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US3283502A Expired / Lapsed US ⏱️ 0.0 years remaining

Fuel injection system for gas turbine engines

Assignee: Individual
•
Filing: 1965-02-24
•
Granted: 1966-11-08
•
Expires: 1985-02-24
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Abstract

No abstract record available.

Inventors

  • 👤 Arthur H Lefebvre

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 11:12
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/28; F23R3/02; F23R3/04; F23R3/10; F23R3/12; F23R3/14; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 1
Claim 1
Independent Claim 54 words
A LIQUID FUEL BURNER COMPRISING A COMBUSTION CHAMBER, AN AIR DUCT OPENING INTO THE CHAMBER FOR SUPPLYING PRIMARY COMBUSTION AIR TO THE COMBUSTION SPACE THEREOF, AN AIR-BLAST ATOMISER IN SAID AIR DUCT, SAID ATOMISER INCLUDING A FUEL SUPPLY ELEMENT IN THE FORM OF A FLOODED EDGE PROJECTING INTO THE AIR STREAM AND LOCATED UPSTREAM

References Cited (Backward Citations)

GB654932A Cited
US2850875A Cited
US2920449A Cited
US2999359A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1969-11-07 1970-05-09 1970-11-08 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1973-11-07 1974-05-09 1974-11-08 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1977-11-07 1978-05-09 1978-11-08 $7700.00 Window Closed / Lapsed

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