DE961151C - Anordnung von TL-Triebwerken an Flugzeugen - Google Patents

Anordnung von TL-Triebwerken an Flugzeugen

Info

Publication number
DE961151C
DE961151C DEB39166A DEB0039166A DE961151C DE 961151 C DE961151 C DE 961151C DE B39166 A DEB39166 A DE B39166A DE B0039166 A DEB0039166 A DE B0039166A DE 961151 C DE961151 C DE 961151C
Authority
DE
Germany
Prior art keywords
engines
aircraft
arrangement
longitudinal direction
arrangement according
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
DEB39166A
Other languages
English (en)
Inventor
Dipl-Ing Walter Blume
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.)
W BLUME INGENIEURBUERO fur LE
Original Assignee
W BLUME INGENIEURBUERO fur LE
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 W BLUME INGENIEURBUERO fur LE filed Critical W BLUME INGENIEURBUERO fur LE
Priority to DEB39166A priority Critical patent/DE961151C/de
Application granted granted Critical
Publication of DE961151C publication Critical patent/DE961151C/de
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plant of jet type within or attached to fuselage

Description

Hierzu 1 Blatt Zeichnungen
© 609 620/80 9.56 (609 853 3.57)

Claims (3)

PATENTANSPRÜCHE:
1. Anordnung von TL-Triebwerken an Flugzeugen, dadurch gekennzeichnet, daß die Triebwerke zur Verringerung der Lastigkeitsänderung bei verschiedenen Beladezuständen in der Längsrichtung verschiebbar angeordnet sind.
2. Anordnung nach Anspruch 1, dadurch gekennzeichnet, daß die Triebwerke am Flugzeug mittels nur in Flugzeuglängsrichtung verstellbaren Biegeträgern gelagert sind.
3. Anordnung nach Anspruch 1 und 2, dadurch gekennzeichnet, daß die Verstellung der. Triebwerke sowohl am Boden als auch im Fluge vorgenommen werden kann.
DEB39166A 1956-02-18 1956-02-18 Anordnung von TL-Triebwerken an Flugzeugen Expired DE961151C (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEB39166A DE961151C (de) 1956-02-18 1956-02-18 Anordnung von TL-Triebwerken an Flugzeugen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB39166A DE961151C (de) 1956-02-18 1956-02-18 Anordnung von TL-Triebwerken an Flugzeugen

Publications (1)

Publication Number Publication Date
DE961151C true DE961151C (de) 1957-04-04

Family

ID=6965725

Family Applications (1)

Application Number Title Priority Date Filing Date
DEB39166A Expired DE961151C (de) 1956-02-18 1956-02-18 Anordnung von TL-Triebwerken an Flugzeugen

Country Status (1)

Country Link
DE (1) DE961151C (de)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1097823B (de) * 1957-09-23 1961-01-19 Heinkel Ag Ernst Flugzeug fuer Senkrechtstart mit schwenkbaren Strahltriebwerken
US3188025A (en) * 1963-08-29 1965-06-08 Boeing Co Means for take-off, cruise, and landing of subsonic and supersonic aircraft
EP0028970A1 (de) * 1979-11-12 1981-05-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Aufhängungsvorrichtungen für Mehrkreisstrahltriebwerke
FR2935953A1 (fr) * 2008-09-18 2010-03-19 Airbus France Partie arriere d'aeronef comprenant deux semi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef.
EP2683609A1 (de) * 2011-03-09 2014-01-15 Gunnar Rosenlund Antriebssystem
DE102018000037A1 (de) * 2018-01-03 2019-07-04 Klaus Mayer In Flugzeug-Längsrichtung verschiebbare Antriebsturbinen/Antriebsturbine für die Gewichtstrimmung und Verlagerung des Flugzeugschwerpunkts während des Flugs für ein- und mehrrumpfige Flugzeuge

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1097823B (de) * 1957-09-23 1961-01-19 Heinkel Ag Ernst Flugzeug fuer Senkrechtstart mit schwenkbaren Strahltriebwerken
US3188025A (en) * 1963-08-29 1965-06-08 Boeing Co Means for take-off, cruise, and landing of subsonic and supersonic aircraft
DE1271557B (de) * 1963-08-29 1968-06-27 Boeing Co Flugzeug mit mindestens einem Strahltriebwerk zur Vortriebserzeugung
EP0028970A1 (de) * 1979-11-12 1981-05-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Aufhängungsvorrichtungen für Mehrkreisstrahltriebwerke
FR2469566A1 (fr) * 1979-11-12 1981-05-22 Snecma Perfectionnements aux dispositifs de fixation de turboreacteurs multiflux
FR2935953A1 (fr) * 2008-09-18 2010-03-19 Airbus France Partie arriere d'aeronef comprenant deux semi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef.
WO2010031958A2 (fr) 2008-09-18 2010-03-25 Airbus Operations (Societe Par Actions Simplifiee) Partie arriere d'aeronef comprenant deux demi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef
WO2010031958A3 (fr) * 2008-09-18 2010-08-26 Airbus Operations (Societe Par Actions Simplifiee) Partie arriere d'aeronef comprenant deux demi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef
JP2012502845A (ja) * 2008-09-18 2012-02-02 エアバス・オペレーションズ 航空機の内部空間内で互いに取り付けられた、エンジンを支持するための二つの準構造体を備えた航空機の後方部分
US8439300B2 (en) 2008-09-18 2013-05-14 Airbus Operations Sas Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod
CN102159460B (zh) * 2008-09-18 2013-12-18 空中客车运作股份公司 包括用于支撑发动机的一个对着另一个地安装在飞行器的内部空间中的两个半结构的飞行器的后部
RU2501711C2 (ru) * 2008-09-18 2013-12-20 Эрбюс Операсьон (Сосьете Пар Аксьон Семплифи) Хвостовая часть самолета и способ ее сборки
EP2683609A1 (de) * 2011-03-09 2014-01-15 Gunnar Rosenlund Antriebssystem
EP2683609A4 (de) * 2011-03-09 2014-10-29 Gunnar Rosenlund Antriebssystem
US9067687B2 (en) 2011-03-09 2015-06-30 Gunnar Rosenlund Propulsion system with movably mounted engines
DE102018000037A1 (de) * 2018-01-03 2019-07-04 Klaus Mayer In Flugzeug-Längsrichtung verschiebbare Antriebsturbinen/Antriebsturbine für die Gewichtstrimmung und Verlagerung des Flugzeugschwerpunkts während des Flugs für ein- und mehrrumpfige Flugzeuge

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