DE247395C - - Google Patents

Info

Publication number
DE247395C
DE247395C DENDAT247395D DE247395DA DE247395C DE 247395 C DE247395 C DE 247395C DE NDAT247395 D DENDAT247395 D DE NDAT247395D DE 247395D A DE247395D A DE 247395DA DE 247395 C DE247395 C DE 247395C
Authority
DE
Germany
Prior art keywords
propeller
resilient
attachment according
bracket
sheet
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.)
Active
Application number
DENDAT247395D
Other languages
German (de)
English (en)
Publication of DE247395C publication Critical patent/DE247395C/de
Active legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02Hub construction
    • B64C11/04Blade mountings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vehicle Body Suspensions (AREA)
DENDAT247395D Active DE247395C (enrdf_load_stackoverflow)

Publications (1)

Publication Number Publication Date
DE247395C true DE247395C (enrdf_load_stackoverflow)

Family

ID=506186

Family Applications (1)

Application Number Title Priority Date Filing Date
DENDAT247395D Active DE247395C (enrdf_load_stackoverflow)

Country Status (1)

Country Link
DE (1) DE247395C (enrdf_load_stackoverflow)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3784319A (en) * 1972-04-17 1974-01-08 Summa Corp Coriolis-relieving aircraft rotor assembly

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3784319A (en) * 1972-04-17 1974-01-08 Summa Corp Coriolis-relieving aircraft rotor assembly

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