http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CA-1305771-C
Outgoing Links
Predicate | Object |
---|---|
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C11-305 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C9-58 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D31-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C9-28 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C11-30 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C9-58 |
filingDate | 1989-08-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate | 1992-07-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_eb98c2a0f94502c1b69f0b206c74b4cb http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_fc406522ebb48c2a16d18bc903502dc4 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_02eb8f6080bf09bbeea98320b4a14e87 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6a58d25b190d87ed1753ec526a4baa69 |
publicationDate | 1992-07-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | CA-1305771-C |
titleOfInvention | Aircraft propeller speed control |
abstract | AIRCRAFT PROPELLER SPEED CONTROL ABSTRACT OF THE DISCLOSURE The invention concerns a control for an aircraft propeller. During operation in reverse pitch, as occurs upon thrust reversal during a landing maneuver; the speed of the propeller is controlled by adjusting pitch of the propeller, in order to prevent overspeeding. Further, during the transition period while the propeller is converting from forward pitch to reverse pitch, the propeller presents a light load to the engine. At this time, fuel flow to the engine is limited in order to restrict delivery of energy to the propeller, again, for the purposes of preventing overspeeding. |
priorityDate | 1988-12-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 24.