I must admit my error, when I read Dreyer, I was thinking Dewar. A dewar is of course an insulated storage vessel that you can store LOX in. With the reference to high pressure, this clearly makes the system being described as gaseous.
Wishing to look a bit further into it, I had a look at AP388 published in 1921, it describes all the systems then current, both liquid and gaseous.
They had got to Mk IV by then for liquid oxygen vaporizers and high pressure delivery regulators.
It seems a lot of development was made in the late and post war period.
From a document titled, “INITIAL EQUIPMENT MANUAL FOR SERVICE SQUADRONS IN THE AIR SERVICE, AMERICAN EXPEDITIONARY FORCES”
APPROVED BY G. H. Q.
SEPTEMBER 12, 1918
INSTRUCTIONS FOR “DREYER” OXYGEN APPARATUS
1. Apparatus (Dreyer).
The apparatus or regulator as used by the British and United States Air Services consists of an automatic aneroid controlled instrument so designed as to furnish the deficiency of oxygen in the air at any altitude.
Oxygen from the storage cylinder enters the regulator at approximately 2200 pounds depending upon the pressure in the storage cylinders. This initial pressure is reduced to atmospheric pressure and cannot exceed seventeen pounds to the square inch.
The hand controlled disc has the following markings : (a) Off., (b) One man (c) Two men. The disc must be set at the proper mark before starting a flight.
As the Airplane ascends the aneroids expand, thereby opening the port in the cylinder and the oxygen at atmospheric pressure is fed through to the low pressure outlet, to the pilot and observer, in increasing proportion the elevation increases.
The pressure gauge indicates the pressure remaining in the cylinder reservoir.
The flow indicator shows the flow to the passengers but does not revolve until the airplane is at an elevation of from 8000 to 10000 feet.
The apparatus itself should be screwed to the dash or side of the cockpit. There has been no definite place decided upon, as the type of plane and position of other instruments govern the location.
This apparatus is not to be dissembled or repaired in any way at squadrons and if not functioning properly a new apparatus must be installed.
Barring accidents and dirt the life of the apparatus is continuous. It should be installed in the pilot’s cockpit if possible but the services of the airplane and the location of other instruments will govern.
The rest of the document goes on to described the cylinders, masks in service etc.
So they were using LOX.
Dave
I am not trying to hijack your thread but my question is just an extension of yours.
I have been trying to locate the BBC interview with Jim Robinson, when he downed 2 aircraft in one day on the 28th August 1943, while flying in MA402 with 81 Sqn, over or near the Messina Straits.
Any leads to this “podcast” would be most welcome.
To answer your first question the RE8 is a candidate according to this web site.
http://www.simonahouse.com/index.php?route=product/product&product_id=129
Now the bit that interests me about this instrument. The supplier code is shown as S on both of these instruments. I have S as being the supplier code for Smith and Sons.
I will need more evident for, if the code was also used by Smiths.
Anyway powerandpassion you have given me another supplier code to add to my database on then (read, a short list that I would like to lengthen).
Its a drawing that I have no detail on, but here are some drawing numbers that are around it. It gives an idea of what was on the drawing boards at the time. Could the F.E.2D be a possibility?
A10078 Details of oil tank RE7
A10080 Detail gun mount FE2B and D
A10083 Radiator support FE2D
A10084 Socket L.H. & R.H., stay R.H. & LH., shock absorber, plate FE2D
A10089 Packing piece, clip FE2D
A10093 Details of block for turn button (front and rear) RE7
A10094 Details of cover, end filling piece (front and rear) RE7
I found a picture of a 5C/4205 on my computer and it looks a bit different to the adapter shown above. The new boost gauge is central within the plate. I found this auction on Ebay which may give more details.
I see that there is a picture of the “font” 2C on the web site referenced above.
http://www.uphill.org.uk/pictures/scans/medium/th_manual/09.jpg
Smiths standard, NUMERALS AND LETTERS FOR AIRCRAFT INSTRUMENT DIAL AND PANEL MARKINGS
From this 1958 standard, the following is given:
8 ENGRAVED CHARACTERS
Where characters are produced by engraving the following shall apply:-
8.1 Square ended cutters shall be used for lines .030″ or greater in width.
8.2 For lines under .030″ wide the cutter angle must not be greater than 60° included.
8.3 Engravings which are to be filled with a colour contrasting with the background shall not be less than .010″ deep.
8.4 Engravings which are to remain the same colour as the background shall be not more than .010″ deep.
8.5 The preferred masters used for engraving the characters are:-
LETTERS Smith Civil and M.O.S. Taylor Hobson 2C.
NUMERALS Smiths Civil 1 to 3, 8 , 0 Taylor Hobson 2C.
Smiths Civil 4 to 7, 9 Special.
NUMERALS M.O.S. 1 to 5, 7, 8, 0 Taylor Hobson 2C.
M.O.S. 6 and 7 Special.
I hope this adds to the collective knowledge as I do not know if the reference to Taylor Hobson is in fact a font?
Just had a look and they all follow the drawing convention that has been given.
369/17
476/18 etc
They appear to be prefixed by DFW.
From 1918 the drawings were issued by the air ministry
I have seen quite a few RFC airfield building plans in various locations on the net. Would this be of interest?
Resmoroh
Thanks for this confirmation. If you have a copy of the book, what are the other instruments shown in the index?
Ed
Will send you a couple of scans from a book I recently found. I have been meaning to write you an email on the subject, I guess it will be today.
It’s a book from the 1930’s which describes what specification steels etc are most suited for what applications.
PM me I have some images. To avoid lowering the resolution, its best that I email them to you. They include a side view of a Serval 5.
I found the NACA No. 240 report on line.
https://archive.org/download/nasa_techdoc_19930081042/19930081042.pdf
No teasing I’m afraid. The 1a profile is only really mentioned as an example in this book, giving values of a couple of parameters but no dimensional data.
Reference is also made to R & M 1383 (Wind tunnel tests on aerofoils at negative incidences) as well as B.A. 643. I suspect that B.A. 643 will reveal all if it can be located.