DK77197C - Compressor gas turbine system with a coolant channel in the rotor body. - Google Patents

Compressor gas turbine system with a coolant channel in the rotor body.

Info

Publication number: DK77197C
Authority: DK; Denmark
Prior art keywords: gas turbine; rotor body; turbine system; coolant channel; compressor gas
Prior art date: 1947-10-15

Application number

DK320548A

Other languages

Danish (da)

Original Assignee

Power Jets Res & Dev Ltd

Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)

1947-10-15

Filing date

1948-10-14

Publication date

1954-03-01

1948-10-14 Application filed by Power Jets Res & Dev Ltd filed Critical Power Jets Res & Dev Ltd

1954-03-01 Application granted granted Critical

1954-03-01 Publication of DK77197C publication Critical patent/DK77197C/en

Links

239000002826 coolant Substances 0.000 title 1

DK320548A 1947-10-15 1948-10-14 Compressor gas turbine system with a coolant channel in the rotor body. DK77197C (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
GB77197X		1947-10-15

Publications (1)

Publication Number	Publication Date
DK77197C true DK77197C (en)	1954-03-01

Family

ID=9838450

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
DK320548A DK77197C (en)	1947-10-15	1948-10-14	Compressor gas turbine system with a coolant channel in the rotor body.

Country Status (1)

Country	Link
DK (1)	DK77197C (en)

1948
- 1948-10-14 DK DK320548A patent/DK77197C/en active

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