GB105051A - An Improved Device for Cooling the Motors of Aircraft. - Google Patents
An Improved Device for Cooling the Motors of Aircraft.Info
- Publication number
- GB105051A GB105051A GB18339/16A GB1833916A GB105051A GB 105051 A GB105051 A GB 105051A GB 18339/16 A GB18339/16 A GB 18339/16A GB 1833916 A GB1833916 A GB 1833916A GB 105051 A GB105051 A GB 105051A
- Authority
- GB
- United Kingdom
- Prior art keywords
- radiator
- air
- holes
- cylinders
- cooling
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
Abstract
105,051. Guyot, H. R. June 19, 1916, [Convention date]. Cylinders, cooling.-In an aeroplane, dirigible balloon, &c., the radiator and cylinders are cooled by separate air currents. A stream of cold air produced by the speed of the aircraft enters an opening b, Fig. 2, in the casing a and, after cooling the motor d, passes through a passage c<1>, formed by a pair of partitions. escaping through holes f. The radiator i of the motor is cooled by air entering holes h and escaping through holes j, f. A screw l of quick pitch may be arranged in the passage e<1>, and a fan k may be arranged behind the radiator i. In a modification, the stream of air from the opening b meets a deflector m, Fig. 3, and escapes wholly through holes j. A fan n draws in air from holes f and discharges it through the radiator i. In the tractor type of aeroplane, air entering an opening b is guided past the radiator into the casing surrounding the cylinders, the currents that cool the radiator flowing away outside of such casing. Or the air that cools the radiator is guided into a trunk which passes between the two rows of cylinders.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB18396/16A GB107574A (en) | 1916-06-29 | 1916-12-22 | An Improved Device for Cooling the Motors of Aircraft. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR105051X | 1916-06-19 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB105051A true GB105051A (en) | 1917-03-29 |
Family
ID=32241871
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB18339/16A Expired GB105051A (en) | 1916-06-19 | 1916-12-21 | An Improved Device for Cooling the Motors of Aircraft. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB105051A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2342804A2 (en) * | 2008-09-23 | 2011-07-13 | AeroVironment, Inc. | Motor air flow cooling |
| CN112455699A (en) * | 2020-11-13 | 2021-03-09 | 中国航空工业集团公司沈阳飞机设计研究所 | High fusion aircraft afterbody |
-
1916
- 1916-12-21 GB GB18339/16A patent/GB105051A/en not_active Expired
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2342804A2 (en) * | 2008-09-23 | 2011-07-13 | AeroVironment, Inc. | Motor air flow cooling |
| EP2342804A4 (en) * | 2008-09-23 | 2013-01-23 | Aerovironment Inc | Motor air flow cooling |
| US8604652B2 (en) | 2008-09-23 | 2013-12-10 | Aerovironment, Inc. | Motor air flow cooling |
| US9673673B2 (en) | 2008-09-23 | 2017-06-06 | Aerovironment, Inc. | Motor air flow cooling |
| US10873229B2 (en) | 2008-09-23 | 2020-12-22 | Aerovironment, Inc. | Motor air flow cooling |
| CN112455699A (en) * | 2020-11-13 | 2021-03-09 | 中国航空工业集团公司沈阳飞机设计研究所 | High fusion aircraft afterbody |
| CN112455699B (en) * | 2020-11-13 | 2024-01-02 | 中国航空工业集团公司沈阳飞机设计研究所 | High-fusion aircraft rear body |
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