Lockheed Flatbed

Lockheed Flatbed

__NOTOC__ Infobox Aircraft
name="Flatbed"


caption=
type=Military transport
manufacturer=Lockheed
designer=
first flight=
introduced=
retired=
status=Design study only
primary user=
more users=
produced=
number built=
variants with their own articles=

The Lockheed "Flatbed" was a proposed cargo aircraft design from the 1980s that mounted large loads "in the open" on the back of the aircraft, similar to a flatbed truck. The name "flatbed" was unofficial, a more formal name was never assigned. Although there was a fair amount of public information released about the design in the early 1980s, the design was never picked up by the US Air Force and disappeared by the mid-80s.

Conventional cargo designs generally "mass out" before they "bulk out", meaning that they often fly mostly empty inside. In this case the aircraft is carrying around a large fuselage for no reason, adding mass and drag and thereby lowering performance. Nevertheless they need to have oversized cargo bays for the cases where they have to carry bulky loads, rare as these may be. Lockheed's patent states it best:

:Historically, transport airplanes have generally been specifically designed to haul either cargo, passengers, or outsize cargo. ... Military cargo aircraft, such as the C-130 and C-141, are designed to haul cargo and some vehicles –but not outsize cargo such as tanks or bridge launchers. The C-5A can carry all militarily defined outsize cargo and large commercial vehicles. Some later military cargo airplanes can carry some outsize vehicles/equipment, but the price is paid in terms of carrying a large fuselage around for the few times such outsize cargo is actually carried. ... Thus an idea transport airplane is considered to be one which is designed to utilize one common airframe to carry passengers, cargo and outsize equipment.

The Flatbed concept avoided these problems by designing the aircraft primarily for massing out, the most common problem. An airliner-sized fuselage is all that is needed for this role. In the case when the aircraft was called upon to carry an oversized load, the cargo bay would be removed, and the cargo chained directly to the back of the aircraft, in the open. Although performance would be greatly degraded due to drag, this would be more than made up for on all the other flights where a more suitable fuselage size was being used.

In keeping with the flatbed concept, the aircraft was designed to sit low to the ground. Trucks would drive up to the aircraft and push their loads onto the back. The bed of the aircraft consisted of parallel I-beams as the primary load-carrying structure, with metal sheeting on the top to provide a smooth walking surface. Like most cargo aircraft, rollers could be raised through small holes cut in the bed to allow palletted loads to be rolled on and off without requiring a forklift.

In a conventional cargo aircraft the wing is high-mounted to keep the under-slung engines as far from the ground as possible. This avoids foreign object damage (FOD) when operating from dirty runways or dirt airfields. This layout also demands that the fuselage be supported from the top, essentially hanging from the wing's spars. For the Flatbed this would not be appropriate because the loads would be carried on top of the aircraft, not hung under it, so Lockheed moved the wing to the low-mounted position similar to most airliners. In order to avoid FOD, the engines were placed above the wing on pylons, which is aerodynamically similar on a modern symmetrical wing planform.

Likewise, most cargo aircraft use some version of a T-tail in order to leave the area at the end of the cargo bay "open" so trucks can approach it. This requires the tail to be high-mounted on the fuselage, so, as with the wings, this approach would not work on the Flatbed. Instead a large two-fin tail was used, extending outward from a point forward of the loading area, placing the rudders well to either side of the bed. In order to allow loading and unloading at the same time, the cockpit area at the nose of the aircraft could be rotated to the right, allowing trucks to approach both ends. The aircraft has a number of design features in common with the Lockheed L-1011, most obviously the crew cabin and cockpit area, and the overall size and layout.

The patent application shows it carrying two tanks (looking more like M4 Shermans than anything modern), and they also released concept artwork displaying various truck-like palletted loads mounted in a similar fashion. In these cases a small aerodynamic fairing was placed behind the cockpit area, which is flat at the rear, turning it into a sort of "pod". In most cases cargo would be carried under a cargo fairing that extended from the cockpit all the way to the tail, turning it into a fairly conventional-looking design, if somewhat "skinny" compared to traditional cargo designs like the C-5 Galaxy. Additionally, they proposed a passenger carrying module the same size as the cargo fairing. These modules could be unloaded as a single unit, sliding forward off the bed to a special-purpose truck.

aerospecs
met or eng?=
crew=
capacity=
length m=
length ft=
length in=
span m=
span ft=
span in=
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=
height ft=
height in=
wing area sqm=
wing area sqft=
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=
gross weight lb=
lift kg=
lift lb=
eng1 number=
eng1 type=
eng1 kw=
eng1 hp=
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=
max speed kmh=
max speed mph=
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=
armament1=
armament2=
armament3=
armament4=
armament5=
armament6=

References

* [http://www.freepatentsonline.com/4379533.html United States Patent #4,379,533] , "Transport Airplane", 12 April 1983
* [http://www.sae.org/technical/papers/801064 Flatbed -- a Unique and Versatile Transport Airplane]

ee also

aircontent

related=

similar aircraft=

sequence=

lists=

see also=


Wikimedia Foundation. 2010.

Игры ⚽ Поможем написать курсовую

Look at other dictionaries:

  • Air New Zealand — IATA NZ ICAO ANZ Callsign NEW ZEALAND …   Wikipedia

  • Integrated Automated Fingerprint Identification System — The Integrated Automated Fingerprint Identification System (IAFIS) is a national automated fingerprint identification and criminal history system maintained by the Federal Bureau of Investigation (FBI). IAFIS provides automated fingerprint search …   Wikipedia

  • SERV — In the top upper left is SERV with MURP SERV, short for Single stage Earth orbital Reusable Vehicle, was a proposed space launch system designed by Chrysler s Space Division for the Space Shuttle project. SERV was a single stage to orbit… …   Wikipedia

  • Dinky Toys — Dinky logo used in the late 1970s Dinky Toys are die cast miniature vehicles which were produced by Meccano Ltd of Liverpool, England, makers of Hornby railway sets. Contents …   Wikipedia

Share the article and excerpts

Direct link
Do a right-click on the link above
and select “Copy Link”