GB1012165A - Method and apparatus for electrical heating of components - Google Patents
Method and apparatus for electrical heating of componentsInfo
- Publication number
- GB1012165A GB1012165A GB6643/60A GB664360A GB1012165A GB 1012165 A GB1012165 A GB 1012165A GB 6643/60 A GB6643/60 A GB 6643/60A GB 664360 A GB664360 A GB 664360A GB 1012165 A GB1012165 A GB 1012165A
- Authority
- GB
- United Kingdom
- Prior art keywords
- skin
- members
- laminated
- ferromagnetic material
- metal
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Resistance Heating (AREA)
Abstract
1,012,165. De-icing aircraft. T. E. EVANS. Nov. 27, 1961 [Aug. 25, 1960], No. 6643/60. Heading B7W. [Also in Division H5] A leading-edge section 9 (Fig. 1) of an aerofoil, e.g. an aircraft wing, comprises a skin or shell 91 and supporting members 10, 13 made of ferromagnetic material, e.g. laminated iron alloy, which are magnetized by passage of alternating current in a coil-winding 11 to effect heating of the skin by induced electric currents circulating in a coating of metal, e.g. copper and/or silver, 17 (Fig. 6) on the inner and outer surfaces thereof, the coatings being connected to one another to form closed loops by slots 16 filled with said metal by, e.g. electrodeposition. Heating of the skin may be partially effected by relatively large eddy-currents circulating therein, the ferromagnetic material being rendered solid, rather than laminated, or of low resistivity. Skin 91 may be secured to members 10, 13 by screws (Fig. 2, not shown). alternatively, the ends of the skin may be turned inwardly to form two adjacent closed loops or U-shaped members, the members 10, 13 being omitted; otherwise, member 10 may be laminated with some of the laminations extended and shaped to form the skin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB6643/60A GB1012165A (en) | 1960-08-25 | 1960-08-25 | Method and apparatus for electrical heating of components |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB6643/60A GB1012165A (en) | 1960-08-25 | 1960-08-25 | Method and apparatus for electrical heating of components |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1012165A true GB1012165A (en) | 1965-12-08 |
Family
ID=9818190
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6643/60A Expired GB1012165A (en) | 1960-08-25 | 1960-08-25 | Method and apparatus for electrical heating of components |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1012165A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2440133A (en) * | 2006-07-18 | 2008-01-23 | Gkn Aerospace Transparency Sys | A de-icing heated leading edge component of an aircraft |
| FR2906786A1 (en) * | 2006-10-09 | 2008-04-11 | Eurocopter France | Aircraft i.e. rotocraft, wall outer face defrosting device for helicopter manufacture field, has thin inductors generating heating of plate when inductors are supplied by current source without heating composite structure |
| EP2292514A3 (en) * | 2009-09-03 | 2013-04-17 | The Boeing Company | Ice protection system and method |
-
1960
- 1960-08-25 GB GB6643/60A patent/GB1012165A/en not_active Expired
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2440133A (en) * | 2006-07-18 | 2008-01-23 | Gkn Aerospace Transparency Sys | A de-icing heated leading edge component of an aircraft |
| US8302911B2 (en) | 2006-07-18 | 2012-11-06 | Gkn Aerospace Services Limited | Aircraft structure |
| FR2906786A1 (en) * | 2006-10-09 | 2008-04-11 | Eurocopter France | Aircraft i.e. rotocraft, wall outer face defrosting device for helicopter manufacture field, has thin inductors generating heating of plate when inductors are supplied by current source without heating composite structure |
| EP1911673A1 (en) * | 2006-10-09 | 2008-04-16 | Eurocopter | Method and device for de-icing the wall of an aircraft |
| EP2292514A3 (en) * | 2009-09-03 | 2013-04-17 | The Boeing Company | Ice protection system and method |
| US8777163B2 (en) | 2009-09-03 | 2014-07-15 | The Boeing Company | Ice protection system and method |
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