GB475123A - Improvements in cowled motive-power plants - Google Patents
Improvements in cowled motive-power plantsInfo
- Publication number
- GB475123A GB475123A GB13656/36A GB1365636A GB475123A GB 475123 A GB475123 A GB 475123A GB 13656/36 A GB13656/36 A GB 13656/36A GB 1365636 A GB1365636 A GB 1365636A GB 475123 A GB475123 A GB 475123A
- Authority
- GB
- United Kingdom
- Prior art keywords
- radiator
- air
- case
- partitions
- lubricating oil
- 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
- 239000010687 lubricating oil Substances 0.000 abstract 2
- 238000005192 partition Methods 0.000 abstract 2
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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 POWERÂ PLANTSÂ 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
475,123. Propelling aircraft. SOC. FRANCAISE HISPANO-SUIZA. May 14, 1936, No. 13656. Convention date, Dec. 24, 1935. [Class 4] [Also in Group XIII] A radiator of arcuate cross-section surrounds the crank-case of, e.g. an aircraft engine, on the side opposite the cylinders. In one form a V-cylinder aircraft engine is mounted on triangulated framework 5 and is surrounded by a cowl 2 having an adjustable air inlet 7 and an air outlet 9. The radiator 3 is arranged in the air stream and under the engine. The radiator may be rectangular or of polygonal longitudinal section. In a modification, two radiators, one for water and the other for lubricating oil, are arranged one above the other and in this case the air for each radiator may be guided by partitions. The radiator for the lubricating oil may be embedded in or disposed between two parts of or behind the radiator 3 as shown in Fig. 8. In this latter case, partitions may be provided to separate the air supplied to and passing through each radiator. The invention may be applied to inverted-V-cylinder engines.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE475123X | 1935-12-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB475123A true GB475123A (en) | 1937-11-15 |
Family
ID=3870222
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB13656/36A Expired GB475123A (en) | 1935-12-24 | 1936-05-14 | Improvements in cowled motive-power plants |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB475123A (en) |
-
1936
- 1936-05-14 GB GB13656/36A patent/GB475123A/en not_active Expired
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