FR2235047A1 - Short or vertical-takeoff aircraft - has total energy of inner engine used by fan supplying two pivoting nozzles - Google Patents

Short or vertical-takeoff aircraft - has total energy of inner engine used by fan supplying two pivoting nozzles

Info

Publication number
FR2235047A1
FR2235047A1 FR7422374A FR7422374A FR2235047A1 FR 2235047 A1 FR2235047 A1 FR 2235047A1 FR 7422374 A FR7422374 A FR 7422374A FR 7422374 A FR7422374 A FR 7422374A FR 2235047 A1 FR2235047 A1 FR 2235047A1
Authority
FR
France
Prior art keywords
aircraft
short
vertical
fan
total energy
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.)
Withdrawn
Application number
FR7422374A
Other languages
English (en)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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
Priority claimed from GB3084773A external-priority patent/GB1473088A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2235047A1 publication Critical patent/FR2235047A1/fr
Withdrawn legal-status Critical Current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
    • B64C29/0066—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 with horizontal jet and jet deflector

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
FR7422374A 1973-06-28 1974-06-27 Short or vertical-takeoff aircraft - has total energy of inner engine used by fan supplying two pivoting nozzles Withdrawn FR2235047A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB3084773A GB1473088A (enExample) 1973-06-28 1973-06-28
GB433474 1974-01-30

Publications (1)

Publication Number Publication Date
FR2235047A1 true FR2235047A1 (en) 1975-01-24

Family

ID=26239049

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7422374A Withdrawn FR2235047A1 (en) 1973-06-28 1974-06-27 Short or vertical-takeoff aircraft - has total energy of inner engine used by fan supplying two pivoting nozzles

Country Status (4)

Country Link
JP (1) JPS5048700A (enExample)
DE (1) DE2430406A1 (enExample)
FR (1) FR2235047A1 (enExample)
IT (1) IT1026017B (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2596810A1 (fr) * 1986-04-08 1987-10-09 Rolls Royce Aeronef a tuyere orientable retractable, avec augmentation de la poussee d'ejection

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3013759A1 (de) * 1980-04-10 1981-12-03 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Verfahren zur verbesserung der steuerbarkeit von strahlgetriebenen flugzeugen
US12420914B2 (en) 2023-12-29 2025-09-23 Rtx Corporation Aircraft airframe component with air system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2596810A1 (fr) * 1986-04-08 1987-10-09 Rolls Royce Aeronef a tuyere orientable retractable, avec augmentation de la poussee d'ejection

Also Published As

Publication number Publication date
IT1026017B (it) 1978-09-20
DE2430406A1 (de) 1975-01-16
JPS5048700A (enExample) 1975-04-30

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Legal Events

Date Code Title Description
CA Change of address
CD Change of name or company name
ST Notification of lapse