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GB105051A - An Improved Device for Cooling the Motors of Aircraft. - Google Patents

An Improved Device for Cooling the Motors of Aircraft.

Info

Publication number
GB105051A
GB105051A GB18339/16A GB1833916A GB105051A GB 105051 A GB105051 A GB 105051A GB 18339/16 A GB18339/16 A GB 18339/16A GB 1833916 A GB1833916 A GB 1833916A GB 105051 A GB105051 A GB 105051A
Authority
GB
United Kingdom
Prior art keywords
radiator
air
holes
cylinders
cooling
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
GB18339/16A
Inventor
Henri Raymond Guyot
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 GB18396/16A priority Critical patent/GB107574A/en
Publication of GB105051A publication Critical patent/GB105051A/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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08—Arrangement 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)
  • Motor Or Generator Cooling System (AREA)

Abstract

105,051. Guyot, H. R. June 19, 1916, [Convention date]. Cylinders, cooling.-In an aeroplane, dirigible balloon, &c., the radiator and cylinders are cooled by separate air currents. A stream of cold air produced by the speed of the aircraft enters an opening b, Fig. 2, in the casing a and, after cooling the motor d, passes through a passage c<1>, formed by a pair of partitions. escaping through holes f. The radiator i of the motor is cooled by air entering holes h and escaping through holes j, f. A screw l of quick pitch may be arranged in the passage e<1>, and a fan k may be arranged behind the radiator i. In a modification, the stream of air from the opening b meets a deflector m, Fig. 3, and escapes wholly through holes j. A fan n draws in air from holes f and discharges it through the radiator i. In the tractor type of aeroplane, air entering an opening b is guided past the radiator into the casing surrounding the cylinders, the currents that cool the radiator flowing away outside of such casing. Or the air that cools the radiator is guided into a trunk which passes between the two rows of cylinders.
GB18339/16A 1916-06-19 1916-12-21 An Improved Device for Cooling the Motors of Aircraft. Expired GB105051A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB18396/16A GB107574A (en) 1916-06-29 1916-12-22 An Improved Device for Cooling the Motors of Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR105051X 1916-06-19

Publications (1)

Publication Number Publication Date
GB105051A true GB105051A (en) 1917-03-29

Family

ID=32241871

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18339/16A Expired GB105051A (en) 1916-06-19 1916-12-21 An Improved Device for Cooling the Motors of Aircraft.

Country Status (1)

Country Link
GB (1) GB105051A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2342804A4 (en) * 2008-09-23 2013-01-23 Aerovironment Inc Motor air flow cooling
CN112455699A (en) * 2020-11-13 2021-03-09 中国航空工业集团公司沈阳飞机设计研究所 High fusion aircraft afterbody

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2342804A4 (en) * 2008-09-23 2013-01-23 Aerovironment Inc Motor air flow cooling
US8604652B2 (en) 2008-09-23 2013-12-10 Aerovironment, Inc. Motor air flow cooling
US9673673B2 (en) 2008-09-23 2017-06-06 Aerovironment, Inc. Motor air flow cooling
US10873229B2 (en) 2008-09-23 2020-12-22 Aerovironment, Inc. Motor air flow cooling
CN112455699A (en) * 2020-11-13 2021-03-09 中国航空工业集团公司沈阳飞机设计研究所 High fusion aircraft afterbody
CN112455699B (en) * 2020-11-13 2024-01-02 中国航空工业集团公司沈阳飞机设计研究所 High-fusion aircraft rear body

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