← Back to Patent Explorer
US3108767A Expired / Lapsed US ⏱️ 0.0 years remaining

By-pass gas turbine engine with air bleed means

Assignee: Rolls Royce PLC
•
Filing: 1961-03-09
•
Granted: 1963-10-29
•
Expires: 1981-03-09
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

No abstract record available.

Inventors

  • 👤 Eltis Ernest
  • 👤 Collins Alec Graham

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 10:36
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/06; F02K1/08; F02K3/00; F02K3/02; F02K3/025

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 119 words
A BY-PASS GAS TURBINE ENGINE COMPRISING (A) A LOW-PRESSURE AIR COMPRESSOR, (B) A HIGH-PRESSURE AIR COMPRESSOR RECEIVING COMPRESSED AIR FROM THE LOW-PRESSURE COMPRESSOR, (C) COMBUSTION EQUIPMENT IN WHICH COMPRESSED AIR FROM THE HIGH PRESSURE COMPRESSOR IS HEATED, (D) A HIGH-PRESSURE TURBINE, (E) A LOW-PRESSURE TURBINE SAID COMPRESSORS, SAID COMBUSTION EQUIPMENT AND SAID TURBINES BEING CONNECTED IN FLOW SERIES ARRANGEMENT, SAID LOW PRESSURE TURBINE DRIVING THE LOW-PRESSURE COMPRESSOR AND SAID HIGHPRESSURE TURBINE DRIVING SAID HIGH-PRESSURE COMPRESSOR, (F) A BY-PASS AIR DUCT HAVING AN INLET THERETO CONNECTED TO SAID FLOW SERIES ARRANGEMENT BETWEEN SAID COMPRESSORS TO RECEIVE AIR COMPRESSED IN THE LOWPRESSURE COMPRESSOR, (G) AN EXHAUST NOZZLE ASSEMBLY, SAID LOW-PRESSURE TURBINE AND SAID BY-PASS DUCT DELIVERING TO SAID EXHAUST NOZZLE ASSEMBLY,
Claim 2
Dependent Claim 119 words
A BY-PASS GAS TURBINE ENGINE COMPRISING (A) A LOW-PRESSURE AIR COMPRESSOR, (B) A HIGH-PRESSURE AIR COMPRESSOR RECEIVING COMPRESSED AIR FROM THE LOW-PRESSURE COMPRESSOR, (C) COMBUSTION EQUIPMENT IN WHICH COMPRESSED AIR FROM THE HIGH PRESSURE COMPRESSOR IS HEATED, (D) A HIGH-PRESSURE TURBINE, (E) A LOW-PRESSURE TURBINE SAID COMPRESSORS, SAID COMBUSTION EQUIPMENT AND SAID TURBINES BEING CONNECTED IN FLOW SERIES ARRANGEMENT, SAID LOW PRESSURE TURBINE DRIVING THE LOW-PRESSURE COMPRESSOR AND SAID HIGHPRESSURE TURBINE DRIVING SAID HIGH-PRESSURE COMPRESSOR, (F) A BY-PASS AIR DUCT HAVING AN INLET THERETO CONNECTED TO SAID FLOW SERIES ARRANGEMENT BETWEEN SAID COMPRESSORS TO RECEIVE AIR COMPRESSED IN THE LOWPRESSURE COMPRESSOR, (G) AN EXHAUST NOZZLE ASSEMBLY, SAID LOW-PRESSURE TURBINE AND SAID BY-PASS DUCT DELIVERING TO SAID EXHAUST NOZZLE ASSEMBLY,
Claim 3
Dependent Claim 36 words
AN AIRCRAFT HAVING BLOWN FLAPS AND A POWER PLANT INCLUDING A BY-PASS ENGINE ACCORDING TO CLAIM 1, SAID BLOWN FLAPS BEING CONNECTED TO SAID BLEED DUCTING TO BE OPERATED BY AIR ABSTRACTED THROUGH SAID BLEED DUCTING.

References Cited (Backward Citations)

US2464724A Cited
GB704669A Cited
US2551229A Cited
US2672726A Cited
US2873576A Cited
US3020008A Cited
FR1218064A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1966-10-28 1967-04-29 1967-10-29 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1970-10-28 1971-04-29 1971-10-29 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1974-10-28 1975-04-29 1975-10-29 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag