Author: D. J. Watts
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 74
Book Description
A Study on the Utilization of Advanced Composites in Commercial Aircraft Wing Structure: Executive Summary
Author: D. J. Watts
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 74
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 74
Book Description
Study on Utilization of Advanced Composites in Commercial Aircraft Wing Structures. Volume 1: Executive Summary
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
The effort required by commercial transport manufacturers to accomplish the transition from current construction materials and practices to extensive use of composites in aircraft wings was investigated. The engineering and manufacturing disciplines which normally participate in the design, development, and production of an aircraft were employed to ensure that all of the factors that would enter a decision to commit to production of a composite wing structure were addressed. A conceptual design of an advanced technology reduced energy aircraft provided the framework for identifying and investigating unique design aspects. A plan development effort defined the essential technology needs and formulated approaches for effecting the required wing development. The wing development program plans, resource needs, and recommendations are summarized.
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
The effort required by commercial transport manufacturers to accomplish the transition from current construction materials and practices to extensive use of composites in aircraft wings was investigated. The engineering and manufacturing disciplines which normally participate in the design, development, and production of an aircraft were employed to ensure that all of the factors that would enter a decision to commit to production of a composite wing structure were addressed. A conceptual design of an advanced technology reduced energy aircraft provided the framework for identifying and investigating unique design aspects. A plan development effort defined the essential technology needs and formulated approaches for effecting the required wing development. The wing development program plans, resource needs, and recommendations are summarized.
Study on Utilization of Advanced Composites in Commercial Aircraft Wing Structures
Author: I. Frank Sakata
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 19
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 19
Book Description
Study on Utilization of Advanced Composites in Commercial Aircraft Wing Structures, Volume 2
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 252
Book Description
A plan is defined for a composite wing development effort which will assist commercial transport manufacturers in reaching a level of technology readiness where the utilization of composite wing structure is a cost competitive option for a new aircraft production plan. The recommended development effort consists of two programs: a joint government/industry material development program and a wing structure development program. Both programs are described in detail.
Publisher:
ISBN:
Category :
Languages : en
Pages : 252
Book Description
A plan is defined for a composite wing development effort which will assist commercial transport manufacturers in reaching a level of technology readiness where the utilization of composite wing structure is a cost competitive option for a new aircraft production plan. The recommended development effort consists of two programs: a joint government/industry material development program and a wing structure development program. Both programs are described in detail.
Study on Utilization of Advanced Composites in Commercial Aircraft Wing Structures
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 243
Book Description
A study was performed to plan the effort required by commercial transport manufacturers to accomplish the transition from current construction materials and practices to extensive use of composites in wings of aircraft that enter service in the 1990 time-period. The engineering and manufacturing disciplines which normally participate in the design, development and production of a new aircraft were employed to ensure that all of the factors that would enter a Company decision to commit to production of a composite wing structure were addressed. A conceptual design of an advanced technology reduced energy aircraft provided the framework for identifying and investigating unique design aspects. A plan development effort defined the essential technology needs and formulated approaches for effecting the required wing development. Presented are two separate programs: (1) a j6int government-industry material development program, and (2) a task-oriented wing structure development program. This report presents the wing development program plans, resource needs and the supporting data for the development plans. (MM).
Publisher:
ISBN:
Category :
Languages : en
Pages : 243
Book Description
A study was performed to plan the effort required by commercial transport manufacturers to accomplish the transition from current construction materials and practices to extensive use of composites in wings of aircraft that enter service in the 1990 time-period. The engineering and manufacturing disciplines which normally participate in the design, development and production of a new aircraft were employed to ensure that all of the factors that would enter a Company decision to commit to production of a composite wing structure were addressed. A conceptual design of an advanced technology reduced energy aircraft provided the framework for identifying and investigating unique design aspects. A plan development effort defined the essential technology needs and formulated approaches for effecting the required wing development. Presented are two separate programs: (1) a j6int government-industry material development program, and (2) a task-oriented wing structure development program. This report presents the wing development program plans, resource needs and the supporting data for the development plans. (MM).
NASA Reference Publication
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 1092
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 1092
Book Description
A Study of the Utilization of Advanced Composites in Fuselage Structures of Commercial Aircraft
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 194
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 194
Book Description
Advanced Composites Wing Study Program
Author: S. T. Harvey
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Study of Utilization of Advanced Composites in Fuselage Structures of Large Transports
Author: A. C. Jackson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 112
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 112
Book Description
Ast Composite Wing Program
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781726214698
Category :
Languages : en
Pages : 98
Book Description
The Boeing Company demonstrated the application of stitched/resin infused (S/RFI) composite materials on commercial transport aircraft primary wing structures under the Advanced Subsonic technology (AST) Composite Wing contract. This report describes a weight trade study utilizing a wing torque box design applicable to a 220-passenger commercial aircraft and was used to verify the weight savings a S/RFI structure would offer compared to an identical aluminum wing box design. This trade study was performed in the AST Composite Wing program, and the overall weight savings are reported. Previous program work involved the design of a S/RFI-base-line wing box structural test component and its associated testing hardware. This detail structural design effort which is known as the "semi-span" in this report, was completed under a previous NASA contract. The full-scale wing design was based on a configuration for a MD-90-40X airplane, and the objective of this structural test component was to demonstrate the maturity of the S/RFI technology through the evaluation of a full-scale wing box/fuselage section structural test. However, scope reductions of the AST Composite Wing Program pre-vented the fabrication and evaluation of this wing box structure. Results obtained from the weight trade study, the full-scale test component design effort, fabrication, design development testing, and full-scale testing of the semi-span wing box are reported.Karal, MichaelLangley Research CenterRESIN FILM INFUSION; STRUCTURAL DESIGN; AIRCRAFT DESIGN; AIRCRAFT STRUCTURES; BODY-WING CONFIGURATIONS; COMPOSITE STRUCTURES; TRANSPORT AIRCRAFT; TORQUE; PASSENGER AIRCRAFT; ALUMINUM; COMMERCIAL AIRCRAFT; FABRICATION; FULL SCALE TESTS...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781726214698
Category :
Languages : en
Pages : 98
Book Description
The Boeing Company demonstrated the application of stitched/resin infused (S/RFI) composite materials on commercial transport aircraft primary wing structures under the Advanced Subsonic technology (AST) Composite Wing contract. This report describes a weight trade study utilizing a wing torque box design applicable to a 220-passenger commercial aircraft and was used to verify the weight savings a S/RFI structure would offer compared to an identical aluminum wing box design. This trade study was performed in the AST Composite Wing program, and the overall weight savings are reported. Previous program work involved the design of a S/RFI-base-line wing box structural test component and its associated testing hardware. This detail structural design effort which is known as the "semi-span" in this report, was completed under a previous NASA contract. The full-scale wing design was based on a configuration for a MD-90-40X airplane, and the objective of this structural test component was to demonstrate the maturity of the S/RFI technology through the evaluation of a full-scale wing box/fuselage section structural test. However, scope reductions of the AST Composite Wing Program pre-vented the fabrication and evaluation of this wing box structure. Results obtained from the weight trade study, the full-scale test component design effort, fabrication, design development testing, and full-scale testing of the semi-span wing box are reported.Karal, MichaelLangley Research CenterRESIN FILM INFUSION; STRUCTURAL DESIGN; AIRCRAFT DESIGN; AIRCRAFT STRUCTURES; BODY-WING CONFIGURATIONS; COMPOSITE STRUCTURES; TRANSPORT AIRCRAFT; TORQUE; PASSENGER AIRCRAFT; ALUMINUM; COMMERCIAL AIRCRAFT; FABRICATION; FULL SCALE TESTS...