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Title: US4265615: Fuel injection system for low emission burners
[ Derwent Title ]


Country: US United States of America

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7 pages

 
Inventor: Lohmann, Robert P.; South Windsor, CT
Markowski, Stanley J.; East Hartford, CT

Assignee: United Technologies Corporation, Hartford, CT
other patents from UNITED TECHNOLOGIES CORPORATION (597550) (approx. 5,761)
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Published / Filed: 1981-05-05 / 1978-12-11

Application Number: US1978000968652

IPC Code: Advanced: F23C 6/04; F23R 3/34;
Core: F23C 6/00; more...
IPC-7: F23D 15/02;

ECLA Code: F23C6/04B1; F23R3/34D;

U.S. Class: Current: 431/353; 060/746; 060/748; 431/158; 431/284;
Original: 431/353; 431/158; 431/284; 060/746; 060/748;

Field of Search: 431/352,353,284,158 060/39.74 B,39.65,39.69

Priority Number:
1978-12-11  US1978000968652

Abstract:     A fuel injection system for low emission burners in which the primary fuel is delivered in an annular spray into the primary combustion zone; at high power operation, secondary fuel is injected additionally in a low angle axial spray to penetrate beyond the primary zone and into the secondary combustion zone downstream of the primary zone.

Attorney, Agent or Firm: Warren, Charles A. ;

Primary / Asst. Examiners: Moy, Joseph Man-Fu;

Family: None

First Claim:
Show all 10 claims
Having thus described a typical embodiment of our invention, that which we claim as new and desire to secure by Letters Patent of the United States is:     1. A burner construction including:
  • an inlet end cap having at least one central opening therein;
  • side walls extending downstream from the end cap and having openings therein, said walls converging in a downstream direction to form a throat spaced from the end cap, and diverging again downstream of the throat;
  • an annular nozzle in the opening in the end cap for directing fuel at a large angle relative to the axis of the burner to cause primary combustion in an annulus closely adjacent to the end cap; and
  • a second nozzle within the annulus of the first nozzle directing fuel at a small angle and substantially parallel to the axis of the burner through the primary combustion, this small angle and the spacing of the throat from the end cap being such that substantially all the fuel from this nozzle passes through the throat without impingement on the converging walls for secondary combustion downstream of the throat.


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Forward References: Show 35 U.S. patent(s) that reference this one

       
U.S. References: Go to Result Set: All U.S. references   |  Forward references (35)   |   Backward references (11)   |   Citation Link

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Patent  Pub.Date  Inventor Assignee   Title
Get PDF - 3pp US2398654  1946-04 Lubbock et al.   Combustion burner
Get PDF - 4pp US2959003* 1960-11 Carlisle et al.    
Get PDF - 14pp US3048014  1962-08 Schmidt   Combustion chamber for jets and similar engines
Get PDF - 3pp US3082603* 1963-03 Hering et al.    
Get PDF - 7pp US3175361  1965-03 Schirmer et al.   Turbojet engine and its operation
Get PDF - 6pp US3576384  1971-04 Peczeli  The British American Oil Company Limited MULTINOZZLE SYSTEM FOR VORTEX BURNERS
Get PDF - 5pp US3630024  1971-12 Hopkins  General Electric Company AIR SWIRLER FOR GAS TURBINE COMBUSTOR
Get PDF - 4pp US3998581  1976-12 Hemingway et al.  Hotwork International Limited Gaseous fuel burners
Get PDF - 24pp US4006589  1977-02 Schirmer  Phillips Petroleum Company Low emission combustor with fuel flow controlled primary air flow and circumferentially directed secondary air flows
Get PDF - 5pp US4062182  1977-12 Fehler et al.  MTU Motoren-und Turbinen-Union GmbH Combustion chamber for gas turbine engines
Get PDF - 11pp US4173118  1979-11 Kawaguchi  Mitsubishi Jukogyo Kabushiki Kaisha Fuel combustion apparatus employing staged combustion
  * some details unavailable
       
Foreign References:
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Publication Date IPC Code Assignee   Title
Buy PDF - 10pp DE2636520 1978-02  F23R 1/06 Daimler-Benz AG, 7000 Stuttgart Brennkammer, insbesondere fuer Gasturbinen 
Buy PDF GB1024775 1966-04  F23C 99/00 TECALEMIT DEVELOPMENTS LTD Burner 


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