Patent US-1911-1039181

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  • Tech class: CPC B64C1/00: Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like; CPC G05D1/0061: Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
  • Inventor location: Washington, DC (FIPSloc=11001) (imputed by HistPat)

Sources


Year filed 1911
Year granted 1912
Office US
Patent number 1039181
Inventors Roy M. Palmer
Inventor country US
Inventor location Washington DC
Applicant person Roy M. Palmer
Applicant firm
Applicant type INDIV
Applicant is inventor? 1
Original title Aerostructural balance
English title Aerostructural balance
Tech fields balance
Filing date 1911-06-16
Full specification filed date
Application number 1911633468
Grant date 1912-09-24
Granted? 1
Publication date
Supplementary to patent
Related to aircraft? 1
Serial number 633468
Patent agent Harry Ellis Chandler
Assigned to
National tech categories USPC 244/177
IPCs
CPCs CPC B64C1/00, CPC G05D1/0061
Family year 1911
First filing? 1
Cites these patents
Citations from after 1930 0
Application ID 47538844
INPADOC family ID 43968063
Number of text pages 2
Number of diagram pages 2
Number of figures 5
Number of claims 4