US1807554A

US1807554A - Wilhelm rohn

Info

Publication number: US1807554A
Authority: US
Publication date: 1931-05-26
Anticipated expiration: 1948-05-26

Description

Patented May 26, 1931.

UNlTE DhS TATES PATENT OFFICE WILHELM ROHN, OF HANAU, GERMANY ALLOY non TURBINE BLADES AND momma PARTS nxrosn n 'ro smmaza oon'nrrrons No Drawing. Application filed December 16, 1936, Serial No. 155,345, and in Germany December 28, 1985.

It has been proposed by various persons to ilse chromium nickel alloys for the manu- "facture of gas and steam turbine blades and of machine parts exposed to similar 'me- 5 chanical, thermic and chemical conditions.

According to the proposals, such alloys contained 40% to 80% nickel, 12%25%. chromium and -30% iron. Besides the main ingredients, in certain cases-there was also 16,. used an addition of 2%5% molybdenum or tungsten. It has also been proposed to replace part of the nickel bycobalt.

The reason for not adopting in practice such alloys for the above-mentioned purposes,

15 is probably that these alloys produced by the processes of manufacture hitherto employed, and with the composition hitherto usual, failed to comply with all the conditions which have to be fulfilled by gas and steam turbine blades and by machine parts exposed to similar mechanical, thermic and chemical conditions.

, It has been found that the chief-reason for the non-adoption was that, according to the Z usual processes of manufacture, the alloys contained 0.2% and more per cent. of carbon, and that the alloys become much more 7 suitable for the purposes mentioned if they are made completely free from carbon. .The

39 absence of carbon reduces in the first place the brittleness of such alloys, so that their toughness or tenacity in the regio of the notch is considerably increased at t e temperatures to'be considered. In the second 5 place,'the resistance to corrosion of;al1oys free from carbon is very much greater than that oi carbon-containing alloys. For instance an. alloy consisting of 62% nickel, %-chromium,'22% iron and 1% manganese,

has four times smaller resistance-to corrosion by dilute sulphuric acid, and 400 times smaller resistance to corrosion by diluted nitric acid,

' thanlwhen it contains 0.9% carbon. In the 1 third place, chromium nickel alloys free from 45 carbon, are completely non-sensitive in heat treatment, so that for instance when soldering on the bands which extend around the ,m'outg' ends of. the turbine blades, and binding wiresfiheredsno need'xto pay any particular attention to the cooling conditions or toefiect a subsequent annealing with definite conditions of cooling. The toughness at the region of'the notch does not change at all, whether they be slowly cooled from the annealing temperature, or cooled suddenly. high yield- In order to ensure a sufliciently 'ing point, to the alloys maybe added up to 15% tungsten, up to 12% molybdenum or up to cobalt. It has been found that the same result maybe obtained by an addition of up to.6% aluminum.

The manufacture of such alloys free from carbon could be efiected by the so-called vacuum smelting process.

Having now particularly described and ascertained the nature of my said invention and in what manner the same is to be performed, I declare that what I claim is A turbine blade which is non-corrodible and non-sensitive by heat treatment to the. thermal, mechanical and physical conditions of use, consisting of an alloy com risin 10 to 40% of chromium, 40 to 85% o a nic ellikemetal, 10 to 40%ofiron, and u to 15% of a toughening metal having the c aracteristics of tungsten, the alloy being substantially free from carbon.

y In testimony whereof signature. g

' WILHELM ROHN.

I have aflixed my