Triple
T23457779
| Position | Surface form | Disambiguated ID | Type / Status |
|---|---|---|---|
| Subject | TAPS (Twin Annular Pre-mixing Swirler) |
E567979
|
entity |
| Predicate | instanceOf |
P0
|
FINISHED |
| Object | low-emissions combustor |
C47701
|
CONCEPT FINISHED |
How this triple was built (1 step)
Every LLM step that produced this triple, in pipeline order — named-entity classification, the disambiguation choices (the exact options shown, with the pick highlighted), and the generated description. The batch + timestamp of each is in the Provenance table below.
CD
Concept disambiguation
gpt-5-mini-2025-08-07
Target class: low-emissions combustor Context triple: [TAPS (Twin Annular Pre-mixing Swirler), instanceOf, low-emissions combustor]
-
A.
low‑carbon fuel project
A low‑carbon fuel project is an initiative that develops, produces, or deploys fuels with significantly reduced lifecycle greenhouse gas emissions compared to conventional fossil fuels, often involving advanced technologies, sustainable feedstocks, and emissions monitoring to support climate and energy transition goals.
-
B.
liquid-fueled rocket engine
A liquid-fueled rocket engine is a propulsion system that burns liquid propellants—typically a fuel and an oxidizer—pumped into a combustion chamber to produce high-velocity exhaust for thrust.
-
C.
hybrid rocket engine
A hybrid rocket engine is a propulsion system that uses propellants in two different phases—typically a solid fuel and a liquid or gaseous oxidizer—to generate thrust through controlled combustion.
-
D.
liquid-cooled aero engine
A liquid-cooled aero engine is an aircraft powerplant that uses a circulating liquid coolant, typically water or glycol, to absorb and dissipate heat from the engine, enabling higher performance and more consistent operating temperatures than air-cooled designs.
-
E.
scramjet demonstrator
A scramjet demonstrator is an experimental high-speed aircraft or test vehicle designed to validate and study the performance, control, and integration of supersonic combustion ramjet propulsion technology in realistic flight conditions.
- F. None of above. chosen
Provenance (1 batch)
The batch behind each pipeline step, in order, with when it ran. Timestamps are batch-level — stages were processed in waves, so the object chain (NER → NED1 → NEDg → NED2) reads in order, but predicate / elicitation batches can sit in a different wave.
| Step | Stage | Batch ID | Status | When |
|---|---|---|---|---|
| creating | Elicitation | batch_69e2458b4c888190b1d7998f9862a558 |
completed | April 17, 2026, 2:36 p.m. |
Created at: April 17, 2026, 5:53 p.m.