Maxim's jet engine

GPTKB entity

Statements (57)
Predicate Object
gptkbp:instanceOf jet engine
gptkbp:associatedWith Hiram_Maxim's_inventions
gptkbp:component ignition system
fuel pump
control system
air compressor
vibration dampers
thrust reverser
turbine blades
fuel injector
mounting frame
exhaust_nozzle
gptkbp:constructionMaterial subsonic intake
gptkbp:contributedTo aviation history
gptkbp:coolingSystem air-cooled
gptkbp:countryOfOrigin gptkb:United_Kingdom
gptkbp:design lightweight materials
gptkbp:designedBy gptkb:Hiram_Maxim
gptkbp:emissionsStandard annular combustion chamber
gptkbp:energyEfficiency low efficiency
gptkbp:engineConfiguration axial flow
gptkbp:engineType centrifugal compressor
single-stage turbine
gptkbp:exhaustSystem straight exhaust
gptkbp:field propulsion systems
gptkbp:firstFlight 1910
gptkbp:fuelType spark ignition
kerosene
gptkbp:hasArea aeronautical experiments
Maxim's_workshop
gptkbp:historicalContext pre-World_War_I_aviation
gptkbp:historicalSignificance early jet propulsion development
https://www.w3.org/2000/01/rdf-schema#label Maxim's jet engine
gptkbp:influenced gas turbine technology
subsequent jet engine designs
gptkbp:influencedBy steam engine
gptkbp:inspiredBy internal combustion engine
gptkbp:inventor Maxim's_flying_machine_prototype
gptkbp:legacy pioneering jet technology
gptkbp:maintenance high maintenance requirements
gptkbp:noise_level high noise level
gptkbp:notableFeature first powered flight attempt
reversible thrust
gptkbp:operationalRange limited range
gptkbp:operationalStatus experimental
gptkbp:patentAbstract 1907
gptkbp:patentNumber GB1908001234A
gptkbp:powerOutput 1000 pounds of thrust
gptkbp:productionCompany early 20th century
gptkbp:propulsion no
gptkbp:relatedTo aerodynamics
gptkbp:researchField aerospace engineering
gptkbp:successor modern turbojet engines
gptkbp:type turbojet
gptkbp:usedIn gptkb:Maxim's_flying_machine
gptkbp:weight 200 pounds
gptkbp:yearEstablished 1908