Heavy Lift Helicopter - Advanced Technology Component Program - Rotor Blade

reportActive / Technical Report | Accession Number: ADA053423 | Open PDF

Abstract:

This report reviews the development of the Model 301 Heavy Lift Helicopter rotor blade. It describes the design, structural analysis, testing, and manufacturing process of the HLH rotor blade.

Author(s):
No Author(s) Identified
Author Organization(s):
BOEING VERTOL CO PHILADELPHIA PA
Descriptive Note:
Final rept. Jul 1971-Jul 1975
Supplementary Note:
DOI: 10.21236/ADA053423
Pagination:
0238

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
USAAMRDL-TR-77-41
Contract/Grant Number(s):
DAAJ01-71-C-0840
Monitor Series:
TR-77-41, USAAMRDL
 Subject Terms
Joint Capability Areas:
JCA_4.6_Engineering; JCA_4.6.1_General Engineering; JCA_5_Command and Control; JCA_5.3_Planning; JCA_1.2.6_Concepts; JCA_1.2.5_Lessons Learned; JCA_1.3.2_Personnel Management
Modernization Areas:
Microelectronics
Communities of Interest:
Air Platforms
Descriptor(s):
*HELICOPTER ROTORS, *ROTOR BLADES(ROTARY WINGS), FLIGHT TESTING, FIBERGLASS, COST ANALYSIS, COMPOSITE MATERIALS, STRUCTURAL ANALYSIS, AEROELASTICITY, RELIABILITY, ENGINEERING DRAWINGS, ARMY AIRCRAFT, FAIL SAFE
Field(s)/Group(s):
Helicopters
Keyword(s):
HEAVY LIFT HELICOPTERS
Report Date:
1977 Sep 01