Search

Malcolm C Staddon

from Middlefield, CT
Age ~61
Get Report
Related to:
Jacqueline M Staddon, 63Alexander C Staddon, 28
Connected to:
Ruth M Staddon, 110Bryan L Stade, 57Caroline M Stade, 98Mary E Stade, 59Terry Stade, 54Benjamin L Stadel, 41Brandon L Stadel, 51Gerhard P Stadel, 84Mark W Stadelbacher, 41Jay A Stadeli, 47

Malcolm Staddon Phones & Addresses

  • 22 Rosemary Ct, Middlefield, CT 06455 (860) 349-3895
  • Meriden, CT
  • 22 Rosemary Ct, Middlefield, CT 06455

Work

Position: Executive, Administrative, and Managerial Occupations

Education

Degree: High school graduate or higher

Publications

Us Patents

Engine Assembled Seal

US Patent:
20110262274, Oct 27, 2011
Filed:
Apr 21, 2010
Appl. No.:
12/764212
Inventors:
Lynn M. Boy - Durham CT, US
Malcolm C. Staddon - Middlefield CT, US
Assignee:
UNITED TECHNOLOGIES CORPORATION - Hartford CT
International Classification:
F01D 25/00
B21D 53/84
US Classification:
416174, 298883
Abstract:
A system for creating a seal between a damper and a platform of a turbine engine component includes a turbine engine component having an airfoil portion, a platform, and a fir tree for joining the turbine engine component to a rotor, a damper located in an area beneath the platform, a seal having a sealing surface which seats against an underside of the platform, which seal has a seal retention feature which bends into contact with an underside of the damper, and which seal with the seal retention feature has a center of gravity which allows the seal retention feature to bend up as result of rotational movement of the rotor. A method for creating the seal is also described.

Gas Turbine Engine Airfoil Trailing Edge Passage And Core For Making Same

US Patent:
20150118064, Apr 30, 2015
Filed:
Mar 12, 2013
Appl. No.:
14/390496
Inventors:
- Hartford CT, US
Jeffrey S. Beattie - South Glastonbury CT, US
Malcolm C. Staddon - Middlefield CT, US
International Classification:
F01D 5/18
US Classification:
416 97 R
Abstract:
An airfoil has a body that includes leading and trailing edges that adjoin pressure and suction sides to provide an exterior airfoil surface. A cooling passage extends in a radial direction from a root to a tip. A trailing edge cooling passage interconnects the cooling passage to the trailing edge. The trailing edge cooling passage includes first and second pedestals of different sizes that are arranged in a repeating pattern with respect to pedestals of the same size and with respect to pedestals of different sizes.
Control profile
Malcolm C Staddon from Middlefield, CT, age ~61 Get Report