CHARLES RICHARD LEJAMBRE
Pilots at Blake Rd, New Britain, CT
License number
Connecticut A1108966
Issued Date
Jul 2015
Expiration Date
Jul 2017
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
474 Blake Rd, New Britain, CT 06053
Personal information
See more information about CHARLES RICHARD LEJAMBRE at radaris.comName
Address
Phone
15 Brewer St, East Hartford, CT 06118
474 Blake Rd, New Britain, CT 06053
New Britain, CT
474 Blake Rd, New Britain, CT 06053
36 Jerry Daniels Rd, Marlborough, CT 06447
Professional information
See more information about CHARLES RICHARD LEJAMBRE at trustoria.com
Coated Variable Area Fan Nozzle
Coated Variable Area Fan Nozzle
US Patent:
2009006, Mar 12, 2009
Filed:
Mar 22, 2007
Appl. No.:
11/689651
Inventors:
Gary D. Roberge - Tolland CT, US
Charles R. Lejambre - New Britain CT, US
Charles R. Watson - Windsor CT, US
Charles R. Lejambre - New Britain CT, US
Charles R. Watson - Windsor CT, US
International Classification:
F01D 17/16, F02K 1/06
US Classification:
415145, 60771, 415 1
Abstract:
A variable area fan nozzle for use with a gas turbine engine system includes a nozzle section that is movable between a plurality of positions to change an effective area associated with a bypass airflow through a fan bypass passage of a gas turbine engine. A protective coating is disposed on the nozzle section and resists change in the effective area of the nozzle section caused by environmental conditions.
Turbine Engine Compressor Vanes
Turbine Engine Compressor Vanes
US Patent:
7726937, Jun 1, 2010
Filed:
Sep 12, 2006
Appl. No.:
11/519629
Inventors:
P. William Baumann - Amesbury MA, US
Om Parkash Sharma - South Windsor CT, US
Charles R. LeJambre - New Britain CT, US
Sanjay S. Hingorani - Glastonbury CT, US
Om Parkash Sharma - South Windsor CT, US
Charles R. LeJambre - New Britain CT, US
Sanjay S. Hingorani - Glastonbury CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F04D 29/54
US Classification:
415191, 4151995, 4152084, 4152085, 4152112
Abstract:
A gas turbine engine rotor stack includes one or more longitudinally outwardly concave spacers. Outboard surfaces of the spacers may be in close facing proximity to inboard tips of vane airfoils. The airfoils have dihedral and sweep.