To build off the materials theme of the last post, the Society of Automotive Engineers published a compilation of various papers presented over the years titled
History of Aircraft Lubricants in 1997. (See the
The History of North American Small Gas Turbine Aircraft Engines for a similar aerospace technical history produced by an industry association.
[1])
The discussion of plastics in the last post is also an excellent segue into claims of the first use of flush or recessed rivets in aviation as the goal of both was to make a smoother skin for increased speed. In March 1941, a man working for Douglas Aircraft Company, Vladimir H. Pavlecka, was issued a patent,
2,233,820, for countersunk rivets.
[2][3]Now, for a bit of a foray now into aircraft intakes.
The first aircraft with an inlet cone may have been the prototype of the MiG-21, the Ye-2, which first flew on 14 February 1955.
[4] In the West, it was also a prototype: the P.1B. While the original progenitors to the English Electric Lightning, the P.1As, lacked an inlet cone, the these later variants incorporated one. It was on 4 April 1957, that the first of the three P.1Bs, XA847, flew for the first time.
[5]Between these two milestones was the first flight of another aircraft: the F-107. It has already been mentioned in a
previous post for potentially being the first modern aircraft with a side-stick. However, this was apparently not the only innovation it introduced. It also may have been the first aircraft with variable intake ramps or, as it was known at the time, variable-area inlet ducts (VAID). While the first F-107 first flew earlier, the third aircraft, 55-5120, was only one to have VAID installed. It had its first flight on 10 December 1956.
[6] While I was not able to find a patent showing the F-107, I did come across a later one,
2,876,621, depicting the design of the F-104.
The first aircraft with a splitter plate,
per se, may have been the F-4 Phantom II. If so, the first airframe with them would be YF4H-1, 142260.
[7] However, it is worth noting that the problem the device solves - turbulent boundary layer air being ingested into an engine - was something that was being addressed as early as the P-51. As can be seen in
pictures of its accident, the original NA-73X had its oil cooler intake flush mounted with the bottom of the fuselage. It may even even have been the cause of the accident.
[8] Therefore, later Mustangs featured a gap at this location. Furthermore, the difference between a splitter plate - which could be defined as a separate part extending ahead of the intake - and an intake with an integral separation is blurry. Even the pre-prototype for the F-4, the F3H-G, featured this design.
[9]The diverterless supersonic inlet, as seen on the F-35, was first tested on an F-16, 83-1120.
[10][11]Also on the subject of powerplants, in a situation not uncomparable to the Kommandogerat in the BMW 801 (see
previous post), the Germans were again first with autothrottles. (At the same time, it is worth keeping in mind the
narrative myth of German superiority in technology.) Although I was unable to find specific dates or detailed descriptions, the Me 262 was equipped with them. (While searching for information on the subject, I discovered the Germans also invented a yaw damper for the 262 as well.
[12]) However, the modern commercial autothrottle was invented by a man named
Leonard Greene and tested on a C-53, 11636, 42-68790, N733A, in 1956.
[13][14] (Mr. Green's work on the stick shaker was mentioned in a
previous post.) The technology was called "AutoPower" and apparently received patent
2,881,635.
The subject of self-sealing fuel tanks was mentioned in the
initial post of the thread, but hasn't been discussed until now. It was invented by George J. Murdock, who would receive patent
1,386,791 for the design. (For a very detailed narrative of advances during World War II, see the "
The Story of the Self-Sealing Tank" in the February 1946 issue of United States Naval Institute Proceedings.)
A related technology, the crashworthy fuel system (CWFS), was apparently pioneered by Dr. S. Harry Robertson III in the 1960s.
[15] The result was that the first CWFS was installed on a UH-1H in May 1970.
[16] (
Another article, which may offer additional detail, is unfortunately behind a paywall.)
EDIT (23-01-08): On the subject of splitter plates and boundary layer control, a
picture of the F7U at the National Naval Aviation Museum shows an interesting series of baffles between the intake and fuselage.
EDIT (24-06-28): As an addition to the story of the self-sealing fuel tank, there was apparently a lawsuit over credit for its invention filed in 1967. The plaintiff alleges he began experimenting with the technology in the mid-1930s and his patents of late 1941 and early 1942 were infringed upon by Martin-Marietta.
[17]