JOHN CHRISTOPHER FANNING
Pilots at Mcnerney Dr, Henderson, NV
License number
Nevada A4263297
Issued Date
Jun 2016
Expiration Date
Dec 2016
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
261 Mcnerney Dr, Henderson, NV 89012
Professional information
Alpha-Beta Ti-Ai-V-Mo-Fe Alloy
US Patent:
6786985, Sep 7, 2004
Filed:
May 9, 2002
Appl. No.:
10/140884
Inventors:
Yoji Kosaka - Henderson NV
Stephen P. Fox - Henderson NV
John C. Fanning - Henderson NV
Stephen P. Fox - Henderson NV
John C. Fanning - Henderson NV
Assignee:
Titanium Metals Corp. - Henderson NV
International Classification:
C22C 1400
US Classification:
148421, 420421, 420420
Abstract:
High strength alpha-beta alloy comprising essentially Al: 4. 5-5. 5%, V: 3. 0-5. 0%, Mo: 0. 3-1. 8%, Fe: 0. 2-1. 2%, oxygen 0. 12-0. 25% Ti: balance. All other incidental elements should be less than 0. 1% for each element and less than 0. 5% in total. The alloy possesses improved machinability and ballistic performance compared to Ti-6Al-4V.
Near-Beta Titanium Alloy For High Strength Applications And Methods For Manufacturing The Same
US Patent:
8454768, Jun 4, 2013
Filed:
Mar 29, 2012
Appl. No.:
13/433458
Inventors:
John Fanning - Henderson NV, US
Assignee:
Titanium Metals Corporation - Exton PA
International Classification:
B64C 25/02
US Classification:
148669, 148566, 148671
Abstract:
A high strength near-beta titanium alloy including, in weight %, 5. 3 to 5. 7% aluminum, 4. 8 to 5. 2% vanadium, 0. 7 to 0. 9% iron, 4. 6 to 5. 3% molybdenum, 2. 0 to 2. 5% chromium, and 0. 12 to 0. 16% oxygen with balance titanium and incidental impurities is provided. An aviation system component comprising the high strength near-beta titanium alloy, and a method for the manufacture of a titanium alloy for use in high strength, deep hardenability, and excellent ductility applications are also provided.
Low-Cost Alpha-Beta Titanium Alloy With Good Ballistic And Mechanical Properties
US Patent:
2012020, Aug 9, 2012
Filed:
Aug 5, 2010
Appl. No.:
12/850691
Inventors:
John Fanning - Henderson NV, US
Assignee:
TITANIUM METALS CORPORATION - Dallas TX
International Classification:
C22C 14/00, C22F 1/18, B32B 15/01, B22D 25/00
US Classification:
428544, 164 47, 164 761, 148557, 420420
Abstract:
An alpha-beta Ti alloy having improved mechanical and ballistic properties formed using a low-cost composition is disclosed. In one embodiment, the Ti alloy composition, in weight percent, is 4.2 to 5.4% aluminum, 2.5 to 3.5% vanadium, 0.5 to 0.7% iron, 0.15 to 0.19% oxygen and balance titanium. The exemplary Ti alloy exhibits a tensile yield strength of at least about 120,000 psi and an ultimate tensile strength of at least about 128,000 psi in both longitudinal and transverse directions, a reduction in area of at least about 43%, an elongation of at least about 12% and about a 0.430-inch-thick plate has a Vballistic limit of about 1936 fps. The Ti alloy may be manufactured using a combination of recycled and/or virgin materials, thereby providing a low-cost route to the formation of high-quality armor plate for use in military systems.
Near-Beta Titanium Alloy For High Strength Applications And Methods For Manufacturing The Same
US Patent:
2010032, Dec 23, 2010
Filed:
May 28, 2010
Appl. No.:
12/790502
Inventors:
John Fanning - Henderson NV, US
Assignee:
TITANIUM METALS CORPORATION - Dallas TX
International Classification:
B64C 25/00, C22C 14/00, C22F 1/18, B64C 1/06
US Classification:
244100 R, 420418, 148669, 148566, 148671, 244131
Abstract:
A high strength near-beta titanium alloy including, in weight %, 5.3 to 5.7% aluminum, 4.8 to 5.2% vanadium, 0.7 to 0.9% iron, 4.6 to 5.3% molybdenum, 2.0 to 2.5% chromium, and 0.12 to 0.16% oxygen with balance titanium and incidental impurities is provided. An aviation system component comprising the high strength near-beta titanium alloy, and a method for the manufacture of a titanium alloy for use in high strength, deep hardenability, and excellent ductility applications are also provided.
Titanium Alloy With Improved Properties
US Patent:
2012010, May 3, 2012
Filed:
Jan 12, 2012
Appl. No.:
13/349483
Inventors:
Roger Thomas - Swansea, GB
Paul Garratt - Birmingham, GB
John Fanning - Henderson NV, US
Paul Garratt - Birmingham, GB
John Fanning - Henderson NV, US
Assignee:
TITANIUM METALS CORPORATION - Dallas TX
International Classification:
F01D 5/14, C22C 14/00, C22F 1/18
US Classification:
416241 R, 148669, 420420
Abstract:
A titanium alloy having high strength, fine grain size, and low cost and a method of manufacturing the same is disclosed. In particular, the inventive alloy offers a strength increase of about 100 MPa over Ti 6-4, with a comparable density and near equivalent ductility. The inventive alloy is particularly useful for a multitude of applications including components of aircraft engines. The Ti alloy comprises, in weight percent, about 6.0 to about 6.7% aluminum, about 1.4 to about 2.0% vanadium, about 1.4 to about 2.0% molybdenum, about 0.20 to about 0.42% silicon, about 0.17 to about 0.23% oxygen, maximum about 0.24% iron, maximum about 0.08% carbon and balance titanium with incidental impurities.