramic material over the aforesaid assembly, the said coating filling the spaces between the turns of the helix, and applying heat to the element to bake the ceramic material thereon; locating the electrical heating element so made in spaced relationship within a mould; and introducing metal into said mould to -encase the heating element with a metallic structure having the form of a blade.
Description
Feb. 6, 1951 w. BOYD ETAL ELECTRICALLY HEATED BLADE AND PROCESS OF MANUFACTURE Filed May 2, 1949 INVENTORS WINNETT BOYD GEORGE FKELK JOHN.E.CL K
ATT NEY Patented Feb. 6, 1951 UNITED STATES RATENT OFFICE ELECTRICALLY HEATED BLADE AND PROCESS OF l /IANUFACTURE a corporation Application May 2, 1949, Serial No. 90,994
7 Claims. 1
This invention relates to means of preventing ice formation on the blades of rotary power conversion machines and particularly on the blades of axial compressors which form a component part of aircraft gas turbine engines.
The formation of ice on the inlet components of axial compressors causes serious obstruction to the flow of air passing through them and furthermore, serious damage may result from pieces of ice breaking loose and being carried by the air stream into the rapidly moving blading. A main object of this invention is therefore to provide means to raise the temperature of the compressor inlet guide vanes and of other compressor blades, when considered desirable, suiliciently to prevent the formation of ice on these parts when flying through atmospheric conditions conducive to icing.
Another object is to provide a means of antiicing which may be readily controlled to suit atmospheric conditions and which requires only a simple electrical installation free of the bulky ducts, pumps and piping associated with other constructions which have heretofore been adopted.
Another important object is to provide, in each blade to be heated, an electrical heating element of minimum cross-sectional area so that the cavity within the blade occupied by the heater will not detract unnecessarily from the structural strengthof the blade.
A further object of this invention is to provide a heating element construction which may be embedded in and form an integral part of a metal casting and also to provide a process of making such a construction.
All of the foregoing and still further objects and advantages of the invention will become apparent from a study of the following specification, taken in conjunction with the accompanying drawings, wherein like characters of reference designate corresponding parts throughout the several views and wherein:
Fig. 1 is an elevation view of a blade constructed in accordance with this invention and showing, in dotted outline, the disposition of the heating element within the blade;
Fig. 2 is a cross sectional view through the line 2-2 of the blade shown in Fig. 1;
Fig. 3 is a broken elevation of a partially completed heating element;
Fig. 4 is a broken elevation of a partially completed heating element showing the manner in which glass thread is wrapped over the wound resistance ribbon to provide electrical insulation for the latter, and r Fig. 5 is a broken elevation of the completed heating element.
Referring to the drawings, a heating element generally indicated at IU comprises a thin sheet II of mica or other suitable electrical insulating material having spaced recesses 52 in its edges, thus providing serrations, and also having perforations i3. An electrical resistance ribbon I4 is wound upon the sheet H in such a manner as to pass through the recesses i2, the turns being thus held in spaced relationship.
One end of the resistance ribbon IA is spot Welded at i5 to a conducting locating lug I6, and the other end is similarly spot welded at ii to a conducting terminal lug I8.
In order to provide electrical insulation for the resistance ribbon, a double winding [9 of inorganic heat-resisting electrical insulating material is applied over the electrical resistance ribbon l4 and mica sheet H, one winding being in a clockwise direction and the other winding being in a counter-clockwise direction; both of these windings are applied in such a manner as to pass through the recesses l2 and so that the completely wound heating element appears as shown in Fig. 4. Around a portion of the terminal lu I8 is provided an electrical insulating sheath 2!].
The heating element described above is then coated or impregnated with ceramic cement 2|. The double winding IS, the sheath 20 and the coat of ceramic cement 2! must be of materials which are thermally stable at the maximum temperatures that the heating element might attain. The double winding i9 is preferably made of glass threads whereas the sheath 2e is preferably woven from glass threads. A satisfactory ceramic cement is an aqueous mixture of nine parts kaolin and 1 part bcrax. The ceramic cement provides additional electrical insulation and moreover secures the components of the assembly, namely the mica sheet H, the resistance ribbon 14, the glass thread winding l9 and the sheath 20 in a unitary structure. Th perforations 13 enable the ceramic cement on opposite faces of the mica sheet to be bound together.
After the heating element [0 has been coated with the ceramic cement it is placed in a suitable form and heat is applied to it; this bakes the ceramic cement and at the same time gives to the element a curvature conforming to the curvature of the blade of which it is to form a part. The finished heating element is illustrated in Fig. 5.
The heating element made as described above is eventually placed in spaced relationship within a mold, and molten metal is introduced into the mold to encase the heating element with a metallic structure having the form of a blade. The completed blade manufactured in accordance with this invention is illustrated in Figs. 1 and 2.
According to this invention, any of the guide vanes or blades of a compressor that ay be found subject to ice formation are constructed as previously described, and obviously the electrical heating elements are suitably connected to an electrical power supply. When icing conditions are encountered, an electrical current is passed through the resistance ribbons of the heating element, causing sufficient heat to be generated within the vanes and blades to raise their surface temperature above the freezing point of water, thereby eliminating undesirable ice formation thereon.
It is to be understood that the form of the invention herewith shown and described is to be taken as a preferred example of the same and that various changes in the shape, size and arrangement of the parts may be resorted to, without departing from the spirit of the invention or the scope of the claims.
What we claim as our invention is:
1. A blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material, electrical resistance wiring supported by the sheet, a helix of inorganic heat resisting electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of the helix being spaced apart, and a coating of ceramic material covering the aforesaid assembly and filling the spaces between the turns of the helix; and a metallic structure having the form of a blade and encasing the electrical heating element.
2 A blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material, electrical resistance wiring supported by the sheet, criss-crossed helices of inorganic heat resisting electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of each helix being spaced apart, this arrangement of helices providing rhombic openings, and a coating of ceramic material covering the aforesaid assembly and filling the openings; and a metallic structure having the form of a blade and encasing the electrical heating element.
3. A blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material having serrations in its edges, electrical resistance wiring supported by the sheet, a helix of inorganic heat resisting electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of the helix being spaced apart by the serrations, and a coating of ceramic material covering the aforesaid assembly and filling the spaces between the turns of the helix; and a metallic structure having the form of a blade and encasing the electrical heating element.
4. A blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material having perforations extending through it, electrical resistance wiring supported by the sheet, a helix of inorganic heat resistin electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of the helix being spaced apart, and a coating of ceramic material covering the aforesaid assembly, the ceramic material filling the spaces between the turns of the helix and also the perforations, thereby locking the coating to the inorganic heat resisting electrical insulating material, the wiring and the sheet; and a metallic structure having the form of a blade and encasing the electrical heating element.
5. A blade for a rotary power conversion machine comprising an electrical heating element which includes a sheet of electrical insulating material having serrations in its edges and having perforations extending through it, electrical resistance wiring sup-ported by the sheet, a helix of inorganic heat resisting electrical insulating material over and around the resistance wiring and the sheet, adjacent turns of the helix being spaced apart by the serrations, and a coating of ceramic material covering the aforesaid assembly, the ceramic material filling the spaces between the turns of the helix and also the perforations, thereby locking the coatin to the inorganic heat resisting electrical insulating material, the wiring and the sheet; and a metallic structure having the form of a blade and encasing the electrical heating element.
6. The process of manufacturing a blade for a rotary power conversion machine comprising making an electrical element by winding an electrical resistance wire around a sheet of electrical insulating material, winding a helix of inorganic heat resisting electrical insulating material over and around the electrical resistance wire and the sheet, adjacent turns of the helix being spaced apart, and applying a coating of ceramic material over the aforesaid assembly, the said coating filling the spaces between the turns of the helix; locating the electrical heating element so made in spaced relationship within a mould; and introducing metal into said mould to encase the heating element with a metallic structure haivng the form of a blade.
7. The process of manufacturing a blade for a rotary power conversion machine comprising making an electrical element by winding an electrical resistance wire around a sheet of elec trical insulating material, winding a helix of inorganic heat resisting electrical insulating material over and around the electrical resistance wire and the sheet, adjacent turns of the helix being spaced apart, and applying a coating of ceramic material over the aforesaid assembly, the said coating filling the spaces between the turns of the helix, and applying heat to the element to bake the ceramic material thereon; locating the electrical heating element so made in spaced relationship within a mould; and introducing metal into said mould to -encase the heating element with a metallic structure having the form of a blade.
WINNETI BOYD.
GEORGE F. KELK.
JOHN E. CLARKE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,525,460 Miller Feb. 10, 1925 1,737,912 Bogard Dec. 3, 1929 1,807,359 Waters May 26, 1931 1,951,846 Scharf Mar. 20, 1934 2,110,621 Cohen Mar. 8, 1938 2,227,931 Greenleaf Jan. 7, 1941 2,309,682 Van Daam Feb. 2, 1943
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US90994A US2540472A (en) | 1949-05-02 | 1949-05-02 | Electrically heated blade and process of manufacture |
Applications Claiming Priority (1)
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US90994A US2540472A (en) | 1949-05-02 | 1949-05-02 | Electrically heated blade and process of manufacture |
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US2540472A true US2540472A (en) | 1951-02-06 |
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US90994A Expired - Lifetime US2540472A (en) | 1949-05-02 | 1949-05-02 | Electrically heated blade and process of manufacture |
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Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2643320A (en) * | 1950-04-19 | 1953-06-23 | Connecticut Hard Rubber Co | Heating element |
US2701092A (en) * | 1949-10-25 | 1955-02-01 | Honorary Advisory Council Sci | Rotary compressor |
US2744680A (en) * | 1951-07-30 | 1956-05-08 | Armstrong Siddeley Motors Ltd | Electrical heating and mounting of axial flow compressor blades |
US2873933A (en) * | 1957-04-23 | 1959-02-17 | United Aircraft Corp | Airfoil temperature control means |
USB451248I5 (en) * | 1974-03-14 | 1976-03-02 | ||
US4993593A (en) * | 1989-07-21 | 1991-02-19 | Ralph Fabiano | Apparatus and methods for dispensing a flowable medium |
US5281091A (en) * | 1990-12-24 | 1994-01-25 | Pratt & Whitney Canada Inc. | Electrical anti-icer for a turbomachine |
US20050022974A1 (en) * | 2002-12-19 | 2005-02-03 | Forced Physics Corp. | Heat exchange technique |
US20050184193A1 (en) * | 2003-12-12 | 2005-08-25 | Eurocopter | Modular anti-icing/de-icing device for an aerodynamic surface |
EP1728991A2 (en) | 2005-05-31 | 2006-12-06 | United Technologies Corporation | Electrothermal inlet ice protection system |
EP1739285A1 (en) * | 2005-07-01 | 2007-01-03 | Siemens Aktiengesellschaft | Cooled gas turbine stator vane and method of operation of a gas turbine |
US20070029498A1 (en) * | 2005-08-04 | 2007-02-08 | Forced Physics Llc, A Limited Liability Company | Enhanced heteroscopic techniques |
US20070029952A1 (en) * | 2005-08-04 | 2007-02-08 | Scott Davis | Coherent emission of spontaneous asynchronous radiation |
EP2113635A1 (en) * | 2008-04-30 | 2009-11-04 | Siemens Aktiengesellschaft | Multi-stage condensation steam turbine |
US20100065541A1 (en) * | 2008-09-16 | 2010-03-18 | Hamilton Sundstrand Corporation | Propeller deicing system |
US20100329836A1 (en) * | 2009-06-30 | 2010-12-30 | Wayne Garcia Edmondson | Method of operating a heated guide vane assembly |
US20100326041A1 (en) * | 2009-06-30 | 2010-12-30 | Wayne Garcia Edmondson | Heated guide vane |
US20130251500A1 (en) * | 2012-03-23 | 2013-09-26 | Kin-Leung Cheung | Gas turbine engine case with heating layer and method |
US20180238233A1 (en) * | 2013-03-15 | 2018-08-23 | United Technologies Corporation | De-icing by integral electric heat generation |
US10690000B1 (en) * | 2019-04-18 | 2020-06-23 | Pratt & Whitney Canada Corp. | Gas turbine engine and method of operating same |
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US1525460A (en) * | 1922-02-13 | 1925-02-10 | Cutler Hammer Mfg Co | Resistance |
US1737912A (en) * | 1928-01-09 | 1929-12-03 | E H Christian | Rotary heating device |
US1807359A (en) * | 1927-10-28 | 1931-05-26 | Waters William | Heater for propellers |
US1951846A (en) * | 1931-11-27 | 1934-03-20 | Megraw Electric Company | Support for electrical resistance elements |
US2110621A (en) * | 1935-02-08 | 1938-03-08 | Thermal Units Mfg Company | Fan |
US2227931A (en) * | 1938-09-10 | 1941-01-07 | Rockbestos Products Corp | Magnet wire |
US2309682A (en) * | 1939-06-27 | 1943-02-02 | Gerrit Van Daam | Means for heating wings of airplanes |
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US1525460A (en) * | 1922-02-13 | 1925-02-10 | Cutler Hammer Mfg Co | Resistance |
US1807359A (en) * | 1927-10-28 | 1931-05-26 | Waters William | Heater for propellers |
US1737912A (en) * | 1928-01-09 | 1929-12-03 | E H Christian | Rotary heating device |
US1951846A (en) * | 1931-11-27 | 1934-03-20 | Megraw Electric Company | Support for electrical resistance elements |
US2110621A (en) * | 1935-02-08 | 1938-03-08 | Thermal Units Mfg Company | Fan |
US2227931A (en) * | 1938-09-10 | 1941-01-07 | Rockbestos Products Corp | Magnet wire |
US2309682A (en) * | 1939-06-27 | 1943-02-02 | Gerrit Van Daam | Means for heating wings of airplanes |
Cited By (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2701092A (en) * | 1949-10-25 | 1955-02-01 | Honorary Advisory Council Sci | Rotary compressor |
US2643320A (en) * | 1950-04-19 | 1953-06-23 | Connecticut Hard Rubber Co | Heating element |
US2744680A (en) * | 1951-07-30 | 1956-05-08 | Armstrong Siddeley Motors Ltd | Electrical heating and mounting of axial flow compressor blades |
US2873933A (en) * | 1957-04-23 | 1959-02-17 | United Aircraft Corp | Airfoil temperature control means |
USB451248I5 (en) * | 1974-03-14 | 1976-03-02 | ||
US3997758A (en) * | 1974-03-14 | 1976-12-14 | Westinghouse Electric Corporation | Moisture control device for steam turbines |
US4993593A (en) * | 1989-07-21 | 1991-02-19 | Ralph Fabiano | Apparatus and methods for dispensing a flowable medium |
US5281091A (en) * | 1990-12-24 | 1994-01-25 | Pratt & Whitney Canada Inc. | Electrical anti-icer for a turbomachine |
US20070243059A1 (en) * | 2002-12-19 | 2007-10-18 | Forced Physics Llc | Techniques for movement through gas or liquid or liquid without a velocity boundary layer |
US20050022974A1 (en) * | 2002-12-19 | 2005-02-03 | Forced Physics Corp. | Heat exchange technique |
US20050184193A1 (en) * | 2003-12-12 | 2005-08-25 | Eurocopter | Modular anti-icing/de-icing device for an aerodynamic surface |
US7523889B2 (en) * | 2003-12-12 | 2009-04-28 | Eurocopter | Modular anti-icing/de-icing device for an aerodynamic surface |
EP1728991A2 (en) | 2005-05-31 | 2006-12-06 | United Technologies Corporation | Electrothermal inlet ice protection system |
US20060280600A1 (en) * | 2005-05-31 | 2006-12-14 | United Technologies Corporation | Electrothermal inlet ice protection system |
EP1728991A3 (en) * | 2005-05-31 | 2009-09-30 | United Technologies Corporation | Electrothermal inlet ice protection system |
US8366047B2 (en) * | 2005-05-31 | 2013-02-05 | United Technologies Corporation | Electrothermal inlet ice protection system |
US20070116563A1 (en) * | 2005-07-01 | 2007-05-24 | Fathi Ahmad | Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine |
US7465150B2 (en) | 2005-07-01 | 2008-12-16 | Siemens Aktiengesellachaft | Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine |
US20090074572A1 (en) * | 2005-07-01 | 2009-03-19 | Fathi Ahmad | Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine |
EP1739285A1 (en) * | 2005-07-01 | 2007-01-03 | Siemens Aktiengesellschaft | Cooled gas turbine stator vane and method of operation of a gas turbine |
US20070029952A1 (en) * | 2005-08-04 | 2007-02-08 | Scott Davis | Coherent emission of spontaneous asynchronous radiation |
US20070029498A1 (en) * | 2005-08-04 | 2007-02-08 | Forced Physics Llc, A Limited Liability Company | Enhanced heteroscopic techniques |
EP2113635A1 (en) * | 2008-04-30 | 2009-11-04 | Siemens Aktiengesellschaft | Multi-stage condensation steam turbine |
US20110129343A1 (en) * | 2008-04-30 | 2011-06-02 | Christoph Ebert | Guide Vane for a Condensation Steam Turbine and Associated Condensation Steam Turbine |
US8740546B2 (en) | 2008-04-30 | 2014-06-03 | Siemens Aktiengesellschaft | Guide vane for a condensation steam turbine and associated condensation steam turbine |
US20100065541A1 (en) * | 2008-09-16 | 2010-03-18 | Hamilton Sundstrand Corporation | Propeller deicing system |
US9656757B2 (en) * | 2008-09-16 | 2017-05-23 | Hamilton Sundstrand Corporation | Propeller deicing system |
US20100329836A1 (en) * | 2009-06-30 | 2010-12-30 | Wayne Garcia Edmondson | Method of operating a heated guide vane assembly |
US20100326041A1 (en) * | 2009-06-30 | 2010-12-30 | Wayne Garcia Edmondson | Heated guide vane |
US20130251500A1 (en) * | 2012-03-23 | 2013-09-26 | Kin-Leung Cheung | Gas turbine engine case with heating layer and method |
US20180238233A1 (en) * | 2013-03-15 | 2018-08-23 | United Technologies Corporation | De-icing by integral electric heat generation |
US10830137B2 (en) * | 2013-03-15 | 2020-11-10 | Raytheon Technologies Corporation | De-icing by integral electric heat generation |
US10690000B1 (en) * | 2019-04-18 | 2020-06-23 | Pratt & Whitney Canada Corp. | Gas turbine engine and method of operating same |
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