GB601086A - Improvements in thermal de-icing devices for aircraft, flying bombs, rockets, and other flying machines and missiles - Google Patents
Improvements in thermal de-icing devices for aircraft, flying bombs, rockets, and other flying machines and missilesInfo
- Publication number
- GB601086A GB601086A GB27603/45A GB2760345A GB601086A GB 601086 A GB601086 A GB 601086A GB 27603/45 A GB27603/45 A GB 27603/45A GB 2760345 A GB2760345 A GB 2760345A GB 601086 A GB601086 A GB 601086A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- flying
- ribs
- rockets
- missiles
- 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
- 235000015842 Hesperis Nutrition 0.000 title 1
- 235000012633 Iberis amara Nutrition 0.000 title 1
- 239000007789 gas Substances 0.000 abstract 2
- 238000005192 partition Methods 0.000 abstract 2
- 230000015572 biosynthetic process Effects 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Thermal Insulation (AREA)
Abstract
601,086. Preventing formation of ice on aircraft. SOC.NATIONALE DE CONSTRUCTIONS AERONAUTIQUES DU SUD-EST. Oct. 19, 1945, No. 27603. Convention date, Oct. 3. 1944. [Class 4] To prevent ice-formation on the leading edge of a wing or other aircraft part, hot gases are discharged through orifices 3 in a thermallv-insulated tube 1, extending along the span, and are then guided rearwardly in contact with the inner face of the skin 5 through a shallow chamber 7 formed by a partition 6 backed by a heat-insulating covering 14, the gases finally escaping through apertures 8 in the wing ribs and openings 9 situated in a region of reduced pressure. The skin 5 is secured to the nose ribs and spaced from the partition by beading strips 11. The tube 1 is secured to the ribs by clamps 4, and its cross-section and the diameter and distribution of the orifices 3 may vary along the span.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR601086X | 1944-10-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB601086A true GB601086A (en) | 1948-04-27 |
Family
ID=8970976
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB27603/45A Expired GB601086A (en) | 1944-10-03 | 1945-10-19 | Improvements in thermal de-icing devices for aircraft, flying bombs, rockets, and other flying machines and missiles |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB601086A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0436243A2 (en) * | 1989-12-29 | 1991-07-10 | The Boeing Company | Anti-icing system for aircraft |
| US6079670A (en) * | 1997-12-12 | 2000-06-27 | Aerospatiale Societe Nationale Industrielle | Hot air diffuser for a jet engine air inlet cowl with de-icing circuit |
| FR2953811A1 (en) * | 2009-12-15 | 2011-06-17 | Airbus Operations Sas | PANEL FOR AN AIRCRAFT NACELLE AIR INTAKE PROVIDING ACOUSTIC TREATMENT AND TREATMENT OF OPTIMIZED GEL |
-
1945
- 1945-10-19 GB GB27603/45A patent/GB601086A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0436243A2 (en) * | 1989-12-29 | 1991-07-10 | The Boeing Company | Anti-icing system for aircraft |
| EP0436243A3 (en) * | 1989-12-29 | 1991-08-07 | The Boeing Company | Anti-icing system for aircraft |
| US6079670A (en) * | 1997-12-12 | 2000-06-27 | Aerospatiale Societe Nationale Industrielle | Hot air diffuser for a jet engine air inlet cowl with de-icing circuit |
| FR2953811A1 (en) * | 2009-12-15 | 2011-06-17 | Airbus Operations Sas | PANEL FOR AN AIRCRAFT NACELLE AIR INTAKE PROVIDING ACOUSTIC TREATMENT AND TREATMENT OF OPTIMIZED GEL |
| US8960589B2 (en) | 2009-12-15 | 2015-02-24 | Airbus Operations Sas | Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment |
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