FR2271982B1 - - Google Patents

Info

Publication number
FR2271982B1
FR2271982B1 FR7440672A FR7440672A FR2271982B1 FR 2271982 B1 FR2271982 B1 FR 2271982B1 FR 7440672 A FR7440672 A FR 7440672A FR 7440672 A FR7440672 A FR 7440672A FR 2271982 B1 FR2271982 B1 FR 2271982B1
Authority
FR
France
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
FR7440672A
Other versions
FR2271982A1 (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.)
Dornier System GmbH
Original Assignee
Dornier System 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
Priority claimed from DE19732363496 external-priority patent/DE2363496C3/de
Application filed by Dornier System GmbH filed Critical Dornier System GmbH
Publication of FR2271982A1 publication Critical patent/FR2271982A1/fr
Application granted granted Critical
Publication of FR2271982B1 publication Critical patent/FR2271982B1/fr
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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
FR7440672A 1973-12-20 1974-11-21 Expired FR2271982B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19732363496 DE2363496C3 (de) 1973-12-20 Gebläseantrieb für Fluggeräte, insbesondere Ringflügler

Publications (2)

Publication Number Publication Date
FR2271982A1 FR2271982A1 (fr) 1975-12-19
FR2271982B1 true FR2271982B1 (fr) 1979-10-12

Family

ID=5901388

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7440672A Expired FR2271982B1 (fr) 1973-12-20 1974-11-21

Country Status (4)

Country Link
CA (1) CA1005649A (fr)
FR (1) FR2271982B1 (fr)
GB (1) GB1441516A (fr)
IT (1) IT1023439B (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5062588A (en) * 1989-02-08 1991-11-05 Boeing Of Canada Ltd. Segmented rotatable nozzles
US6253550B1 (en) 1999-06-17 2001-07-03 New Power Concepts Llc Folded guide link stirling engine
US10822101B2 (en) * 2017-07-21 2020-11-03 General Electric Company Vertical takeoff and landing aircraft having a forward thrust propulsor

Also Published As

Publication number Publication date
DE2363496A1 (de) 1975-07-03
FR2271982A1 (fr) 1975-12-19
DE2363496B2 (de) 1977-04-21
CA1005649A (en) 1977-02-22
GB1441516A (en) 1976-07-07
IT1023439B (it) 1978-05-10

Similar Documents

Publication Publication Date Title
AR201758A1 (fr)
AU476761B2 (fr)
AU465372B2 (fr)
AR201235Q (fr)
AR201231Q (fr)
AU474593B2 (fr)
AU474511B2 (fr)
AU474838B2 (fr)
AU471343B2 (fr)
AU465453B2 (fr)
AU465434B2 (fr)
AU450229B2 (fr)
AU476714B2 (fr)
AR201229Q (fr)
AU466283B2 (fr)
AU476696B2 (fr)
AU472848B2 (fr)
AR199451A1 (fr)
AU477823B2 (fr)
AU461342B2 (fr)
AU471461B2 (fr)
AR200256A1 (fr)
AU476873B1 (fr)
AR210729A1 (fr)
AU477824B2 (fr)

Legal Events

Date Code Title Description
ST Notification of lapse