Английская Википедия:Conformal fuel tank

Материал из Онлайн справочника
Перейти к навигацииПерейти к поиску

Шаблон:Short description

Файл:USAF F-15E Strike Eagle, Iraq 2004.jpg
A McDonnell Douglas F-15E Strike Eagle fitted with conformal fuel tanks under the wing roots
Файл:F-15E CFT.jpg
Ground crew handling the CFT of an F-15E

Conformal fuel tanks (CFTs) are additional fuel tanks fitted closely to the profile of an aircraft that extend the endurance of the aircraft.

Advantages

CFTs have a reduced aerodynamic penalty compared to external drop tanks, and do not significantly increase an aircraft's radar cross-section. Another advantage CFTs provide is that they do not occupy ordnance hardpoints like drop tanks, allowing the aircraft to carry its full payload.

Disadvantages

Conformal fuel tanks have the disadvantage that, unlike drop tanks, they cannot be discarded in flight, because they are plumbed into the aircraft and so can only be removed on the ground. As a result, they will impose a slight drag-penalty and minor weight gain on the aircraft even when the tanks are empty, without any benefit. They can also impose slight g-load limits, although not always an absolute issue: the CFTs on the F-15E actually allow the same maneuverability without g-limitations.

Examples

Conformal fuel tanks

F-15C entered service with CFT capability.[1] Initially known as FAST packs (Fuel And Sensor Tactical),[1] each unit carried an additional Шаблон:Convert of fuel,[2] while retaining hardpoints for four AIM-7F Sparrow missiles or bombs, some on the FAST packs.[3] They were first tested on the F-15B in 1974. All U.S. F-15Es, and Strike Eagle export variants such as the Israeli and Singapore models, are fitted with CFTs under the wing[4] outside the engine intake and require modification to fly without them.[5] The FAST pack was originally intended to carry a navigational and targeting infrared sensor system (thus "Fuel And Sensor"); however, the F-15 simply began carrying LANTIRN pods for ground-attack missions instead.[1]
Файл:Israeli F-16s at Red Flag2.jpg
Israeli F-16I Sufa, based on the F-16D Block 50/52+, with 2 attached CFTs on top of the aircraft near the wing root and 2 wing-mounted drop tanks.
Export aircraft for Greece, Chile, Israel, Poland, Pakistan, Turkey, Singapore, Morocco, Egypt and the UAE are plumbed for carriage of two CFTs mounted atop the aircraft near the wing root. Together they hold Шаблон:Convert, 3050lb of fuel.[6][7]
Two Шаблон:Convert CFTs were first tested by Dassault in April 2001.[8]Шаблон:Unreliable source?
One Шаблон:Convert CFTs in a further enlarged spine.[9][10]
Wind tunnel tested by BAE, two CFTs with Шаблон:Convert capacity each.[11][12]
The F-CK-1D prototype ("Brave Hawk") and the F-CK-1C single-seater prototype are equipped with the new CFTs. The prototype Indigenous Defence Fighter II “Goshawk” has over-wing CFTs.[13]
Conformal fuel tanks are mounted above the wings to replace the drag of underwing tanks. Combined, they carry 1,590 kg (3,500 lb) of extra fuel, while adding extra lift and expanding combat radius by 130 nmi (240 km) with a small transonic acceleration penalty.[14][15]
Wind tunnel tested by Chengdu.[16]
Conformal fuel tanks were installed on the wingtips.

Distended internal tanks

Distended internal tanks are fuel tanks that either create a bulge in the fuselage, or are mounted flush with the fuselage.

References

Notes

Шаблон:Reflist

Шаблон:Aircraft fuel tanks Шаблон:Aircraft components