← Back to Patent Explorer
US3172253A Expired / Lapsed US ⏱️ 0.0 years remaining

Combination turbo and ramjet propulsion apparatus

Assignee: Garrett Corp
•
Filing: 1959-01-02
•
Granted: 1965-03-09
•
Expires: 1979-01-02
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

No abstract record available.

Inventors

  • 👤 Schelp Helmut Rudolf
  • 👤 Hughes Frederick Ambrose

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 15:22
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/06; F02K1/15; F02K1/16; F02K1/165; F02K7/00; F02K7/10; F02K7/16; Y; Y10; Y10T; Y10T137/00; Y10T137/0536

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 122 words
PROPULSION APPARATUS COMPRISING: INNER AND OUTER SHELLS DISPOSED TO FORM A RAMJET PASSAGE OPEN AT ITS FORWARD END TO RECEIVE RAM AIR AND HAVING A CONVERGING-DIVERGING JET NOZZLE AT THE REAR END, SAID NOZZLE HAVING A THROAT BETWEEN THE CONVERGING AND DIVERGING PORTIONS; A TURBOJET ENGINE DISPOSED IN SAID INNER SHELL, THE LATTER HAVING AN INLET FOR AIR AT ITS FORWARD END AND A CONVERGING JET NOZZLE AT THE REAR END, SAID CONVERGING JET NOZZLE COMMUNICATING WITH SAID RAMJET PASSAGE ADJACENT THE THROAT OF SAID RAMJET NOZZLE AND DIRECTING THE TURBOJET ENGINE EXHAUST THERETHROUGH TO INDUCE AIR FLOW THROUGH SAID RAMJET PASSAGE; AND COMBUSTOR MEANS DISPOSED IN SAID RAMJET PASSAGE UPSTREAM FROM THE POINT OF COMMUNICATION OF SAID TURBOJET ENGINE NOZZLE THEREWITH.
Claim 2
Dependent Claim 122 words
PROPULSION APPARATUS COMPRISING: INNER AND OUTER SHELLS DISPOSED TO FORM A RAMJET PASSAGE OPEN AT ITS FORWARD END TO RECEIVE RAM AIR AND HAVING A CONVERGING-DIVERGING JET NOZZLE AT THE REAR END, SAID NOZZLE HAVING A THROAT BETWEEN THE CONVERGING AND DIVERGING PORTIONS; A TURBOJET ENGINE DISPOSED IN SAID INNER SHELL, THE LATTER HAVING AN INLET FOR AIR AT ITS FORWARD END AND A CONVERGING JET NOZZLE AT THE REAR END, SAID CONVERGING JET NOZZLE COMMUNICATING WITH SAID RAMJET PASSAGE ADJACENT THE THROAT OF SAID RAMJET NOZZLE AND DIRECTING THE TURBOJET ENGINE EXHAUST THERETHROUGH TO INDUCE AIR FLOW THROUGH SAID RAMJET PASSAGE; AND COMBUSTOR MEANS DISPOSED IN SAID RAMJET PASSAGE UPSTREAM FROM THE POINT OF COMMUNICATION OF SAID TURBOJET ENGINE NOZZLE THEREWITH.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1968-03-08 1968-09-07 1969-03-09 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1972-03-08 1972-09-07 1973-03-09 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1976-03-08 1976-09-07 1977-03-09 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag