GB585317A - Improvements in or relating to cooling arrangements for the engines of aircraft - Google Patents
Improvements in or relating to cooling arrangements for the engines of aircraftInfo
- Publication number
- GB585317A GB585317A GB4285/45D GB428545D GB585317A GB 585317 A GB585317 A GB 585317A GB 4285/45 D GB4285/45 D GB 4285/45D GB 428545 D GB428545 D GB 428545D GB 585317 A GB585317 A GB 585317A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- flaps
- engine
- aircraft
- fan
- 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
- F01P7/00—Controlling of coolant flow
- F01P7/02—Controlling of coolant flow the coolant being cooling-air
- F01P7/10—Controlling of coolant flow the coolant being cooling-air by throttling amount of air flowing through 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
585,317. Propelling aircraft. UNITED AIRCRAFT CORPORATION. Feb. 20, 1945, No. 4284. Convention date, July 1, 1944. [Class 4] [Also in Group XXVII] In a cooling arrangement of an aircraft engine in which the flow of cooling air through a cowl 15 surrounding the engine is assisted by a fan 25, means is provided for by-passing some of the air when less cooling is required so as to maintain constant the flow of air past the fan. These means may comprise flaps 30 allowing air to be drawn in behind the engine. If the fan is in front of the engine the flaps may also be in front and allow some air to escape. Alternatively an auxiliary cowl may be placed inside the cowl 15 and arranged with flaps at the front and rear ends to by-pass part of the air through an annular space between the cowls. Exit flaps 20 are also provided. The flaps may be operated manually, or automatically in accordance with altitude.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US585317XA | 1944-07-01 | 1944-07-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB585317A true GB585317A (en) | 1947-02-04 |
Family
ID=22017392
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4285/45D Expired GB585317A (en) | 1944-07-01 | 1945-02-20 | Improvements in or relating to cooling arrangements for the engines of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB585317A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4830312A (en) * | 1987-03-26 | 1989-05-16 | Dr. Ing. H.C.F. Porshce Aktiengesellschaft | Airplane, preferably a helicopter |
-
1945
- 1945-02-20 GB GB4285/45D patent/GB585317A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4830312A (en) * | 1987-03-26 | 1989-05-16 | Dr. Ing. H.C.F. Porshce Aktiengesellschaft | Airplane, preferably a helicopter |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1069033A (en) | Improvements in or relating to gas turbine jet propulsion engines | |
GB924331A (en) | Improved combined turbo-jet-ram-jet-engine | |
GB585317A (en) | Improvements in or relating to cooling arrangements for the engines of aircraft | |
GB1073458A (en) | Improvements relating to by-pass ducted for gas-turbine aircraft engines | |
GB1228806A (en) | ||
GB1030521A (en) | Mounting arrangement for gas turbine engines in aircraft | |
GB1190364A (en) | Gas Turbine Engines | |
GB881967A (en) | Improved propulsion unit for use in vertical take-off aircraft | |
GB1032274A (en) | Mounting of ducted fan turbine engines in the tail of an aircraft | |
US2076232A (en) | Engine cowling and cooling | |
US2476643A (en) | By-pass system for cooling fans | |
GB723406A (en) | Improvements in or relating to aircraft jet engine cooling system | |
GB543219A (en) | Improvements in the direct cooling of aircraft engines | |
GB974384A (en) | An arrangement of turbo jet engines at the tail end of an aircraft | |
GB890703A (en) | An improved tiltable pod for jet power units on aircraft | |
GB983051A (en) | Aircraft | |
GB612796A (en) | Improvements in aeroplanes | |
GB1041048A (en) | Improvements in aircraft having jet-propulsion power-plants | |
GB574795A (en) | Improvement in or relating to aeroplane construction | |
GB604013A (en) | Improvements in and relating to aircraft | |
GB472555A (en) | Improvements in aircraft | |
GB942286A (en) | Gas turbine engine | |
GB723817A (en) | Improvements in or relating to jet-propelled aircraft | |
GB536189A (en) | Improvements relating to the testing of engines and airscrews | |
GB530542A (en) | Improvements in and relating to the utilisation of the exhaust gas energy of aircraft engines for propulsion purposes |