GB456335A - Improvements in radiator cowling for aircraft - Google Patents
Improvements in radiator cowling for aircraftInfo
- Publication number
- GB456335A GB456335A GB10418/35A GB1041835A GB456335A GB 456335 A GB456335 A GB 456335A GB 10418/35 A GB10418/35 A GB 10418/35A GB 1041835 A GB1041835 A GB 1041835A GB 456335 A GB456335 A GB 456335A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flap
- tunnel
- radiator
- underside
- slide
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 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 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
456,335. Aircraft engine accessories. ELLOR, J. E., Grandell, South Drive, Mickleover, Derby. April 3, 1935, Nos. 10418 and 11761. [Class 4] The area of the exit of a cowling for the radiator or vapour condenser of an internal combustion engine for aircraft is made variable during flight by means of a flap forming part of the wall of the tunnel and movable about a hinge at its forward end in such manner that no gap is left between the front of the flap or the sides of the flap and the adjacent walls of the tunnel through which air may escape. In one form, Fig. 1, a radiator b<2> is placed in a divergent-convergent tunnel b. A flap d is hinged at its front end on a bracket d<1> secured to the base of the tunnel and completes the end of the lower side thereof. Flap d is constituted by a hollow body of metal sheet carrying upstanding wings d<2>. A piece of sheeting f<1>, Fig. 2, attached to the bottom of the radiator closes off bracket d<1> from the airstream. Wings d<2> slide on the sides of the gap in the underside of the tunnel normally occupied by the flap d when the flap is moved outwards. In a modification, Fig. 4, a flap g pivoted at g<1> to the underside of the fuselage has pivoted thereto a flap g<3> adapted to slide at g<4> on a slide carried at the underside of the fuselage. According to one Provisional Specification, the flap means may be arranged entirely to close the outlet from the tunnel. Specification 454,266 is referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB10418/35A GB456335A (en) | 1935-04-03 | 1935-04-03 | Improvements in radiator cowling for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB10418/35A GB456335A (en) | 1935-04-03 | 1935-04-03 | Improvements in radiator cowling for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB456335A true GB456335A (en) | 1936-11-03 |
Family
ID=9967443
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB10418/35A Expired GB456335A (en) | 1935-04-03 | 1935-04-03 | Improvements in radiator cowling for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB456335A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2424335A (en) * | 1945-06-02 | 1947-07-22 | Cons Vultee Aircraft Corp | Cowling for aircraft engines |
| US2450709A (en) * | 1943-02-22 | 1948-10-05 | Lockheed Aircraft Corp | Aircraft control |
| US20120256045A1 (en) * | 2011-03-28 | 2012-10-11 | Steven Gagne | Airborne cooling system |
| US9534537B2 (en) | 2011-03-29 | 2017-01-03 | Rolls-Royce North American Technologies Inc. | Phase change material cooling system for a vehicle |
| US9797297B2 (en) | 2015-02-20 | 2017-10-24 | Pratt & Whitney Canada Corp. | Compound engine assembly with common inlet |
| US9879591B2 (en) | 2015-02-20 | 2018-01-30 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
| US9896998B2 (en) | 2015-02-20 | 2018-02-20 | Pratt & Whitney Canada Corp. | Compound engine assembly with modulated flow |
| US9932892B2 (en) | 2015-02-20 | 2018-04-03 | Pratt & Whitney Canada Corp. | Compound engine assembly with coaxial compressor and offset turbine section |
-
1935
- 1935-04-03 GB GB10418/35A patent/GB456335A/en not_active Expired
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2450709A (en) * | 1943-02-22 | 1948-10-05 | Lockheed Aircraft Corp | Aircraft control |
| US2424335A (en) * | 1945-06-02 | 1947-07-22 | Cons Vultee Aircraft Corp | Cowling for aircraft engines |
| US20120256045A1 (en) * | 2011-03-28 | 2012-10-11 | Steven Gagne | Airborne cooling system |
| US8973868B2 (en) * | 2011-03-28 | 2015-03-10 | Rolls Royce North American Technologies, Inc. | Airborne cooling system |
| US10358977B2 (en) | 2011-03-29 | 2019-07-23 | Rolls-Royce North American Technologies Inc. | Phase change material cooling system for a vehicle |
| US9534537B2 (en) | 2011-03-29 | 2017-01-03 | Rolls-Royce North American Technologies Inc. | Phase change material cooling system for a vehicle |
| US9797297B2 (en) | 2015-02-20 | 2017-10-24 | Pratt & Whitney Canada Corp. | Compound engine assembly with common inlet |
| US9879591B2 (en) | 2015-02-20 | 2018-01-30 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
| US9896998B2 (en) | 2015-02-20 | 2018-02-20 | Pratt & Whitney Canada Corp. | Compound engine assembly with modulated flow |
| US9932892B2 (en) | 2015-02-20 | 2018-04-03 | Pratt & Whitney Canada Corp. | Compound engine assembly with coaxial compressor and offset turbine section |
| US10533489B2 (en) | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Compound engine assembly with common inlet |
| US10533487B2 (en) | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
| US10883414B2 (en) | 2015-02-20 | 2021-01-05 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB456335A (en) | Improvements in radiator cowling for aircraft | |
| GB390363A (en) | An improved method of increasing the sustaining and propelling power of wings for aerial vehicles and apparatus therefor | |
| US2408867A (en) | Means for utilizing radiant heat in aircraft | |
| GB1158792A (en) | Disposable Oven-Liners | |
| US2292392A (en) | Safety device for use on aircraft employing retractible landing gears | |
| GB471371A (en) | Cooling of aircraft engines | |
| US2198229A (en) | Cooling means for aircraft engine exhaust stacks | |
| GB407530A (en) | Improvements in or relating to radiators for aircraft engines | |
| GB504737A (en) | Improvements in means for preventing ice formation on aircraft propellers | |
| US2404394A (en) | Heating shield for all types of airplane engines | |
| GB557905A (en) | Means for preventing or removing ice formations on the wings of airplanes | |
| GB472555A (en) | Improvements in aircraft | |
| US1511667A (en) | Cooling system for the power plants of aircraft | |
| SU67530A1 (en) | Device for adjusting the exit section of the channel for cooling air radiators on airplanes | |
| GB372344A (en) | Improvements in or relating to aeroplane wings | |
| USD169807S (en) | Combination automobile-airplane | |
| US2397282A (en) | Passenger body ventilator | |
| GB542653A (en) | Improvements in or relating to aircraft | |
| DK60657C (en) | Cooling air supply device at the Engine compartment in Streamlined vehicles with Rear engine. | |
| GB506446A (en) | Improvements in or relating to the air supply to carburettors of internal-combustion engines for aircraft | |
| GB592091A (en) | Improvements in or relating to gas turbine power plants for aircraft | |
| USD155404S (en) | William k. ebel albert j. subasky willem d. van zelm | |
| GB585317A (en) | Improvements in or relating to cooling arrangements for the engines of aircraft | |
| GB546067A (en) | Improvements in and relating to apparatus for preventing ice formation on aircraft or for de-icing aircraft | |
| FR874341A (en) | Device for supplying cooling air to the engine chamber of aerodynamic vehicles, with engine at the rear |