SU163896A1 - - Google Patents

Info

Publication number
SU163896A1
SU163896A1 SU803548A SU803548A SU163896A1 SU 163896 A1 SU163896 A1 SU 163896A1 SU 803548 A SU803548 A SU 803548A SU 803548 A SU803548 A SU 803548A SU 163896 A1 SU163896 A1 SU 163896A1
Authority
SU
USSR - Soviet Union
Prior art keywords
spar
blade
frame
corrosion
nose
Prior art date
Application number
SU803548A
Other languages
English (en)
Russian (ru)
Publication of SU163896A1 publication Critical patent/SU163896A1/ru

Links

SU803548A SU163896A1 (enrdf_load_stackoverflow)

Publications (1)

Publication Number Publication Date
SU163896A1 true SU163896A1 (enrdf_load_stackoverflow)

Family

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2738888A1 (de) * 1976-08-30 1978-03-09 Boeing Co Zusammengesetzte aerodynamische rotorblatteinheit
US4316701A (en) * 1976-08-30 1982-02-23 The Boeing Company Composite aerodynamic rotor blade assembly
US4696623A (en) * 1984-12-19 1987-09-29 Aerospatiale Societe Nationale Industrielle Helicopter rotor blade made from a multispar composite material with torsion compartments and a process for manufacturing same
US4895491A (en) * 1988-06-17 1990-01-23 Environmental Elements Corp. Fan blade protection system

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2738888A1 (de) * 1976-08-30 1978-03-09 Boeing Co Zusammengesetzte aerodynamische rotorblatteinheit
US4316701A (en) * 1976-08-30 1982-02-23 The Boeing Company Composite aerodynamic rotor blade assembly
US4696623A (en) * 1984-12-19 1987-09-29 Aerospatiale Societe Nationale Industrielle Helicopter rotor blade made from a multispar composite material with torsion compartments and a process for manufacturing same
US4895491A (en) * 1988-06-17 1990-01-23 Environmental Elements Corp. Fan blade protection system

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