FR688873A - Aircraft radiator system - Google Patents
Aircraft radiator systemInfo
- Publication number
- FR688873A FR688873A FR688873DA FR688873A FR 688873 A FR688873 A FR 688873A FR 688873D A FR688873D A FR 688873DA FR 688873 A FR688873 A FR 688873A
- Authority
- FR
- France
- Prior art keywords
- radiator system
- aircraft
- aircraft radiator
- radiator
- 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; ARRANGEMENT 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR688873T | 1930-01-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR688873A true FR688873A (en) | 1930-08-29 |
Family
ID=9026966
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR688873D Expired FR688873A (en) | 1930-01-25 | 1930-01-25 | Aircraft radiator system |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR688873A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE746905C (en) * | 1940-12-24 | 1944-12-27 | Device to prevent the flow from breaking off in steep-walled diffusers | |
DE746904C (en) * | 1940-10-31 | 1944-12-27 | Device to prevent the flow from breaking off in steep-walled diffusers | |
US3205964A (en) * | 1960-05-07 | 1965-09-14 | Citroen Sa Andre | Cooling-air circuits for the engines of automobile vehicles |
FR2846941A1 (en) * | 2002-11-13 | 2004-05-14 | Soc D Const Aeronautique Auver | Process for extracting or helping to extract heat given off by an aircraft engine in the aircraft fuselage, involves forming rear fuselage into profile that accelerates air flow to extract heat from engine |
-
1930
- 1930-01-25 FR FR688873D patent/FR688873A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE746904C (en) * | 1940-10-31 | 1944-12-27 | Device to prevent the flow from breaking off in steep-walled diffusers | |
DE746905C (en) * | 1940-12-24 | 1944-12-27 | Device to prevent the flow from breaking off in steep-walled diffusers | |
US3205964A (en) * | 1960-05-07 | 1965-09-14 | Citroen Sa Andre | Cooling-air circuits for the engines of automobile vehicles |
FR2846941A1 (en) * | 2002-11-13 | 2004-05-14 | Soc D Const Aeronautique Auver | Process for extracting or helping to extract heat given off by an aircraft engine in the aircraft fuselage, involves forming rear fuselage into profile that accelerates air flow to extract heat from engine |
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