GB407530A - Improvements in or relating to radiators for aircraft engines - Google Patents
Improvements in or relating to radiators for aircraft enginesInfo
- Publication number
- GB407530A GB407530A GB7340/33A GB734033A GB407530A GB 407530 A GB407530 A GB 407530A GB 7340/33 A GB7340/33 A GB 7340/33A GB 734033 A GB734033 A GB 734033A GB 407530 A GB407530 A GB 407530A
- Authority
- GB
- United Kingdom
- Prior art keywords
- venturi
- radiator
- wing
- shaped passage
- chamber
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P11/00—Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
- F01P11/10—Guiding or ducting cooling-air, to, or from, liquid-to-air heat exchangers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
407,530. Radiators for aircraft and motor vehicles. FERLAY, G., 66, Rue Pierre-Larousse, Paris. March 10, 1933, No. 7340. Convention date, March 12, 1932. [Class 29.] The radiator 11 is placed in a Venturi-shaped passage in a casing secured to the leading edge of the wing of an aircraft. The cooling air leaves the casing through a slot 7 controlled by a hinged shutter 8 and arranged towards the back of the wing to give to the latter the characteristics of a slotted wing. The Specification, as open to inspection under Sect. 91 comprises also the placing of the radiator 11, Fig. 6 (Cancelled), in a Venturi-shaped passage in an open-ended chamber disposed beneath the fuselage and provided with a pair of hinged dampers 24 and a pivoted vane 8, an aperture 26 being provided to admit additional air into the chamber. Fig. 5 (Cancelled) shows a radiator 11 disposed in a Venturi-shaped passage in a chamber arranged on the roof of a motor vehicle and to which additional air is supplied through a duct 23 by a fan 21 driven by the engine. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR407530X | 1932-03-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB407530A true GB407530A (en) | 1934-03-22 |
Family
ID=8897354
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB7340/33A Expired GB407530A (en) | 1932-03-12 | 1933-03-10 | Improvements in or relating to radiators for aircraft engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB407530A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2423175A (en) * | 1943-11-15 | 1947-07-01 | Churchill John Adrian | Heat exchange apparatus |
| US3205964A (en) * | 1960-05-07 | 1965-09-14 | Citroen Sa Andre | Cooling-air circuits for the engines of automobile vehicles |
| US4962903A (en) * | 1987-10-19 | 1990-10-16 | Red Eye Arms, Inc. | Cooling method and apparatus for wings and other fuselage components |
| GB2234805A (en) * | 1989-08-04 | 1991-02-13 | Rolls Royce Plc | A heat exchanger arrangement for a gas turbine engine |
| WO2014048731A1 (en) * | 2012-09-26 | 2014-04-03 | Siemens Aktiengesellschaft | Cooling system for components in (airborne) vehicle structures |
-
1933
- 1933-03-10 GB GB7340/33A patent/GB407530A/en not_active Expired
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2423175A (en) * | 1943-11-15 | 1947-07-01 | Churchill John Adrian | Heat exchange apparatus |
| US3205964A (en) * | 1960-05-07 | 1965-09-14 | Citroen Sa Andre | Cooling-air circuits for the engines of automobile vehicles |
| US4962903A (en) * | 1987-10-19 | 1990-10-16 | Red Eye Arms, Inc. | Cooling method and apparatus for wings and other fuselage components |
| GB2234805A (en) * | 1989-08-04 | 1991-02-13 | Rolls Royce Plc | A heat exchanger arrangement for a gas turbine engine |
| WO2014048731A1 (en) * | 2012-09-26 | 2014-04-03 | Siemens Aktiengesellschaft | Cooling system for components in (airborne) vehicle structures |
| CN104812670A (en) * | 2012-09-26 | 2015-07-29 | 西门子公司 | Cooling system for components in (airborne) vehicle structures |
| US9415878B2 (en) | 2012-09-26 | 2016-08-16 | Siemens Aktiengesellschaft | Cooling system for components in (airborne) vehicle structures |
| CN104812670B (en) * | 2012-09-26 | 2016-11-16 | 西门子公司 | Aircraft and the method being used for cooling down the battery in described aircraft |
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