GB491616A - Improvements in internal combustion turbines - Google Patents

Improvements in internal combustion turbines

Info

Publication number
GB491616A
GB491616A GB16523/37A GB1652337A GB491616A GB 491616 A GB491616 A GB 491616A GB 16523/37 A GB16523/37 A GB 16523/37A GB 1652337 A GB1652337 A GB 1652337A GB 491616 A GB491616 A GB 491616A
Authority
GB
United Kingdom
Prior art keywords
internal combustion
turbines
combustion turbines
fins
ribs
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
GB16523/37A
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 GB16523/37A priority Critical patent/GB491616A/en
Priority to US212522A priority patent/US2174266A/en
Publication of GB491616A publication Critical patent/GB491616A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air-Conditioning For Vehicles (AREA)

Abstract

491,616. Gas turbines. JACKSON, T., and STANLEY, G. W. June 15, 1937, No. 16523. [Class 110 (iii)] In turbines of the kind described in Specification 452,297, the internal ribs or fins F of the combustion chambers are curved transversely and arranged spirally or at an inclination to the surface of the chamber. The edges of the fins may be tapered to a fine edge or be serrated as at f. The ribs may be built with end rings F<1> as a unit to facilitate replacement.
GB16523/37A 1937-06-15 1937-06-15 Improvements in internal combustion turbines Expired GB491616A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB16523/37A GB491616A (en) 1937-06-15 1937-06-15 Improvements in internal combustion turbines
US212522A US2174266A (en) 1937-06-15 1938-06-08 Internal combustion turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB16523/37A GB491616A (en) 1937-06-15 1937-06-15 Improvements in internal combustion turbines

Publications (1)

Publication Number Publication Date
GB491616A true GB491616A (en) 1938-09-06

Family

ID=10078869

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16523/37A Expired GB491616A (en) 1937-06-15 1937-06-15 Improvements in internal combustion turbines

Country Status (2)

Country Link
US (1) US2174266A (en)
GB (1) GB491616A (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE904255C (en) * 1944-07-12 1954-02-15 Daimler Benz Ag Combustion chamber for jet engines
US2620122A (en) * 1945-10-09 1952-12-02 Herman H Curry Combination propeller and diffuser inlet assembly
US2743163A (en) * 1952-02-18 1956-04-24 Ryan Aeronautical Co Inert gas generator
US2858672A (en) * 1954-10-29 1958-11-04 Gen Electric Monofuel decomposition apparatus
US8438834B2 (en) * 2009-03-30 2013-05-14 Alliant Techsystems Inc. Helical cross flow (HCF) pulse detonation engine
KR102343001B1 (en) * 2020-07-06 2021-12-23 두산중공업 주식회사 Nozzle for combustor, combustor, and gas turbine including the same
KR102363091B1 (en) * 2020-07-06 2022-02-14 두산중공업 주식회사 Nozzle for combustor, combustor, and gas turbine including the same
US11274603B1 (en) * 2020-08-21 2022-03-15 Bob Burkett Electric heating systems and methods for gas turbine engines and jet engines
KR102663869B1 (en) * 2022-01-18 2024-05-03 두산에너빌리티 주식회사 Nozzle for combustor, combustor, and gas turbine including the same

Also Published As

Publication number Publication date
US2174266A (en) 1939-09-26

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