GB468064A - Improvements in air supply to carburettors of internal combustion engines for aircraft - Google Patents
Improvements in air supply to carburettors of internal combustion engines for aircraftInfo
- Publication number
- GB468064A GB468064A GB3274635A GB3274635A GB468064A GB 468064 A GB468064 A GB 468064A GB 3274635 A GB3274635 A GB 3274635A GB 3274635 A GB3274635 A GB 3274635A GB 468064 A GB468064 A GB 468064A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- radiator
- tunnel
- pipe
- drawn
- 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 title 1
- 238000010276 construction Methods 0.000 abstract 2
- 238000001816 cooling Methods 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 239000007921 spray Substances 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
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/028—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for piston engines
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
468,064. Spray carburetters. ELLOR, J. E. Nov. 26, 1935, No. 32746. [Class 7 (iii)] [Also in Group XXXIII] The air intake of a carburetter for an aircraft engine is provided with means for substituting in various proportions for a supply of cold air from the external air stream, heated air from the interior of a radiator tunnel. In the construction shown in Fig. 1, cooling-air passing through a tunnel B containing a liquid cooling radiator A or a vapour condenser, is discharged around a streamlined member D through which the air intake pipe C of a carburetter passes. Normally, cold air is drawn into the pipe C through an opening C<2> below the tunnel, but when a valve G is opened by hand or by a thermally sensitive device, air, heated by the radiator, passes through a slot F into the member D and enters the pipe C. A flap G<3> admits warm air, when desired, from the member D into the cockpit. In the construction shown in Fig. 5, the proportions of hot air, drawn through a branch H<2> opening into the radiator tunnel B, and cold air, drawn from branches H<3>, and supplied to two carburetters, are controlled by valves J. In the modification shown in Fig. 6, the cold air is supplied through a pipe K which passes through the radiator A, while the hot air is admitted behind the radiator when flaps K<2> are opened. The exit of the cooling-air from the tunnel is controlled by a flap L. Vanes M help the flow of air in the intake pipe through a right-angle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3274635A GB468064A (en) | 1935-11-26 | 1935-11-26 | Improvements in air supply to carburettors of internal combustion engines for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3274635A GB468064A (en) | 1935-11-26 | 1935-11-26 | Improvements in air supply to carburettors of internal combustion engines for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB468064A true GB468064A (en) | 1937-06-28 |
Family
ID=10343393
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3274635A Expired GB468064A (en) | 1935-11-26 | 1935-11-26 | Improvements in air supply to carburettors of internal combustion engines for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB468064A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0743247A2 (en) * | 1995-05-15 | 1996-11-20 | The Boeing Company | Passive cooling device and method for cooling an auxiliary power unit on an airoplane |
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 |
US10794280B2 (en) * | 2017-05-15 | 2020-10-06 | Pratt & Whitney Canada Corp. | Air intake for gas turbine engine |
-
1935
- 1935-11-26 GB GB3274635A patent/GB468064A/en not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0743247A2 (en) * | 1995-05-15 | 1996-11-20 | The Boeing Company | Passive cooling device and method for cooling an auxiliary power unit on an airoplane |
EP0743247A3 (en) * | 1995-05-15 | 1998-01-07 | The Boeing Company | Passive cooling device and method for cooling an auxiliary power unit on an airoplane |
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 |
US10533487B2 (en) | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
US10533489B2 (en) | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Compound engine assembly with common inlet |
US10883414B2 (en) | 2015-02-20 | 2021-01-05 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
US10794280B2 (en) * | 2017-05-15 | 2020-10-06 | Pratt & Whitney Canada Corp. | Air intake for gas turbine engine |
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