DE2125330A1 - Strömungsmaschine - Google Patents

Strömungsmaschine

Info

Publication number
DE2125330A1
DE2125330A1 DE19712125330 DE2125330A DE2125330A1 DE 2125330 A1 DE2125330 A1 DE 2125330A1 DE 19712125330 DE19712125330 DE 19712125330 DE 2125330 A DE2125330 A DE 2125330A DE 2125330 A1 DE2125330 A1 DE 2125330A1
Authority
DE
Germany
Prior art keywords
engine
thrust
guide vanes
jet
working position
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.)
Pending
Application number
DE19712125330
Other languages
German (de)
English (en)
Inventor
William Thomas Sandiacre Nottingham; Rodgers Leonard John Spondon Derbyshire; Monaghan (Großbritannien)
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Publication of DE2125330A1 publication Critical patent/DE2125330A1/de
Pending 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
    • B64C29/005—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 fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE19712125330 1970-05-22 1971-05-21 Strömungsmaschine Pending DE2125330A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2483370 1970-05-22

Publications (1)

Publication Number Publication Date
DE2125330A1 true DE2125330A1 (de) 1972-03-23

Family

ID=10217953

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19712125330 Pending DE2125330A1 (de) 1970-05-22 1971-05-21 Strömungsmaschine

Country Status (5)

Country Link
US (1) US3731489A (https=)
DE (1) DE2125330A1 (https=)
FR (1) FR2090235A1 (https=)
GB (1) GB1258699A (https=)
IT (1) IT945914B (https=)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4066214A (en) * 1976-10-14 1978-01-03 The Boeing Company Gas turbine exhaust nozzle for controlled temperature flow across adjoining airfoils
US4252286A (en) * 1979-04-16 1981-02-24 The Boeing Company Simplified core flow thrust control device
FR2859176B1 (fr) * 2003-09-03 2005-10-28 Airbus France Aeronef pourvu d'inverseurs de poussee

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2734698A (en) * 1956-02-14 Aikplane control surface and jet
US3112616A (en) * 1962-10-18 1963-12-03 Gen Electric Thrust vectoring and modulating device
US3262645A (en) * 1963-12-30 1966-07-26 Gen Electric Thrust vectoring and modulating apparatus

Also Published As

Publication number Publication date
FR2090235A1 (https=) 1972-01-14
IT945914B (it) 1973-05-10
US3731489A (en) 1973-05-08
GB1258699A (https=) 1971-12-30

Similar Documents

Publication Publication Date Title
DE69205791T3 (de) Schubumkehrvorrichtung mit verbesserter Umlenkung der Gasstrahlen.
DE2645349C3 (de) Gasturbinen-Triebwerksanlage für Flugzeuge
DE602004001924T2 (de) Flugzeugtriebwerkscowling mit verringertem Spaltmass
DE69902618T2 (de) Schubumkehrvorrichtung mit teleskopischen Gittern
DE69602296T2 (de) Schubumkehrvorrichtung für ein Bläsertriebwerk
DE1279478B (de) Strahltriebwerk, insbesondere Mantelstromtriebwerk, mit Strahlumlenkklappen
DE2549771A1 (de) Gasturbinentriebwerk mit konvertiblen zubehoerteilen
DE2833678A1 (de) Triebwerkssystem fuer senkrecht/ kurzstart- und kurzlandeflugzeuge
DE3720578C2 (de) Gasturbinen-Mantelstrom-Triebwerk mit veränderbarem Nebenstromverhältnis
DE2623764A1 (de) Schubverstellduese fuer geraeuscharmes turbogeblaese-triebwerk und verfahren zum betrieb desselben
DE2112967A1 (de) Triebwerksanlage mit einem Gasturbinenstrahltriebwerk
DE2103397A1 (de) Einrichtung zur Lärmunterdrückung
DE69511797T2 (de) Schubumkehrvorrichtung für ein Zweikreistriebwerk mit externen Klappen
DE2853340A1 (de) Vorrichtung zum erzeugen eines vorwirbels am verdichtereingang eines turbinen-triebwerkes
DE1190799B (de) Einrichtung zur Umkehr der Schubrichtung fuer kombinierte Turbo-Staustrahltriebwerke
DE2129985A1 (de) Gasturbinenanlage
DE2154481A1 (de) Lufteinlaß für Gasturbinenstrahltriebwerke
DE2132494A1 (de) Antriebssystem fuer Senkrechtstart
DE2848240A1 (de) Gasturbinentriebwerksanlage fuer vertikalstartflugzeuge
DE2412242A1 (de) Gasturbinentriebwerk fuer stroemungsdeflektor im fankanal
DE2125330A1 (de) Strömungsmaschine
DE1186336B (de) Flugzeugtriebwerk mit einem Axialverdichter, der seitlich angeordnete Ablenkduesen speist
DE1214942B (de) Schubduesenanordnung fuer Flugzeugstrahltrieb-werke
DE1756616A1 (de) Mantelstromgasturbinenstrahltriebwerk
DE1250278B (https=)