GB528774A - Two stage compression arrangement for aircraft engines - Google Patents

Two stage compression arrangement for aircraft engines

Info

Publication number
GB528774A
GB528774A GB14422/39A GB1442239A GB528774A GB 528774 A GB528774 A GB 528774A GB 14422/39 A GB14422/39 A GB 14422/39A GB 1442239 A GB1442239 A GB 1442239A GB 528774 A GB528774 A GB 528774A
Authority
GB
United Kingdom
Prior art keywords
stage compression
aircraft engines
compression arrangement
shaft
crank
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
GB14422/39A
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
Publication of GB528774A publication Critical patent/GB528774A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00—Engines characterised by provision of pumps for charging or scavenging
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/33—Compressors for piston combustion engines
    • F02M2700/331—Charging and scavenging compressors
    • F02M2700/336—Arrangements thereof on the engine

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)

Abstract

528,774. Pumps. POTEZ, H. C. A. May 15, 1939, No. 14422. Convention date, May 16, 1938. [Class 7 (ii)] In two-stage compression, one pump A is arranged with its axis at right-angles to that of the crank-shaft and the other pump B with its axis parallel to the crank-shaft. The drive is taken from both ends of the shaft. A clutch 19 permits idling of the rotor 9. Cooling ribs 22 are provided on the conduit 5, and carburation is effected at the elbow 23.
GB14422/39A 1938-05-16 1939-05-15 Two stage compression arrangement for aircraft engines Expired GB528774A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR528774X 1938-05-16

Publications (1)

Publication Number Publication Date
GB528774A true GB528774A (en) 1940-11-06

Family

ID=8922286

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14422/39A Expired GB528774A (en) 1938-05-16 1939-05-15 Two stage compression arrangement for aircraft engines

Country Status (1)

Country Link
GB (1) GB528774A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2653591A (en) * 1948-06-17 1953-09-29 United Aircraft Corp Supercharger arrangement

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2653591A (en) * 1948-06-17 1953-09-29 United Aircraft Corp Supercharger arrangement

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