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Research and development of turbo engines in HYPR project. Choonsoku yusokiyo suishin system no kenkyu kaihatsu ni okeru turbo kei engine no shisaku

Journal Article:

Abstract

The present paper outlined the project which aimed at developing a combined cycle engine by a combination of turbojet engine operable from the takeoff or landing to Mach 3 and ramjet engine operable from Mach 2.5 to 5. The outline included the test result report of a prototypical engine which was the main subject of project. Upon conceptual research on the engine to comply with the future supersonic passenger plane, a variable cycle engine jointly equipped with a mixer/ejector noise lowering device was applied as a turbojet engine to lower the noise. The prototypical turbojet engine which was a target engine subscaled to about 1/10 in thrust aimed at demonstrating the total system performance of the turbojet engine which structured a combined cycle engine. Prior to testing the above prototype, the core engine was singly tested (in Phase 1) with a confirmed good result in firing and startup characteristics. 4 refs., 9 figs., 3 tabs.
Authors:
Watanabe, Y; Itahara, H; Kohara, S [1] 
  1. Ishikawajima-Harima Heavy Industries, Co. Ltd., Tokyo (Japan)
Publication Date:
May 01, 1994
Product Type:
Journal Article
Reference Number:
NEDO-94-920313; EDB-95-008234
Resource Relation:
Journal Name: Ishikawajima-Harima Giho (Ishikawajima-Harima Engineering Review); (Japan); Journal Volume: 34:3
Subject:
33 ADVANCED PROPULSION SYSTEMS; 32 ENERGY CONSERVATION, CONSUMPTION, AND UTILIZATION; AIRCRAFT; MACH NUMBER; PROPULSION SYSTEMS; SUPERSONIC TRANSPORT; TURBOFAN ENGINES; TURBOJET ENGINES; ENGINES; COMBINED CYCLES; IGNITION; START-UP; NOISE POLLUTION ABATEMENT; MIXERS; VAPOR JET EJECTORS; AIR TRANSPORT; EQUIPMENT; HEAT ENGINES; INTERNAL COMBUSTION ENGINES; MACHINERY; MATERIALS HANDLING EQUIPMENT; POLLUTION ABATEMENT; THERMODYNAMIC CYCLES; TRANSPORT; TURBOMACHINERY; VELOCITY; 330103* - Internal Combustion Engines- Turbine; 320201 - Energy Conservation, Consumption, & Utilization- Transportation- Air & Aerospace
OSTI ID:
6768591
Country of Origin:
Japan
Language:
Japanese
Other Identifying Numbers:
Journal ID: ISSN 0578-7904; CODEN: ISHGAV
Submitting Site:
NEDO
Size:
Pages: 167-171
Announcement Date:
Jan 15, 1995

Journal Article:

Citation Formats

Watanabe, Y, Itahara, H, and Kohara, S. Research and development of turbo engines in HYPR project. Choonsoku yusokiyo suishin system no kenkyu kaihatsu ni okeru turbo kei engine no shisaku. Japan: N. p., 1994. Web.
Watanabe, Y, Itahara, H, & Kohara, S. Research and development of turbo engines in HYPR project. Choonsoku yusokiyo suishin system no kenkyu kaihatsu ni okeru turbo kei engine no shisaku. Japan.
Watanabe, Y, Itahara, H, and Kohara, S. 1994. "Research and development of turbo engines in HYPR project. Choonsoku yusokiyo suishin system no kenkyu kaihatsu ni okeru turbo kei engine no shisaku." Japan.
@misc{etde_6768591,
title = {Research and development of turbo engines in HYPR project. Choonsoku yusokiyo suishin system no kenkyu kaihatsu ni okeru turbo kei engine no shisaku}
author = {Watanabe, Y, Itahara, H, and Kohara, S}
abstractNote = {The present paper outlined the project which aimed at developing a combined cycle engine by a combination of turbojet engine operable from the takeoff or landing to Mach 3 and ramjet engine operable from Mach 2.5 to 5. The outline included the test result report of a prototypical engine which was the main subject of project. Upon conceptual research on the engine to comply with the future supersonic passenger plane, a variable cycle engine jointly equipped with a mixer/ejector noise lowering device was applied as a turbojet engine to lower the noise. The prototypical turbojet engine which was a target engine subscaled to about 1/10 in thrust aimed at demonstrating the total system performance of the turbojet engine which structured a combined cycle engine. Prior to testing the above prototype, the core engine was singly tested (in Phase 1) with a confirmed good result in firing and startup characteristics. 4 refs., 9 figs., 3 tabs.}
journal = {Ishikawajima-Harima Giho (Ishikawajima-Harima Engineering Review); (Japan)}
volume = {34:3}
journal type = {AC}
place = {Japan}
year = {1994}
month = {May}
}