FR1232710A - Two-circuit reactor with separate mounting of a shaft drive train and thrust nozzle - Google Patents

Two-circuit reactor with separate mounting of a shaft drive train and thrust nozzle

Info

Publication number
FR1232710A
FR1232710A FR802281A FR802281A FR1232710A FR 1232710 A FR1232710 A FR 1232710A FR 802281 A FR802281 A FR 802281A FR 802281 A FR802281 A FR 802281A FR 1232710 A FR1232710 A FR 1232710A
Authority
FR
France
Prior art keywords
drive train
shaft drive
separate mounting
thrust nozzle
circuit reactor
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
FR802281A
Other languages
French (fr)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BMW Triebwerkbau GmbH
Original Assignee
BMW Triebwerkbau GmbH
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 by BMW Triebwerkbau GmbH filed Critical BMW Triebwerkbau GmbH
Application granted granted Critical
Publication of FR1232710A publication Critical patent/FR1232710A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0075—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors the motors being tiltable relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR802281A 1958-09-22 1959-08-07 Two-circuit reactor with separate mounting of a shaft drive train and thrust nozzle Expired FR1232710A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1232710X 1958-09-22

Publications (1)

Publication Number Publication Date
FR1232710A true FR1232710A (en) 1960-10-11

Family

ID=7735202

Family Applications (1)

Application Number Title Priority Date Filing Date
FR802281A Expired FR1232710A (en) 1958-09-22 1959-08-07 Two-circuit reactor with separate mounting of a shaft drive train and thrust nozzle

Country Status (1)

Country Link
FR (1) FR1232710A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3162397A (en) * 1961-08-04 1964-12-22 Snecma V/stol aircraft with directional control nozzle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3162397A (en) * 1961-08-04 1964-12-22 Snecma V/stol aircraft with directional control nozzle

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