GB485395A - Means for preventing the formation of ice on the wings and/or fuselage of aircraft - Google Patents
Means for preventing the formation of ice on the wings and/or fuselage of aircraftInfo
- Publication number
- GB485395A GB485395A GB33165/36A GB3316536A GB485395A GB 485395 A GB485395 A GB 485395A GB 33165/36 A GB33165/36 A GB 33165/36A GB 3316536 A GB3316536 A GB 3316536A GB 485395 A GB485395 A GB 485395A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wings
- aircraft
- ice
- preventing
- formation
- 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
- 230000015572 biosynthetic process Effects 0.000 title abstract 3
- 238000005192 partition Methods 0.000 abstract 2
- 238000009825 accumulation Methods 0.000 abstract 1
- 239000004020 conductor Substances 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/04—Hot gas application
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Thermal Insulation (AREA)
Abstract
485,395. Preventing the formation and accumulation of snow and ice on aircraft. BROOKFIELD, J. C. Dec. 3, 1936, No. 33165. [Class 4] Means applied to the wings or fuselage of aircraft for preventing the formation of ice thereon comprise, in combination, a heat-radiating pipe 3 conveying the exhaust gases from the engine and which is carried along the wings or fuselage immediately behind the leading surface thereof, and an internal partition which, in conjunction with the surface, forms a hot air chamber through which the pipe is led, the said surface being made of or impregnated with a heat-conducting material. As applied to the wings the partition may be flat or may consist of a heat-insulating tube 6, Fig. 1, attached to the wing covering 8 and provided with a longitudinal slot 9. The tube 3 may be constituted by a hollow tubular member of the wing structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB33165/36A GB485395A (en) | 1936-12-03 | 1936-12-03 | Means for preventing the formation of ice on the wings and/or fuselage of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB33165/36A GB485395A (en) | 1936-12-03 | 1936-12-03 | Means for preventing the formation of ice on the wings and/or fuselage of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB485395A true GB485395A (en) | 1938-05-19 |
Family
ID=10349386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB33165/36A Expired GB485395A (en) | 1936-12-03 | 1936-12-03 | Means for preventing the formation of ice on the wings and/or fuselage of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB485395A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101962076A (en) * | 2010-09-15 | 2011-02-02 | 北京航空航天大学 | Gas film ice prevention structure of leading edge of nacelle of airplane |
| FR2951436A1 (en) * | 2009-10-15 | 2011-04-22 | Airbus Operations Sas | AIRCRAFT TURBOHOMOTOR HANGING MACHINE WITH CONCENTRIC HOT AIR PIPING |
-
1936
- 1936-12-03 GB GB33165/36A patent/GB485395A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2951436A1 (en) * | 2009-10-15 | 2011-04-22 | Airbus Operations Sas | AIRCRAFT TURBOHOMOTOR HANGING MACHINE WITH CONCENTRIC HOT AIR PIPING |
| US8459588B2 (en) | 2009-10-15 | 2013-06-11 | Airbus Operations S.A.S. | Attachment pylon for an aircraft turbo-shaft engine with concentric hot air channels |
| CN101962076A (en) * | 2010-09-15 | 2011-02-02 | 北京航空航天大学 | Gas film ice prevention structure of leading edge of nacelle of airplane |
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