The Pratt & Whitney TF30 (company designation JTF10A[1]) is a military low-bypass turbofan engine originally designed by Pratt & Whitney for the subsonic F6D Missileer fleet defense fighter, but this project was cancelled.

Subseries 7. houses operation manuals, service guides, production information, and reports on both propeller and jet powered aircraft engines. Subseries 8. contains reports, documents, photographs, and articles, related to milestones and important moments in aviation.

Dec 17, 2021 · When the F-14 Tomcat first entered service, it was powered by a pair of Pratt & Whitney TF30 engines that had been designed for the F-111B, which was more multi-role bomber than fighter. These engines were powerful, but incredibly problematic, ultimately leading to the loss of as many as 40 Tomcats over the years.

Sep 15, 2011 · Well, a glance at a table in Jack Connor's The Engines of Pratt and Whitney: A Technical History shows 38 versions of the JTF10A/TF30 ranging from 41.6 inches to 50.7 inches in diameter falling into two main camps Afterburning models Engines for the FB-111 are 50.7 inches The TF-30-P-100 for the F-111F is 48.9 inches Other F-111 models are 48 ...

Nov 21, 2004 · Pratt & Whitney TF30: The Engine: Specifications (TF30-P-3) The TF30 was Pratt & Whitney's first afterburning turbofan. Selected for the F-111, there were problems matching the engine with the aircraft, specifically the inlet system.

The Pratt & Whitney TF30 (company designation JTF10A [1]) is a military low-bypass turbofan engine originally designed by Pratt & Whitney for the subsonic F6D Missileer fleet defense fighter, but this project was cancelled.

The TF30 engine breather-pressure modification consists of an engine sensor that detects an abnormal condition to allow the pilot time to take action to prevent engine failure.

Aug 17, 2012 · Advanced Floatwall combustor liner technology eliminates TF30-P-100 transition duct fatigue cracking. T. DUBELL, J. LETOURNEAU and R. KAPLAN

Dec 27, 2005 · The TF30-P-100/111 engine for the F-111F had a redesigned fan and low compressor with a bulged flow path in the LPC that increases airflow, pressure ratio, and distortion tolerance, which in addition to a higher temperature capable turbine resulted in a big step up in performance, with takeoff max AB thrust going up from the 19k range to 25k ...

TF30 P100 engine exhaust nozzle, a similar thrust class engine of 1960'svintage used to power the FIll aircraft. Extensive design trades were made before choosing a cooled inner fiowpath configuration with titanium structural flaps as opposed to an uncooled system with heavier higher temperature capability superalloys such as INCO 718 and Waspaloy.