Supersonic Transport Aircraft Engine Phase Ii B Development Program Fuel Control System Study Appendix A

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Supersonic Transport Aircraft Engine. Phase Ii-b. Development Program Fuel Control System Study. Appendix a

Author : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.
Publisher :
ISBN 13 :
Total Pages : 187 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Supersonic Transport Aircraft Engine. Phase Ii-b. Development Program Fuel Control System Study. Appendix a by : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.

Download or read book Supersonic Transport Aircraft Engine. Phase Ii-b. Development Program Fuel Control System Study. Appendix a written by PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT. and published by . This book was released on 1965 with total page 187 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of the current program was to continue the design and development of critical components, to analyze and implement any changes in control design resulting from changes in engine requirements, and to develop a control installation concept compatible with envelope limitations dictated by the engine installation.

Supersonic Transport Aircraft Engine. Phase Ii-b. Development Program Fuel Control System Study. Appendix B

Author : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.
Publisher :
ISBN 13 :
Total Pages : 164 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Supersonic Transport Aircraft Engine. Phase Ii-b. Development Program Fuel Control System Study. Appendix B by : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.

Download or read book Supersonic Transport Aircraft Engine. Phase Ii-b. Development Program Fuel Control System Study. Appendix B written by PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT. and published by . This book was released on 1965 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hamilton Standard, under contract to Pratt and Whitney Aircraft, has conducted a design and development study to conceive and optimize, within contract and time limitations, a fuel control system for the P and WA SST engine. This effort consisted of design and analytical studies, material investigations, and development efforts necessary to adapt current state-of-the-art concepts and new concepts into a fuel control system compatible with the SST environments, envelope requirements, and accuracy tolerances specified for this application. The system decided upon and studied is a hydromechanical unitized concept featuring high reliability, ease of maintenance, durability, and low overall system weight. This report covers all studies conducted under Phase 2 B of the contract for the fuel control system as well as Hamilton Standard funded elastomeric seal development work.

Development of a Supersonic Transport Aircraft Engine. Phase Ii-c. Appendix A. Control System Review

Author : PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FL FLORIDA RESEARCH AND DEVELOPMEN T CENTER.
Publisher :
ISBN 13 :
Total Pages : 434 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Development of a Supersonic Transport Aircraft Engine. Phase Ii-c. Appendix A. Control System Review by : PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FL FLORIDA RESEARCH AND DEVELOPMEN T CENTER.

Download or read book Development of a Supersonic Transport Aircraft Engine. Phase Ii-c. Appendix A. Control System Review written by PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FL FLORIDA RESEARCH AND DEVELOPMEN T CENTER. and published by . This book was released on 1966 with total page 434 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report covers the control system programs conducted during the first 7 months of the Phase II-C contract, and includes the following items: A detailed description of the fuel control systems and components being procured for initial test engines; Results of analytical and bench test evaluation of the system and various components; Detailed description of the fuel control system and components presently being considered for the prototype engine, including certain alternative approaches; and Results of analytical investigations of the system.

Technical Abstract Bulletin

Author : Defense Documentation Center (U.S.)
Publisher :
ISBN 13 :
Total Pages : 784 pages
Book Rating : 4.:/5 (1 download)

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Book Synopsis Technical Abstract Bulletin by : Defense Documentation Center (U.S.)

Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:

SUPERSONIC TRANSPORT AIRCRAFT ENGINE PHASE II-B DEVELOPMENT PROGRAM

Author :
Publisher :
ISBN 13 :
Total Pages : 467 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis SUPERSONIC TRANSPORT AIRCRAFT ENGINE PHASE II-B DEVELOPMENT PROGRAM by :

Download or read book SUPERSONIC TRANSPORT AIRCRAFT ENGINE PHASE II-B DEVELOPMENT PROGRAM written by and published by . This book was released on 1965 with total page 467 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Development of a Supersonic Transport Aircraft Engine - Phase Ii-b

Author : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.
Publisher :
ISBN 13 :
Total Pages : 21 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Development of a Supersonic Transport Aircraft Engine - Phase Ii-b by : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.

Download or read book Development of a Supersonic Transport Aircraft Engine - Phase Ii-b written by PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT. and published by . This book was released on 1965 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: Current developments included: (1) The detailed work plan for the Phase II-B development effort was submitted to the FAA on 11 January 1965; (2) Meetings were held to discuss installation and performance problems and the Phase II-B fuel control program; (3) Detailed design of the STF-219 engine was started on the basis of a 700 lb/sec airflow and a cruising velocity of Mach 2.7; (4) A total of 557 endurance cycles (alternating between idle and 2300 F turbine inlet temperature) were completed on the JT4 high spool engine; (5) Reassembly of the full-scale duct burner rig was completed and testing was initiated; (6) Studies were conducted to determine the effect of inlet airflow Mach number on compressor noise attenuation; (7) A laboratory investigation was started on ASTM Type fuels samples furnished by twelve refineries. (Author).

Supersonic Transport Engine Development. Appendix A. Fuel Control System Study

Author : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.
Publisher :
ISBN 13 :
Total Pages : 146 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Supersonic Transport Engine Development. Appendix A. Fuel Control System Study by : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.

Download or read book Supersonic Transport Engine Development. Appendix A. Fuel Control System Study written by PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT. and published by . This book was released on 1964 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt: The control design which was evolved during Phase I was reviewed in more detail from the standpoint of reliability, maintenance features, effect on engine plumbing, disassembly and assembly techniques, size, weight and materials, and economic considerations in the design approach. Detailed investigations were conducted in areas in which design substantiation was considered to be necessary. Developmental testing was specifically directed toward continuing the evaluation of the fan pressure-ratio sensor and the fluid state latch mechanism which had been fabricated during the previous phase. The testing was intended to determine the performance capability of the two critical subsystems under SST environmental conditions of pressure, temperature, and vibration.

Supersonic Transport Engine Development. Appendix B. Fuel Control System Study

Author : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.
Publisher :
ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Supersonic Transport Engine Development. Appendix B. Fuel Control System Study by : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.

Download or read book Supersonic Transport Engine Development. Appendix B. Fuel Control System Study written by PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT. and published by . This book was released on 1964 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Control schematic revisions dictated by new engine requirements have been investigated and are described in the report. Some control components have been reviewed and modified from the standpoint of one or more of the following objectives: improved performance, reduced weight, and decreased size. A packaging and arrangement feasibility study has resulted in a reduction in control size which is compatible with the latest envelope requirements. Continued development testing of the pressure ratio sensor has shown very satisfactory performance when operating in a vibratory field. The elastomeric seal development program has indicated that seals capable of satisfactory performance can be developed. Satisfactory dynamic performance has been demonstrated by the results of the control transient studies performed on computers. (Author).

SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-B DEVELOPMENT PROGRAM

Author :
Publisher :
ISBN 13 :
Total Pages : 245 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-B DEVELOPMENT PROGRAM by :

Download or read book SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-B DEVELOPMENT PROGRAM written by and published by . This book was released on 1965 with total page 245 pages. Available in PDF, EPUB and Kindle. Book excerpt:

SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-B. DEVELOPMENT PROGRAM

Author :
Publisher :
ISBN 13 :
Total Pages : 600 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-B. DEVELOPMENT PROGRAM by :

Download or read book SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-B. DEVELOPMENT PROGRAM written by and published by . This book was released on 1965 with total page 600 pages. Available in PDF, EPUB and Kindle. Book excerpt:

SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-B. DEVELOPMENT PROGRAM

Author :
Publisher :
ISBN 13 :
Total Pages : 289 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-B. DEVELOPMENT PROGRAM by :

Download or read book SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-B. DEVELOPMENT PROGRAM written by and published by . This book was released on 1965 with total page 289 pages. Available in PDF, EPUB and Kindle. Book excerpt:

SUPERSONIC TRANSPORT PROGRAM. PHASE IIB.

Author : BOEING CO RENTON WA.
Publisher :
ISBN 13 :
Total Pages : 180 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis SUPERSONIC TRANSPORT PROGRAM. PHASE IIB. by : BOEING CO RENTON WA.

Download or read book SUPERSONIC TRANSPORT PROGRAM. PHASE IIB. written by BOEING CO RENTON WA. and published by . This book was released on 1965 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Configuration Design and Development -- Landing gear study, Body depth study, Vertical tail studies, Weight review, Interior arrangement development, and Landing gear deflection systems; Performance -- Wind tunnel testing, Performance analysis, Stability and control, Flight dynamics, Noise, and Airport compatibility; Structures -- Criteria and loads analysis, Stress analysis, Structural design, Flutter and dynamic loads analysis, Weight and balance analysis, and Structural and material tests; Propulsion -- Inlet and exhaust test and analysis, Engine performance analysis, Propulsion system integration, Fuel system, and Propulsion control; Systems -- Avionics, Flight controls, Hydraulics and electrical, Environmental control and oxygen systems, Fire detecting and extinguishing systems, Flight instrument systems, Accessory power drive system; and Design Support and Integration -- Maintainability engineering and Customer engineering.

Development of a Supersonic Transport Aircraft Engine - Phase Ii-a

Author : PRATT AND WHITNEY AIRCRAFT EAST HARTFORD CONN.
Publisher :
ISBN 13 :
Total Pages : 8 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Development of a Supersonic Transport Aircraft Engine - Phase Ii-a by : PRATT AND WHITNEY AIRCRAFT EAST HARTFORD CONN.

Download or read book Development of a Supersonic Transport Aircraft Engine - Phase Ii-a written by PRATT AND WHITNEY AIRCRAFT EAST HARTFORD CONN. and published by . This book was released on 1964 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Analyses and Preliminary Design; Specifications; Compressor Development; Primary Combustion; Turbine Development; Augmentors; Exhaust System; Noise Reduction; Controls and Accessories; Bearing and Seal Development; Fuels; Lubricants; Inlets; Materials and Manufacturing Techniques; Operations and Economics; and Supporting Design Considerations.

Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-13. Propulsion Report-part B. Engine Installation Fuel System Exhaust System

Download Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-13. Propulsion Report-part B. Engine Installation Fuel System Exhaust System PDF Online Free

Author : BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV.
Publisher :
ISBN 13 :
Total Pages : 112 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-13. Propulsion Report-part B. Engine Installation Fuel System Exhaust System by : BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV.

Download or read book Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-13. Propulsion Report-part B. Engine Installation Fuel System Exhaust System written by BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Engine Installation; Fuel System; System Studies; Exhaust System; and Noise Suppression.

Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-12. Propulsion Report-part A. Engine Inlet and Controls

Download Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-12. Propulsion Report-part A. Engine Inlet and Controls PDF Online Free

Author : BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV.
Publisher :
ISBN 13 :
Total Pages : 308 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-12. Propulsion Report-part A. Engine Inlet and Controls by : BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV.

Download or read book Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-12. Propulsion Report-part A. Engine Inlet and Controls written by BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document includes the summary and three major sections of the propulsion report describing the engines, supersonic inlet, and the propulsion control systems. Studies conducted during Phase II C have resulted in significant improvements to the Boeing Model 2707 propulsion system. Optimum sized engines with improved thrust and fuel consumption characteristics are available from General Electric and Pratt and Whitney Aircraft. The four separate and interchangeable propulsion pods are mounted below the lower surface of the horizontal stabilizer at such a position that the engine exhaust will not impinge on any part of the airplane. The pod location and shape provides optimum lift effect on the airplane.

Development of a Supersonic Transport Aircraft Engine. Phase Ii-c

Author : PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FLA FLORIDA RESEARCH AND DEVELOPMENT CENTER.
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Development of a Supersonic Transport Aircraft Engine. Phase Ii-c by : PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FLA FLORIDA RESEARCH AND DEVELOPMENT CENTER.

Download or read book Development of a Supersonic Transport Aircraft Engine. Phase Ii-c written by PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FLA FLORIDA RESEARCH AND DEVELOPMENT CENTER. and published by . This book was released on 1965 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Engine Design; Engine Test; Compressor; Primary Combustor; Turbine; Augmentor; Exhaust System; Controls; Bearings and Seals; Fuels and Lubricants; Inlet System Compatibility; Noise; Mockups; Coordination; Maintainability; Value Engineering; Configuration Management; Quality Assurance; and Reliability.

Commercial Supersonic Transport Program. Phase Ii-a. Comprehensive Report. Volume Xiv-a. Aircraft System Concept

Author : BOEING CO RENTON WA AIRPLANE DIV.
Publisher :
ISBN 13 :
Total Pages : 33 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Commercial Supersonic Transport Program. Phase Ii-a. Comprehensive Report. Volume Xiv-a. Aircraft System Concept by : BOEING CO RENTON WA AIRPLANE DIV.

Download or read book Commercial Supersonic Transport Program. Phase Ii-a. Comprehensive Report. Volume Xiv-a. Aircraft System Concept written by BOEING CO RENTON WA AIRPLANE DIV. and published by . This book was released on 1964 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: The improved performance location of the engines reduces engine exhaust noise on the tail and fuselage, while virtually eliminating noise impingement on the wing. Sound suppression techniques are used and the structure is designed to be fully capable of coping with the temperature and noise for the design life of the airplane, even with occasional hot-day augmented operation under static and takeoff conditions. Passengers are located completely ahead of the engine exhaust nozzle noise cone. The aerodynamic pitchup tendency at high-angles-of-attack has been resolved in wind tunnel tests at both NASA Ames and Boeing. Risk of engine ingestion of debris and slush is eliminated by the use of deflectors and by providing greater distance between inlet and ground. Distribution of hydraulic system power to the control surfaces is balanced so that any failure of a power system does not result in asymmetric control surface operation. Spring-actuated mechanical locks are provided on the aileron and rudder control surfaces to prevent flutter in the event of hydraulic powr failure. Primary flight control system complexity has been reduced. Formal design reviews, system mockups, an extensive equipment quality analysis program, and an integrated test plan using large developmental test rigs provide early detection of problems and permit verification of system operation through prompt revision and refinement.