FR636026A - Turbo-compression thruster - Google Patents

Turbo-compression thruster

Info

Publication number
FR636026A
FR636026A FR636026DA FR636026A FR 636026 A FR636026 A FR 636026A FR 636026D A FR636026D A FR 636026DA FR 636026 A FR636026 A FR 636026A
Authority
FR
France
Prior art keywords
turbo
thruster
compression
compression thruster
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 Stapelle
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 FR636026A publication Critical patent/FR636026A/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
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR636026D 1927-06-15 1927-06-15 Turbo-compression thruster Expired FR636026A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR636026T 1927-06-15

Publications (1)

Publication Number Publication Date
FR636026A true FR636026A (en) 1928-03-30

Family

ID=8994657

Family Applications (1)

Application Number Title Priority Date Filing Date
FR636026D Expired FR636026A (en) 1927-06-15 1927-06-15 Turbo-compression thruster

Country Status (1)

Country Link
FR (1) FR636026A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2425121A (en) * 1944-01-12 1947-08-05 Adolphe C Peterson Combustion jet propulsioned means
US2427845A (en) * 1941-07-08 1947-09-23 Fairey Aviat Co Ltd Periodically actuated jet motor
US2445114A (en) * 1948-07-13 Arrangement of jet propulsion
US2477683A (en) * 1942-09-30 1949-08-02 Turbo Engineering Corp Compressed air and combustion gas flow in turbine power plant
DE1025681B (en) * 1953-02-25 1958-03-06 Snecma Recoil engine
US3570766A (en) * 1969-01-15 1971-03-16 Us Navy Integral plug and strut nozzle
DE10220820A1 (en) * 2002-05-10 2003-12-04 Siegfried Witte Pulse combustion engine for aircraft has ring of nozzles in streamlined ring-shaped fairing at mouth of duct supplied with air from compressor driven by reciprocating internal combustion engine
DE102005044312B3 (en) * 2005-09-16 2007-01-11 Siegfried Witte Parting plane driving gear for aircraft comprises a valve control unit in the elongation of a valve shaft and operated by a connecting rod with a row of actuating plungers

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445114A (en) * 1948-07-13 Arrangement of jet propulsion
US2427845A (en) * 1941-07-08 1947-09-23 Fairey Aviat Co Ltd Periodically actuated jet motor
US2477683A (en) * 1942-09-30 1949-08-02 Turbo Engineering Corp Compressed air and combustion gas flow in turbine power plant
US2425121A (en) * 1944-01-12 1947-08-05 Adolphe C Peterson Combustion jet propulsioned means
DE1025681B (en) * 1953-02-25 1958-03-06 Snecma Recoil engine
US3570766A (en) * 1969-01-15 1971-03-16 Us Navy Integral plug and strut nozzle
DE10220820A1 (en) * 2002-05-10 2003-12-04 Siegfried Witte Pulse combustion engine for aircraft has ring of nozzles in streamlined ring-shaped fairing at mouth of duct supplied with air from compressor driven by reciprocating internal combustion engine
DE102005044312B3 (en) * 2005-09-16 2007-01-11 Siegfried Witte Parting plane driving gear for aircraft comprises a valve control unit in the elongation of a valve shaft and operated by a connecting rod with a row of actuating plungers

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