FR972222A - Explosion or internal combustion engine exhaust energy utilization system applicable to the propulsion of aircraft - Google Patents

Explosion or internal combustion engine exhaust energy utilization system applicable to the propulsion of aircraft

Info

Publication number
FR972222A
FR972222A FR972222DA FR972222A FR 972222 A FR972222 A FR 972222A FR 972222D A FR972222D A FR 972222DA FR 972222 A FR972222 A FR 972222A
Authority
FR
France
Prior art keywords
propulsion
explosion
aircraft
combustion engine
internal combustion
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
Other languages
French (fr)
Inventor
Joseph Bayon
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 filed Critical
Application granted granted Critical
Publication of FR972222A publication Critical patent/FR972222A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
    • F02K5/02—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan the engine being of the reciprocating-piston type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N5/00—Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR972222D 1948-09-24 1948-09-24 Explosion or internal combustion engine exhaust energy utilization system applicable to the propulsion of aircraft Expired FR972222A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR972222T 1948-09-24

Publications (1)

Publication Number Publication Date
FR972222A true FR972222A (en) 1951-01-26

Family

ID=9515798

Family Applications (1)

Application Number Title Priority Date Filing Date
FR972222D Expired FR972222A (en) 1948-09-24 1948-09-24 Explosion or internal combustion engine exhaust energy utilization system applicable to the propulsion of aircraft

Country Status (1)

Country Link
FR (1) FR972222A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3069848A (en) * 1959-02-23 1962-12-25 Rolls Royce Jet lift gas turbine engines having thrust augmenting and silencing means
US3091922A (en) * 1960-02-12 1963-06-04 John A Johnson Multi-stage parallel flow turbo-fan
DE1209807B (en) * 1959-02-23 1966-01-27 Rolls Royce Gas turbine jet engine with a jet device that accelerates the ambient air in an outer ring duct

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3069848A (en) * 1959-02-23 1962-12-25 Rolls Royce Jet lift gas turbine engines having thrust augmenting and silencing means
DE1209807B (en) * 1959-02-23 1966-01-27 Rolls Royce Gas turbine jet engine with a jet device that accelerates the ambient air in an outer ring duct
US3091922A (en) * 1960-02-12 1963-06-04 John A Johnson Multi-stage parallel flow turbo-fan

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