AU2002303573A1 - Device for controlling the deployment of jet engine thrust reversers - Google Patents

Device for controlling the deployment of jet engine thrust reversers

Info

Publication number
AU2002303573A1
AU2002303573A1 AU2002303573A AU2002303573A AU2002303573A1 AU 2002303573 A1 AU2002303573 A1 AU 2002303573A1 AU 2002303573 A AU2002303573 A AU 2002303573A AU 2002303573 A AU2002303573 A AU 2002303573A AU 2002303573 A1 AU2002303573 A1 AU 2002303573A1
Authority
AU
Australia
Prior art keywords
deployment
controlling
jet engine
engine thrust
thrust reversers
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU2002303573A
Inventor
Terry Ahrendt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell International Inc filed Critical Honeywell International Inc
Publication of AU2002303573A1 publication Critical patent/AU2002303573A1/en
Abandoned legal-status Critical Current

Links

AU2002303573A 2001-04-30 2002-04-30 Device for controlling the deployment of jet engine thrust reversers Abandoned AU2002303573A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/846,914 2001-04-30

Publications (1)

Publication Number Publication Date
AU2002303573A1 true AU2002303573A1 (en) 2002-11-11

Family

ID=

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