摘要:
Isolated polynucleotide from coryneform bacteria, comprising a polynucleotide sequence chosen from the group consisting of a) polynucleotide which is identical to the extent of at least 70% to a polynucleotide which codes for a polypeptide which comprises the amino acid sequence of SEQ ID No. 2, b) polynucleotide which is identical to the extent of at least 70% to a polynucleotide which codes for the polypeptide which is expressed by the pck gene contained on vector pK19mobsacB&Dgr;pck in the deposited E.coli strain DSM 13047, c) polynucleotide which codes for a polypeptide which comprises an amino acid sequence which is identical to the extent of at least 70% to the amino acid sequence of SEQ ID No. 2, d) polynucleotide which is complementary to the polynucleotides of a), b) or c) and e) polynucleotide comprising at least 15 successive bases of the polynucleotide sequence of a), b), c) or d).
摘要翻译:来自棒状细菌的分离的多核苷酸,包含选自以下的多核苷酸序列:a)与编码包含SEQ ID No.2的氨基酸序列的多肽的多核苷酸的程度相同的多核苷酸, b)与编码由沉积的大肠杆菌菌株DSM 13047中载体pK19mobsacBDELTApck上包含的pck基因表达的多肽的多核苷酸的程度至少70%相同的多核苷酸,c)编码 多肽,其包含与SEQ ID No.2的氨基酸序列至少70%相同的氨基酸序列,d)与a),b)或c)和ee)的多核苷酸互补的多核苷酸, 包含a),b),c)或d)的多核苷酸序列的至少15个连续碱基的多核苷酸。
摘要:
The invention relates to isolated nucleotide sequences from Coryneform bacteria which code for the pck gene encoding the enzyme phosphoenol pyruvate carboxykinase (PEP carboxykinase). The invention also relates a process for the fermentative preparation of L-amino acids, in particular L-lysine, L-threonine, and L-glutamate by attenuation of the pck gene.
摘要:
A device for attaching an aircraft cabin module, which device comprises a component with limbs for the releasable locking of a plug pin, fitted to the aircraft cabin module, and a plurality of electrical contacts. The component is configured in U shape as the rail component, the limbs thereof having locking points for the releasable locking of the plug pin fitted to the aircraft cabin module and the center portion thereof connecting the two limbs comprising the electrical contacts for the voltage supply and for the exchange of data with the aircraft cabin module.
摘要:
System and method for the voltage supply of aircraft cabin modules (1). An electric supply voltage and an additive data signal are transmitted via a cable (3). The aircraft cabin modules (1) have a connection plug (2) for plugging onto the cable (3) and an isolating circuit (5), which isolates the transmitted supply voltage from the data signal.
摘要:
A device is provided for fastening a first part to a stationary second part, in particular to a part of a vehicle, having a fastening element which can be connected to the first part and has at least one locking element arranged so it cannot be lost, such that it can be brought into a locked position where the first part is joined to the second part and it can also be brought into an unlocked position where the first part is released from the second part, where the fastening element has a top part facing the second part and a bottom part facing the first part, where the top part and the bottom part are designed to pivot about a pivot axis, and the locking element is mounted on the top part.
摘要:
A supply module is provided for a passenger transport vehicle that includes, but is not limited to a first supply unit for supplying passengers with a first supply medium in a first supply area and a second supply unit for supplying passengers with a second supply medium in a second supply area. Furthermore, the supply module includes, but is not limited to a control unit which is configured to activate the first supply unit in a first subregion of the first supply area and to activate the second supply unit in a second subregion of the second supply area, based on a predeterminable seating configuration.
摘要:
An apparatus and a method for transferring data and energy over network units of a defined network. The apparatus has at least two units, a bus coupling the units with a receive line and a transmit line and a bus control device coupled with the bus, the bus control device having first means for controlling the transfer of data defined by the defined network as data voltage signals over the transmit line and over the receive line, second means for charging the data voltage signals on the transmit line with first supply voltage signals adapted for voltage supply of units of a first plane system, and third means for charging the data voltage signals on the receive line with second supply voltage signals adapted for voltage supply of units of a second plane system.
摘要:
A method for displaying information by means of a dual-view-display in a passenger-cabin of an air-/spacecraft, comprising the following steps: providing the dual-view-display on a predetermined portion of the passenger-cabin; providing first information by means of the dual-view-display, in such a way that said information can be perceived from a gangway between rows of seats of the passenger cabin; and simultaneously providing second information, different from the first information, by means of the dual-view-display, in such a way that said information can be perceived from one of the rows of seats. A display device for displaying information in a passenger-cabin of an air-/spacecraft, comprising a dual-view-display which is arranged on a predetermined portion of the passenger-cabin, the dual-view-display being configured to provide first and second information in the above described ways. A passenger-cabin for an air-/spacecraft comprising said display-device. An air-/spacecraft comprising said display-device or said passenger-cabin.
摘要:
System and method for the voltage supply of aircraft cabin modules (1). An electric supply voltage and an additive data signal are transmitted via a cable (3). The aircraft cabin modules (1) have a connection plug (2) for plugging onto the cable (3) and an isolating circuit (5), which isolates the transmitted supply voltage from the data signal.
摘要:
A method of monitoring and controlling aircraft cabin systems using a user interface having a touch sensitive display and a plurality of input keys corresponding to the systems. One of the input keys corresponding to a first aircraft cabin system is activated to display a first system graphical menu having status information and operating functions of the first system, and a touch sensitive input area of the first system graphical menu is touched to perform selection or control of the first system. Another one of the input keys corresponding to a second aircraft cabin system can be activated to display a second system graphical menu having status information and operating functions of the second system, and a touch sensitive input area of the second system graphical menu can be touched to perform selection and control of the second system.