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 aircraft

Info

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
Application number
GB3274635A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB3274635A priority Critical patent/GB468064A/en
Publication of GB468064A publication Critical patent/GB468064A/en
Expired legal-status Critical Current

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
    • B64D33/02—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.
GB3274635A 1935-11-26 1935-11-26 Improvements in air supply to carburettors of internal combustion engines for aircraft Expired GB468064A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (10)

* Cited by examiner, † Cited by third party
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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