JOHN A MARTIN
Plumbers in Danvers, MA
License number
Massachusetts 20342
Issued Date
Jan 2, 1986
Expiration Date
May 1, 1988
Type
Journeyman Plumber
Address
Address
Danvers, MA 01923
Professional information
General Manager At Hostmark Hospitality Group
Position:
General Manager at Hostmark Hospitality Group
Location:
Greater Boston Area
Industry:
Hospitality
Work:
Hostmark Hospitality Group
- San Antonio, Texas Area since 2012
-
General Manager
Prism Hotels
- Multiple properties 2009 - 2012
-
General Manager-Task Force
Sage Hospitality
- Danvers, MA 2010 - 2011
-
General Manager, Crowne Plaza Hotel
Gemstone Hotels & Resorts
- Lake Lawn Resort, Delavan, WI. & Pala Mesa Golf Resort, San Diego, CA 2007 - 2008
-
General Manager
Handlery Hotel and Resort San Diego
2002 - 2007
-
General Manager, Handlery Hotel and Resort
Grand Heritage Hotel Group
- Cleveland/Akron, Ohio Area 2000 - 2002
-
Vice President Operations
The Kimpton Group
- Greater Chicago Area 1999 - 2000
-
General Manager, Hotel Allegro Chicago
Education:
Broward College
Educational Institute, American Hotel and Motel Association
Educational Institute, American Hotel and Motel Association
Interests:
Hospitality, tourism, fishing, diving, football, and new cultures
Awards:
Profit Improvement Award
Sage Hospitality
Sage Hospitality
Certifications:
GM Certification, IHG
Engine Full Authority Digital Engine Control Automatic Mach Hold
US Patent:
5517819, May 21, 1996
Filed:
Dec 19, 1994
Appl. No.:
8/359254
Inventors:
John F. Martin - Danvers MA
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F02C 600, F02C 900
US Classification:
60204
Abstract:
An engine controller system maintains a desired mach number for an aircraft. The fan speed of a slave engine is synchronized with the fan speed of a master engine. A previous Mach number value is compared with an actual Mach number value to determine a Mach number error. The resulting error corresponds to a fan speed which increases or decreases engine thrust to achieve a Mach number error equal to zero, maintaining the desired aircraft Mach number.