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公开(公告)号：AU675597B2
公开(公告)日：1997-02-06
申请号：AU7956994
申请日：1994-09-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor： PARKINSON GERALD W , BRADFORD MICHAEL
Abstract: An aircraft warning and display system monitors the status of various aircraft equipement (20, 22), and provides cockpit audible and visual messages and indications (52, 53, 59, 67) indicative o f the operational status of the equipment. The operational status of the aircraft is monitored (37, 40), and in response to changes in the operational status of the aircraft for a given equipment status, the priority level of cockpit audible and visual messages and indications are modified to attract the attention of a pilot when pilot action is required. Additionally, information may be displayed (52) to the pilot that indicates specific actions needed to downgrade the priority level of the cockpit messages/indications.
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公开(公告)号：ES2105773T3
公开(公告)日：1997-10-16
申请号：ES94930453
申请日：1994-09-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor： PARKINSON GERALD W , BRADFORD MICHAEL
Abstract: An aircraft warning and display system monitors the status of various aircraft equipement (20, 22), and provides cockpit audible and visual messages and indications (52, 53, 59, 67) indicative o f the operational status of the equipment. The operational status of the aircraft is monitored (37, 40), and in response to changes in the operational status of the aircraft for a given equipment status, the priority level of cockpit audible and visual messages and indications are modified to attract the attention of a pilot when pilot action is required. Additionally, information may be displayed (52) to the pilot that indicates specific actions needed to downgrade the priority level of the cockpit messages/indications.
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公开(公告)号：CA1016927A
公开(公告)日：1977-09-06
申请号：CA235711
申请日：1975-09-15
Applicant: UNITED TECHNOLOGIES CORP
Inventor： CARTER DONALD R , PARKINSON GERALD W , CUTTING JACK R
IPC: B64C27/00 , B64C27/46 , B64C27/473 , B64D45/02
Abstract: A composite helicopter blade made of electrically conductive and electrically nonconductive materials in which the blade parts most susceptible to being struck by lightning are either insulated from the lightning or are grounded to the blade root and hence to the fuselage.
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Patent Agency Ranking
公开(公告)号：AU682875B2
公开(公告)日：1997-10-23
申请号：AU6903694
申请日：1994-04-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor： VERNEY JAY FELTON , PARKINSON GERALD W
Abstract: In response to the loss of a generator in an electrical power system, all operating electrical loads are automatically switched to a second generator, and the electric power system continues to provide power to all of the loads. The total power required to operate all operating loads is permitted to exceed the nominal rated capacity of the operating generator, and the winding temperature or other critical hotspot temperature of the operating generator is monitored to determine whether thermal stress limits will be exceeded. If the critical hotspot temperature approaches the thermal stress limit, certain electrical loads are disconnected via a pre-programmed load shed priority schedule, and thereafter loads are re-connected as other loads are de-energized or if the critical hotspot temperature decreases.
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公开(公告)号：AU7956994A
公开(公告)日：1995-04-18
申请号：AU7956994
申请日：1994-09-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor： PARKINSON GERALD W , BRADFORD MICHAEL
Abstract: An aircraft warning and display system monitors the status of various aircraft equipement (20, 22), and provides cockpit audible and visual messages and indications (52, 53, 59, 67) indicative o f the operational status of the equipment. The operational status of the aircraft is monitored (37, 40), and in response to changes in the operational status of the aircraft for a given equipment status, the priority level of cockpit audible and visual messages and indications are modified to attract the attention of a pilot when pilot action is required. Additionally, information may be displayed (52) to the pilot that indicates specific actions needed to downgrade the priority level of the cockpit messages/indications.
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公开(公告)号：CA2172488A1
公开(公告)日：1995-04-06
申请号：CA2172488
申请日：1994-09-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor： PARKINSON GERALD W , BRADFORD MICHAEL
Abstract: An aircraft warning and display system monitors the status of various aircraft equipement (20, 22), and provides cockpit audible and visual messages ant indications (52, 53, 59, 67) indicative of the operational status of the equipement. The operational status of the aircraft is monitored (37, 40), and in response to changes in the operational status of the aircraft for a given equipement status, the priority level of cockpit audible and visual messages and indications are modified to attract the attention of a pilot when pilot action is required. Additionally, information may be displayed (52) to the pilot that indicates specific actions needed to downgrade the priority level of the cockpit messages/indications.
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公开(公告)号：AU6903694A
公开(公告)日：1994-12-20
申请号：AU6903694
申请日：1994-04-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor： VERNEY JAY FELTON , PARKINSON GERALD W
Abstract: In response to the loss of a generator in an electrical power system, all operating electrical loads are automatically switched to a second generator, and the electric power system continues to provide power to all of the loads. The total power required to operate all operating loads is permitted to exceed the nominal rated capacity of the operating generator, and the winding temperature or other critical hotspot temperature of the operating generator is monitored to determine whether thermal stress limits will be exceeded. If the critical hotspot temperature approaches the thermal stress limit, certain electrical loads are disconnected via a pre-programmed load shed priority schedule, and thereafter loads are re-connected as other loads are de-energized or if the critical hotspot temperature decreases.
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公开(公告)号：CA2161528A1
公开(公告)日：1994-12-08
申请号：CA2161528
申请日：1994-04-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor： VERNEY JAY FELTON , PARKINSON GERALD W
Abstract: In response to the loss of a generator in an electrical power system, all operating electrical loads are automatically switched to a second generator, and the electric power system continues to provide power to all of the loads. The total power required to operate all operating loads is permitted to exceed the nominal rated capacity of the operating generator, and the winding temperature or other critical hotspot temperature of the operating generator is monitored to determine whether thermal stress limits will be exceeded. If the critical hotspot temperature the thermal stress limit, certain electrical loads are disconnected via a pre-programmed load shed priority schedule, and thereafter loads are re-connected as other loads are de-energized or if the critical hotspot temperature decreases.
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