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The Turbo-Hydramatic or Turbo Hydra-Matic (THM) series was developed to replace both the original Hydra-Matic models and the Buick Dynaflow. In its original incarnation as the Turbo-Hydramatic 400, it was first used in the 1964 model year in Cadillacs. The Buick version, which followed shortly thereafter, was known as the Super-Turbine 400.
400+ [1] The Europrop International TP400-D6 is an 11,000 shp (8,200 kW) powerplant, developed and produced by Europrop International for the Airbus A400M Atlas military transport aircraft . The TP400 is the most powerful turboprop in service using a single propeller; only the Soviet-designed Kuznetsov NK-12 and Progress D-27 , using contra ...
Data from Extra EA-400 Standard Specification, Pilots Information Manual General characteristics Crew: 1 Capacity: 5 passengers Length: 9.57 m (31 ft 5 in) Wingspan: 11.5 m (37 ft 9 in) Height: 3.09 m (10 ft 2 in) Empty weight: 1,500 kg (3,307 lb) Max takeoff weight: 1,999 kg (4,407 lb) Powerplant: 1 × Continental TSIOL-550-C Voyager 6-cyl. horizontally opposed liquid cooled turbocharged ...
The 715 shp TPE331-6 used in the Beech King Air B100 have a 400-hr. fuel nozzle cleaning interval, 1,800-hr. hot section inspection interval and a 5,400-hr. time between overhaul; approval is possible for 3,000-hr. HSIs and 6,000-hr. overhauls and engine reserves are cheaper than for the PT6A.
The De Havilland Canada DHC-8, [2] commonly known as the Dash 8, is a series of turboprop-powered regional airliners, introduced by de Havilland Canada (DHC) in 1984. DHC was bought by Boeing in 1986, then by Bombardier in 1992, then by Longview Aviation Capital in 2019; Longview revived the De Havilland Canada brand. [3]
Introduced in 1970, the 402 cu in (6.6 L) was a 396 cu in (6.5 L) bored out by 0.03 in (0.76 mm). Despite being 6 cubic inches (98 cc) larger, Chevrolet continued marketing it under the popular "396" label in the smaller cars while at the same time labeling it "Turbo-Jet 400" in the full-size cars. Power rating(s) by year:
Data from Jane's All The World's Aircraft 1982–83 General characteristics Crew: 1 or 2 pilots Capacity: 8–10 passengers Length: 39 ft 0 in (11.89 m) Wingspan: 49 ft 4 in (15.04 m) Height: 13 ft 2 in (4.01 m) Wing area: 253.6 sq ft (23.56 m 2) Aspect ratio: 9.6:1 Airfoil: NACA 23018 at root, NACA 23019 at tip Empty weight: 5,682 lb (2,577 kg) Gross weight: 9,850 lb (4,468 kg) Powerplant: 2 ...
The BorgWarner developed turbo can produce up to 27 psi (1.9 bar) of boost thanks in part to its unique dual volute turbine housing and an electrically actuated wastegate. Instead of two side-by-side exhaust passages like on a regular twin-scroll turbocharger , in this design the two exhaust passages are concentric and allow for better use of ...
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