DE3913561A1 - Tragende struktur - Google Patents

Tragende struktur

Info

Publication number
DE3913561A1
DE3913561A1 DE3913561A DE3913561A DE3913561A1 DE 3913561 A1 DE3913561 A1 DE 3913561A1 DE 3913561 A DE3913561 A DE 3913561A DE 3913561 A DE3913561 A DE 3913561A DE 3913561 A1 DE3913561 A1 DE 3913561A1
Authority
DE
Germany
Prior art keywords
fibre
structure according
fibers
metallic
fiber
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.)
Granted
Application number
DE3913561A
Other languages
German (de)
English (en)
Other versions
DE3913561C2 (enExample
Inventor
Siegfried Dipl Ing Roth
Hans-Wolfgang Dr Rer Schroeder
Norbert Dipl Ing Himmel
Werner Dr Ing Poenitzsch
Wolfgang Dipl Ing Uhse
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.)
Fairchild Dornier GmbH
Original Assignee
Dornier Luftfahrt 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 Dornier Luftfahrt GmbH filed Critical Dornier Luftfahrt GmbH
Priority to DE3913561A priority Critical patent/DE3913561A1/de
Publication of DE3913561A1 publication Critical patent/DE3913561A1/de
Application granted granted Critical
Publication of DE3913561C2 publication Critical patent/DE3913561C2/de
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/40—Sound or heat insulation, e.g. using insulation blankets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52—Protection, safety or emergency devices; Survival aids
    • B64G1/58—Thermal protection, e.g. heat shields
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Critical Care (AREA)
  • Emergency Medicine (AREA)
  • General Health & Medical Sciences (AREA)
  • Remote Sensing (AREA)
  • Laminated Bodies (AREA)
DE3913561A 1989-04-25 1989-04-25 Tragende struktur Granted DE3913561A1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE3913561A DE3913561A1 (de) 1989-04-25 1989-04-25 Tragende struktur

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3913561A DE3913561A1 (de) 1989-04-25 1989-04-25 Tragende struktur

Publications (2)

Publication Number Publication Date
DE3913561A1 true DE3913561A1 (de) 1990-10-31
DE3913561C2 DE3913561C2 (enExample) 1992-03-05

Family

ID=6379396

Family Applications (1)

Application Number Title Priority Date Filing Date
DE3913561A Granted DE3913561A1 (de) 1989-04-25 1989-04-25 Tragende struktur

Country Status (1)

Country Link
DE (1) DE3913561A1 (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5377935A (en) * 1993-05-14 1995-01-03 Interferometrics Inc. Spacecraft ceramic protective shield
US6607851B2 (en) 2001-10-26 2003-08-19 The Boeing Company Multi-layer ceramic fiber insulation tile

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19945586B4 (de) * 1999-09-23 2005-03-31 Eads Space Transportation Gmbh Verwendung eines Thermalschutzsystems

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4344591A (en) * 1979-09-05 1982-08-17 The United States Of America Asrepresented By The Administrator Of The National Aeronautics And Space Administration Multiwall thermal protection system
US4706912A (en) * 1985-12-16 1987-11-17 The United States Of America As Represented By The Secretary Of The Army Structural external insulation for hypersonic missiles

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4344591A (en) * 1979-09-05 1982-08-17 The United States Of America Asrepresented By The Administrator Of The National Aeronautics And Space Administration Multiwall thermal protection system
US4706912A (en) * 1985-12-16 1987-11-17 The United States Of America As Represented By The Secretary Of The Army Structural external insulation for hypersonic missiles

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5377935A (en) * 1993-05-14 1995-01-03 Interferometrics Inc. Spacecraft ceramic protective shield
US6607851B2 (en) 2001-10-26 2003-08-19 The Boeing Company Multi-layer ceramic fiber insulation tile
US6699342B2 (en) 2001-10-26 2004-03-02 The Boeing Company Method of producing a multi-layer ceramic fiber insulation tile

Also Published As

Publication number Publication date
DE3913561C2 (enExample) 1992-03-05

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Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee