Aero Propulsion Alliance was a European aeroengine consortium set up to develop the TP400-D1 turboprop for the Airbus A400M military transport, using a modified SNECMA M88 high pressure spool as the gas generator. Early studies adopted a two shaft design with a shared-load power turbine, but a three-shaft configuration, with a free power turbine, was later adopted.
| Property | Value |
|---|
| dbpprop:abstract
|
- Aero Propulsion Alliance was a European aeroengine consortium set up to develop the TP400-D1 turboprop for the Airbus A400M military transport, using a modified SNECMA M88 high pressure spool as the gas generator. Early studies adopted a two shaft design with a shared-load power turbine, but a three-shaft configuration, with a free power turbine, was later adopted. However, Airbus considered the specific fuel consumption (SFC) of the TP400-D1 uncompetitive, so a new consortium (EuroProp International) was formed to develop the TP400-D6, with an all-new gas generator.
|
| dbpprop:hasPhotoCollection
| |
| rdf:type
| |
| rdfs:comment
|
- Aero Propulsion Alliance was a European aeroengine consortium set up to develop the TP400-D1 turboprop for the Airbus A400M military transport, using a modified SNECMA M88 high pressure spool as the gas generator. Early studies adopted a two shaft design with a shared-load power turbine, but a three-shaft configuration, with a free power turbine, was later adopted.
|
| rdfs:label
| |
| owl:sameAs
| |
| skos:subject
| |
| foaf:page
| |
| is owl:sameAs
of | |
![[RDF Data]](/statics/sw-cube.png)
