Abstract
Modifications are being made to the CH-47 Drive System in order to increase power capacity and lower operating costs. In addition to designing in capacity improvements to the CH-47 Drive System, Boeing is investigating weight reduction technologies for the CH-47F Block II Program. One opportunity is focused on advancing the Manufacturing Readiness Level (MRL) and Technology Readiness Level (TRL) of a Fiber-Reinforced Polymer (Composite) Section of the Chinook's Aft Rotor Shaft. The Composite Section is calculated to save over 50 pounds in the Aft Section of the aircraft. The Hybrid Steel/Composite Aft Rotor Shaft Development was split into a phased program to advance the MRL and TRL while keeping program risk low. Early phases defined component requirements and developed a preliminary ply table to validate weight predictions. The development then moved into manufacturability studies, revising the preliminary ply table and fabricating and inspecting a Half-Length Composite Shaft (Half-Shaft). As the design matures, future phases will encompass full-scale shaft fabrication and risk-reduction and qualification tests. This paper summarizes the interim design considerations of a full-scale hybrid composite shaft and fabrication and inspection of a thick-walled composite tube to develop the technology.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 1760-1769 |
| Number of pages | 10 |
| Journal | Annual Forum Proceedings - AHS International |
| State | Published - Jan 1 2017 |
| Externally published | Yes |
| Event | 73rd American Helicopter Society International Annual Forum and Technology Display 2017 - Fort Worth, United States Duration: May 9 2017 → May 11 2017 |
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All Science Journal Classification (ASJC) codes
- Engineering(all)
Cite this
Thick-walled composite cylinder fabrication to support composite rotor shaft development for CH-47 chinook. / Darmstadt, Patrick R.; Hendrickson, Anthony; Moore, Jeron; Barbato, Kelli; Vitlip, Robert; Hu, Zhenning.
In: Annual Forum Proceedings - AHS International, 01.01.2017, p. 1760-1769.Research output: Contribution to journal › Conference article
}
TY - JOUR
T1 - Thick-walled composite cylinder fabrication to support composite rotor shaft development for CH-47 chinook
AU - Darmstadt, Patrick R.
AU - Hendrickson, Anthony
AU - Moore, Jeron
AU - Barbato, Kelli
AU - Vitlip, Robert
AU - Hu, Zhenning
PY - 2017/1/1
Y1 - 2017/1/1
N2 - Modifications are being made to the CH-47 Drive System in order to increase power capacity and lower operating costs. In addition to designing in capacity improvements to the CH-47 Drive System, Boeing is investigating weight reduction technologies for the CH-47F Block II Program. One opportunity is focused on advancing the Manufacturing Readiness Level (MRL) and Technology Readiness Level (TRL) of a Fiber-Reinforced Polymer (Composite) Section of the Chinook's Aft Rotor Shaft. The Composite Section is calculated to save over 50 pounds in the Aft Section of the aircraft. The Hybrid Steel/Composite Aft Rotor Shaft Development was split into a phased program to advance the MRL and TRL while keeping program risk low. Early phases defined component requirements and developed a preliminary ply table to validate weight predictions. The development then moved into manufacturability studies, revising the preliminary ply table and fabricating and inspecting a Half-Length Composite Shaft (Half-Shaft). As the design matures, future phases will encompass full-scale shaft fabrication and risk-reduction and qualification tests. This paper summarizes the interim design considerations of a full-scale hybrid composite shaft and fabrication and inspection of a thick-walled composite tube to develop the technology.
AB - Modifications are being made to the CH-47 Drive System in order to increase power capacity and lower operating costs. In addition to designing in capacity improvements to the CH-47 Drive System, Boeing is investigating weight reduction technologies for the CH-47F Block II Program. One opportunity is focused on advancing the Manufacturing Readiness Level (MRL) and Technology Readiness Level (TRL) of a Fiber-Reinforced Polymer (Composite) Section of the Chinook's Aft Rotor Shaft. The Composite Section is calculated to save over 50 pounds in the Aft Section of the aircraft. The Hybrid Steel/Composite Aft Rotor Shaft Development was split into a phased program to advance the MRL and TRL while keeping program risk low. Early phases defined component requirements and developed a preliminary ply table to validate weight predictions. The development then moved into manufacturability studies, revising the preliminary ply table and fabricating and inspecting a Half-Length Composite Shaft (Half-Shaft). As the design matures, future phases will encompass full-scale shaft fabrication and risk-reduction and qualification tests. This paper summarizes the interim design considerations of a full-scale hybrid composite shaft and fabrication and inspection of a thick-walled composite tube to develop the technology.
UR - http://www.scopus.com/inward/record.url?scp=85029628880&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85029628880&partnerID=8YFLogxK
M3 - Conference article
AN - SCOPUS:85029628880
SP - 1760
EP - 1769
JO - Annual Forum Proceedings - AHS International
JF - Annual Forum Proceedings - AHS International
SN - 1552-2938
ER -